QRH 202-PEC

0.0172

GENERALOCT 08 001

TABLE OF CONTENTS

0 GENERAL

1 EMERGENCY PROCEDURES

2 PROCEDURES FOLLOWING FAILURES

3 NORMAL PROCEDURES

4 OPS DATA

5 MANAGEMENT PAGES

6 NORMAL CHECK LIST

COMMENTS ON PARTS 1 AND 2

LAYOUT

RThe boxed items correspond to actions performed by memory by thecrew within a minimum period of time

: highlights a precondition to apply an action

: highlights the moment when an action is to be applied

PROCEDURES INITIATION

No action will be taken (apart from depressing MC/MW pushbutton) :

RR

- until flight path is stabilized- under 400 ft above runway, except propeller feathering after enginefailure during approach at reduced power if go around is considered

RRR

At flight crew discretion, one reset of a system failure associated withan amber caution (except PEC SGL CH) may be performed byselecting OFF then ON related pushbutton.

Flight Crew may reengage a tripped circuit breaker only if he/shejudges it necessary for a safe continuation of the flight. In this caseonly one reengagement should be attempted.

If the failure alert disappears, continue normal operation and recordthe event in the maintenance log. If not, apply the associated failureprocedure.

Before performing a procedure, the crew must assess the situation asa whole, taking into consideration the failures, when fully identified,and the flight constraints imposed.

TASK SHARING

For all procedures, the general task sharing stated below isapplicable. The pilot flying remains pilot flying throughout theprocedure.

PF, Pilot Flying, responsible for :- PL- flight path and airspeed control- aircraft configuration- navigation

PNF, Pilot Non Flying, responsiblefor :

- Check List reading- execution of required actions- actions on OVHD panel- CL- communications

The AFCS is always coupled to the PF side (CPL selection)

ANALYSIS OF CONSEQUENCES OF A FAILURE ON FLIGHT

Basic airmanship calls for a management review of the remainingaircraft capabilities under the responsibility of CM1.

EM

ER

GE

NC

Y P

RO

CE

DU

RE

S

1.01

72

EMERGENCY SEP 07 001

1 - EMERGENCY PROCEDURES Content 1/1 IN FLIGHT ENG FIRE OR SEVERE MECHANICAL DAMAGE 1.02

R ON GROUND ENG FIRE OR SEVERE MECHANICAL DAMAGE 1.02 ON GROUND EMER EVACUATION 1.02 BOTH ENGINES FLAME OUT 1.03

ENG FLAME OUT AT TAKE OFF 1.04 BOMB ON BOARD 1.04

COCKPIT DOOR SECURITY SYSTEM 1.04A R SMOKE 1.05 R ELECTRICAL SMK 1.05A R AIR COND SMOKE 1.05A FWD SMK 1.06 AFT SMK 1.06

R AUX AFT COMPT SMK 1.06 DUAL DC GEN LOSS 1.07

R EMERGENCY DESCENT 1.07A DITCHING 1.08 FORCED LANDING 1.08A SEVERE ICING 1.09

1.02

72


IN FLIGHT ENG FIRE

OR SEVERE MECHANICAL DAMAGE

PL affected side .................................................................................. FI CL affected side .................................................. FTR THEN FUEL SO FIRE HANDLE affected side..........................................................PULL

After 10 seconds FIRST AGENT affected side.................................................. DISCH

If fire after further 30 seconds SECOND AGENT affected side ............................................ DISCH LAND ASAP SINGLE ENG OPERATION procedure (2.04)............................APPLY

ON GROUND ENG FIRE OR SEVERE MECHANICAL DAMAGE

PL 1 + 2............................................................GI / REVERSE AS RQD

When aircraft stopped PARKING BRAKE ............................................................. ENGAGE CL 1 + 2 .......................................................... FTR THEN FUEL SO FIRE HANDLE affected side ....................................................PULL FIRST AGENT affected side.................................................. DISCH If fire after further 30 seconds SECOND AGENT affected side ........................................ DISCH If evacuation required ON GROUND EMER EVACUATION procedure (1.02) ...APPLY

ON GROUND EMER EVACUATION

AIRCRAFT / PARKING BRAKE ................................ STOP / ENGAGE ATC (VHF 1) ............................................................................. NOTIFY CL 1 + 2 ............................................................... FTR THEN FUEL SO MIN CAB LIGHT ............................................................................... ON CABIN CREW (PA)................................................................... NOTIFY FIRE HANDLES 1 + 2....................................................................PULL AGENTS ...................................................................................AS RQD ENG START ROTARY SELECTOR...................OFF / START ABORT FUEL PUMPS 1 + 2........................................................................ OFF EVACUATION (PA) .................................................................INITIATE

Before leaving aircraft BAT ............................................................................................ OFF

1.03

72


BOTH ENGINES FLAME OUT

PL 1 + 2............................................................................................... FI

If NH drops below 30 % (no automatic relight) CL 1 + 2 .......................................................... FTR THEN FUEL SO FUEL SUPPLY .....................................................................CHECK OPTIMUM SPEED.................................................................. VmHB CAPT EHSI................................................................................ OFF COMMUNICATIONS .............................................................. VHF 1 ENG START ROTARY SELECTOR........................... START A & B

ENG 2 RELIGHT ENG 2 START PB .................................................................. ON When NH above 10 % CL 2 ..................................................................................FTR ENG 2 RELIGHT ....................................................MONITOR CL 2 then PL 2...........................................................AS RQD

ENG 1 RELIGHT ENG 1 START PB .................................................................. ON When NH above 10 % CL 1 ..................................................................................FTR ENG 1 RELIGHT ....................................................MONITOR CL 1 then PL 1...........................................................AS RQD

If neither engine starts CL 1 + 2 .......................................................... FTR THEN FUEL SO ENG START ROTARY SELECTOR..............OFF / START ABORT FUEL PUMPS 1 + 2................................................................... OFF FORCED LANDING (1.08A) or DITCHING (1.08) procedure ........... ...............................................................................................APPLY

CAUTION: Do not select AVIONICS VENT EXHAUST MODE to OVBD

If engine(s) recovered CL / PL engine(s) recovered................................................AS RQD If one engine not recovered CL engine NON recovered ........................ FTR THEN FUEL SO SYSTEMS affected.......................................................... RESTORE

Mod : 3973 or 4371 or 4457

1.04

72


ENG FLAME OUT AT TAKE OFF

UPTRIM .....................................................................................CHECK

If no UPTRIM PL 1 + 2 ................................................. ADVANCE TO THE RAMP AUTOFEATHER ........................................................................CHECK

Above 400 ft AGL PL affected side ............................................................................. FI CL affected side.............................................. FTR THEN FUEL SO

If damage suspected FIRE HANDLE affected side ....................................................PULL SINGLE ENG OPERATION procedure (2.04).......................APPLY

If no damage suspected ENG RESTART IN FLIGHT procedure (2.08) .......................APPLY If unsuccessful SINGLE ENG OPERATION procedure (2.04)..................APPLY

BOMB ON BOARD

AUTO PRESS - LANDING ELEVATION .................. CABIN ALTITUDE FLIGHT LEVEL................................ DESCEND TO CABIN ALTITUDE AVOID LOAD FACTORS HANDLE BOMB CAREFULLY - AVOID SHOCKS

When Z aircraft = Z cabin APPROACH CONFIG: FLAPS 15 GEAR DOWN ......... SELECTED AUTO PRESS.........................................................................DUMP SERVICE DOOR ................................................................UNLOCK PLACE BOMB NEAR SERVICE DOOR PREFERABLY IN A BAG ATTACHED TO THE DOOR HANDLE SURROUND IT WITH DAMPING MATERIAL CABIN ATTENDANT OXYGEN AND FIRE EXTINGUISHER........... ............................................................................ MOVE FORWARD PAX................................... MOVE FORWARD / CRASH POSITION LAND ASAP

Mod : 4111

1.05A72

EMERGENCYSEP 10 001

ELECTRICAL SMOKE

SMOKE procedure (1.05) ...........................................................APPLYAVIONICS VENT EXHAUST MODE ........................................... OVBDAIR FLOW......................................................................................HIGHDC SVCE AND UTLY BUS............................................................. OFFDC BTC.......................................................................................... ISOLACW GEN 1 + 2.............................................................................. OFFSUSPECTED EQUIPMENTS......................................................... OFF

If smoke origin not identifiedLAND ASAPACW TOTAL LOSS procedure (2.16A) .................................APPLY

If smoke origin identifiedNOT AFFECTED EQUIPMENTS .................................... RESTORE

When P < 1 PSIOVBD VALVE ................................................................FULL OPENAVIONICS VENT EXHAUST MODE......................................NORM

AIR COND SMOKE

R

SMOKE procedure (1.05) ...........................................................APPLYPACK VALVE 1............................................................................... OFFMAX FL ..................................................................................200 / MEA

If smoke persistsPACK VALVE 1 ........................................................................... ONPACK VALVE 2 ......................................................................... OFFCAUTION: Evacuation of air conditioning smoke may trigger

electrical smoke warning. Disregard it.ENGINES PARAMETERS......................... CAREFULLY MONITOR

If any anomaly occurs, such as:- amber engine caution illumination associated to local ITT alert- total loss of NL indication- engine abnormality clearly identified (NH, NL, ITT indications,

noise, surge…)

CAUTION: Confirm which engine is showing signs of abnormaloperation in order to avoid shutting down safe engine.

PL affected side ............................................................................. FICL affected side.............................................. FTR THEN FUEL SOSINGLE ENG OPERATION procedure (2.04).......................APPLY

1.0972

EMERGENCYSEP 04 001

SEVERE ICINGR

MINIMUM ICING SPEED ............................ INCREASE RED BUG by 10 ktPWR MGT .......................................................................................... MCTCL / PL ................................................................................... 100% / MCTAP (if engaged).......FIRMLY HOLD CONTROL WHEEL and DISENGAGESEVERE ICING CONDITIONS .....................................................ESCAPEATC...............................................................................................NOTIFY

n If an unusual roll response or uncommanded roll controlmovement is observed :

Push firmly on the control wheel FLAPS ..................................................................................... 15

n If the flaps are extended, do not retract them until the airframe isclear of ice.

n If the aircraft is not clear of ice :GPWS..........................................................FLAP/GPWS OVRDSTEEP SLOPE APPROACH (≥4.5°).......................PROHIBITEDAPP/LDG CONF.........................................MAINTAIN FLAPS 15

with "REDUCED FLAPS APP/LDG icing speeds" + 5 ktMultiply landing distance FLAPS 30 by 1.91.

DETECTIONVisual cue identifying severe icing is characterized by ice covering all or asubstantial part of the unheated portion of either side window

and / orUnexpected decrease in speed or rate of climb

and / orThe following secondary indications :. Water splashing and streaming on the windshield. Unusually extensive ice accreted on the airframe in areas not normally

observed to collect ice. Accumulation of ice on the lower surface of the wing aft of the protected

areas. Accumulation of ice on propeller spinner farther aft than normally

observed

The following weather conditions may be conducive to severe in-flighticing :. Visible rain at temperatures close to 0°C ambient air temperature (SAT). Droplets that splash or splatter on impact at temperatures close to 0°C

ambient air temperature (SAT)

Eng : PW124

1.10

72

EMERGENCY MAY 11 050

RECOVERY AFTER STALL or ABNORMAL ROLL CONTROL

CONTROL WHEEL........................................................ PUSH FIRMLY

If flaps 0° configuration FLAPS........................................................................................... 15° PWR MGT...................................................................................MCT CL / PL ........................................................................... 100% / MCT ATC ....................................................................................... NOTIFY If flaps are extended PWR MGT...................................................................................MCT CL / PL ........................................................................... 100% / MCT ATC ....................................................................................... NOTIFY

Note: this procedure is applicable whatever the LDG GEAR position is

(DOWN or UP)

RR UNRELIABLE AIRSPEED INDICATION

R

AP/YD/FD BARS .............................................................. OFF/OFF/STBY

PITCH AND TQ......................................................................... MAINTAIN If at take off or GA below 1500 ft:

PITCH IMMEDIATELY........................................................................8°

ICING / VOLCANIC ASHES CONDITIONS.................................ESCAPE PROBE HEATING, DE-/ANTI-ICING...................................... CHECK ON APM..................................................................................................... OFF

WARNING: respect STALL alarm. Note: Use any GPS speed information if available.

Take off phase, at or above acceleration altitude ALTITUDE.................................... MAINTAIN AT LEAST 30 SECONDS FLAPS..................................................................................................0° PITCH ..................................................................................................8° Note: Use climb table here after to adjust pitch if required. AFTER TAKE OFF normal procedure .........................................APPLY LAND AT THE NEAREST SUITABLE AIRPORT

Climb TLU ............................................................................................ LO SPD PWR MGT........................................................................................ CLB PL 1 + 2.......................................................................................NOTCH

Altitude (ft) 5000 10000 15000 20000 Normal conditions pitch 7° 5° 4° 3° Icing conditions pitch 6° 4° 3° 2°

Continuing next page …/…

Mod : 3973 or 4371 or 4457 Eng : PW124

1.11

72

EMERGENCY MAY 11 050

UNRELIABLE AIRSPEED INDICATION (CONT’D)

Cruise

ALTITUDE ............................................................................... MAINTAIN TLU............................................................................................... HI SPD Note: Average pitch around 0° at cruise speed PWR MGT .........................................................................................CRZ PL 1 + 2 ........................................................................................NOTCH

Descent TLU............................................................................................... HI SPD PITCH........................................................................MAINTAIN AT -2.5° PL 1 + 2 ........................................................................ ADJUST 30% TQ DESCENT normal procedure ........................................................APPLY

Initial Approach TLU.............................................................................................. LO SPD APPROACH normal procedure .....................................................APPLY CAUTION: Transition from clean configuration to LDG configuration is to be performed in level flight - REFER TO ALTIMETER - (if possible 30 seconds between each step). Note: Refer to following tables to adjust TQ:

TQ (Altitude of 3000ft) Aircraft configuration

- Average speed 14 T

18 T

22 T

Flaps 0° - 180 kt 45% 45% 50% FLAPS .................................................................................................15°

Flaps 15° - 150 kt 40% 40% 45% LDG GEAR ....................................................................................DOWN PWR MGT ........................................................................................... TO FLAPS .................................................................................................30°

Flaps 30° - 130 kt 45% 45% 50%

Final Approach PL 1 + 2 ........................................................................ ADJUST 35% TQ BEFORE LANDING normal procedure .........................................APPLY Note: Set an average pitch of -5° for a 3° slope approach.

Mod : 3973 or 4371 or 4457 Eng : PW124

1.04A72

EMERGENCYSEP 04 200

COCKPIT DOOR SECURITY SYSTEM

RRRRRRRR

Electrical Power LostMove the manual lock bolts to CLOSE positionNote : When the door is locked with the manual bolts, the

emergency access to the cockpit is unavailable. It isrecommended that at least two crew members remain inthe cockpit during that time.

Cockpit Door Jammed

l When cockpit exit requiredRemove the inspection seals from the two latches of the door left

panel (facing the door)Actuate the two corresponding latches as per placardsCOCKPIT DOOR LOCKING SYSTEM ............................... OFFDisconnect PLUG from the doorPush and remove corresponding door panel

Mod : 5377 + (5434 or 8330)

1.05

72


SMOKE

CREW OXY MASKS.............................................................ON / 100% GOGGLES................................................................................AS RQD CREW COMMUNICATIONS ..............................................ESTABLISH RECIRC FANS 1 + 2 ...................................................................... OFF AP ..................................................................................................... ON SMOKE SOURCE.................................................................. IDENTIFY

If source not identified or electrical smoke suspected Note: ELEC light may be activated by an air conditioning smoke source ELECTRICAL SMOKE procedure (1.05A) ............................APPLY

If air conditioning smoke identified AIR COND SMOKE procedure (1.05A) .................................APPLY

If FWD SMK illuminated or smoke in FWD zone of aircraft FWD SMOKE procedure (1.06).............................................APPLY

If AFT SMK illuminated or smoke in AFT zone of aircraft AFT SMOKE procedure (1.06) ..............................................APPLY

If AUX AFT COMPT SMK illuminated (depending on models) AUX AFT COMPT SMK procedure (1.06) .............................APPLY

1.05A

72


ELECTRICAL SMOKE

AVIONICS VENT EXHAUST MODE ........................................... OVBD AIR FLOW......................................................................................HIGH DC SVCE AND UTLY BUS............................................................. OFF DC BTC.......................................................................................... ISOL ACW GEN 1 + 2.............................................................................. OFF SUSPECTED EQUIPMENTS......................................................... OFF

If smoke origin not identified LAND ASAP ACW TOTAL LOSS procedure (2.16) ...................................APPLY

If smoke origin identified NOT AFFECTED EQUIPMENTS .................................... RESTORE

When ΔP < 1 PSI OVBD VALVE ............................................................... FULL OPEN AVIONICS VENT EXHAUST MODE......................................NORM

AIR COND SMOKE

PACK VALVE 1............................................................................... OFF MAX FL ..................................................................................200 / MEA

If smoke persists PACK VALVE 1 ........................................................................... ON PACK VALVE 2 ......................................................................... OFF CAUTION: Evacuation of air conditioning smoke may trigger

electrical smoke warning. Disregard it. ENGINES PARAMETERS......................... CAREFULLY MONITOR

If any anomaly occurs, such as: - amber engine warning illumination associated to local ITT alert - total loss of NL indication - engine abnormality clearly identified (NH, NL, ITT indications,

noise, surge…) WARNING: Confirm which engine is showing signs of abnormal

operation in order to avoid shutting down safe engine. PL affected side ............................................................................. FI CL affected side.............................................. FTR THEN FUEL SO SINGLE ENG OPERATION procedure (2.04).......................APPLY

1.06

72


FWD SMK

1) PASSENGERS VERSION CABIN CREW (PA).............................................................. ADVISE AVIONICS VENT EXHAUST MODE...................................... OVBD AIR FLOW ................................................................................HIGH EXTRACT AIR FLOW LEVER (RH MAINT PANEL)..........CLOSED CABIN CREW WITH PORTABLE EXTINGUISHER, LOCATE AND KILL SOURCE OF SMOKE When ΔP < 1 PSI OVBD VALVE.......................................................... FULL OPEN AVIONICS VENT EXHAUST MODE.................................NORM

2) CARGO VERSION CAB PRESS MODE SEL...........................................................MAN CAB ALT................................................................ MAX INCREASE ENG 2 BLEED (Except when in single bleed operation)........... OFF PACK VALVE 2 (Except when in single pack operation) .......... OFF CAB VENT AIR FLOW .............................................................. OFF FLIGHT COMPT TEMP SEL .....................................................HOT

CAUTION: LAND ASAP. If a quick landing is not possible, climb and maintain minimum FL160; FL200 is recommended.

Note: Smoke alert may be generated during smoke evacuation process.

AFT SMK

1) PASSENGERS VERSION CABIN CREW (PA).......................................ADVISE FOR ACTION AIR FLOW ................................................................................HIGH

2) CARGO VERSION CAB PRESS MODE SEL...........................................................MAN CAB ALT................................................................ MAX INCREASE ENG 2 BLEED (Except when in single bleed operation)........... OFF PACK VALVE 2 (Except when in single pack operation) .......... OFF CAB VENT AIR FLOW .............................................................. OFF FLIGHT COMPT TEMP SEL .....................................................HOT

CAUTION: LAND ASAP. If a quick landing is not possible, climb and maintain minimum FL160; FL200 is recommended.

Note: Smoke alert may be generated during smoke evacuation process.

AUX AFT COMPT SMK (depending on models)

AUX AFT COMPT AGENT ......................................................... DISCH

Model : 102-202-212-212A

1.07

72

EMERGENCY OCT 08 001

DUAL DC GEN LOSS

R R

DC GEN 1 + 2...................................................................OFF then ON

If no generator recovered LAND ASAP MAN RATE KNOB..........................................................9 O'CLOCK CAB PRESS MODE SEL...........................................................MAN AVIONICS VENT EXHAUST MODE...................................... OVBD BAT SW .................................................................................. OVRD CAPT EHSI................................................................................ OFF ATC (VHF 1 or HF or HF 2) ................................................. NOTIFY MIN CAB LIGHT ........................................................................ OFF Note: NAV lights switch set to ON is necessary to provide IEP

illumination STICK PUSHER / SHAKER ...................................................... OFF STICK PUSHER / SHAKER FAULT procedure (2.21) ..........APPLY SIDE WINDOWS ANTI-ICING................................................... OFF HF (If installed) .......................................................................... OFF ADC SW....................................................................SET TO ADC 1 ATC SW.................................................................... SET TO ATC 1 TLU ................................................................. MAN MODE LO SPD When TLU LO SPD illuminates TLU.....................................................................................AUTO

CAUTION: Avoid large rudder input if IAS above 180 kt MAIN BATTERY CHARGE (on LH maintenance panel) ......CHECK BUS EQUIPMENT LISTS.....................................................CHECK If STBY BUS UNDV light illuminates STBY BUS...............For approach, OVRD only when necessary Before descent PAX INSTRUCTIONS .................................................... USE PA HYD X FEED .......................................................................... ON

Note: Selecting HYD X FEED ON allows to recover green hydraulic system

At touch down IDLE GATE LEVER .............................................................PULL

1.07A

72


EMERGENCY DESCENT

OXYGEN MASKS / CREW COMMUNICATIONS ....................AS RQD GOOGLES................................................................................AS RQD DESCENT................................................................................INITIATE PL 1 + 2............................................................................................... FI CL 1 + 2 .............................................................................100% OVRD

OXYGEN PAX SUPPLY ...........................................................AS RQD SPEED........... MMO / VMO (or less if structural damage is suspected) SIGNS............................................................................................... ON ATC........................................................................................... NOTIFY MEA ...........................................................................................CHECK

Mod : 3973 or 4371 or 4457

1.08

72


DITCHING

Preparation (time permitting) ATC (VHF1 or HF or HF2) ................................................... NOTIFY CABIN CREW (PA).............................................................. NOTIFY SIGNS.......................................................................................... ON GPWS........................................................................................ OFF TERR (If Enhanced GPWS installed) ........................................ OFF CABIN AND COCKPIT .................................................... PREPARE

- Loose equipment secured - Survival equipment prepared - belts and shoulder harnesses locked

AUTO PRESS - LDG ELEVATION.............................................SET Approach

If ΔP≠0 AUTO PRESS.....................................................................DUMP PACKS 1 + 2.............................................................................. OFF OVBD VALVE ............................................................. FULL CLOSE FLAPS (If available).......................................................................30 LDG GEAR LEVER ......................................................................UP

30 seconds before impact or 1250 ft above sea level DITCH PB .................................................................................... ON ENG START ROTARY SELECTOR..............OFF / START ABORT CABIN REPORT............................................................. OBTAINED

Before ditching (200 ft) MINIMIZE IMPACT SLOPE OPTIMAL PITCH ATTITUDE FOR IMPACT ................................. 9° BRACE FOR IMPACT ..........................................................ORDER CL 1 + 2 .......................................................... FTR THEN FUEL SO FIRE HANDLES 1 + 2 ..............................................................PULL FUEL PUMPS 1 + 2................................................................... OFF

Note: In case of night ditching, shutting down both engines may be performed at captain discretion, immediately after the impact (avoiding loss of landing lights during flare out).

After ditching Note: After ditching, one aft door will be under the water line. CABIN CREW (PA).............................................................. NOTIFY EVACUATION ....................................................................INITIATE Before leaving aircraft BAT........................................................................................ OFF

1.08A

72


FORCED LANDING

Preparation (time permitting)

ATC (VHF1 or HF or HF2) ................................................... NOTIFY CABIN CREW (PA).............................................................. NOTIFY SIGNS.......................................................................................... ON GPWS........................................................................................ OFF TERR (If Enhanced GPWS installed) ........................................ OFF CABIN AND COCKPIT .................................................... PREPARE

- loose equipment secured - survival equipment prepared - belts and shoulder harnesses locked

AUTO PRESS - LDG ELEVATION.............................................SET

Approach FLAPS (If available).......................................................................30 LDG GEAR LEVER .............................................................AS RQD AUTO PRESS.........................................................................DUMP ENG START ROTARY SELECTOR..............OFF / START ABORT CABIN REPORT............................................................. OBTAINED

Before impact (200 ft) BRACE FOR IMPACT ..........................................................ORDER CL 1 + 2 .......................................................... FTR THEN FUEL SO FIRE HANDLES 1 + 2 ..............................................................PULL FUEL PUMPS 1 + 2................................................................... OFF

Note: In case of night forced landing, shutting down both engines may be performed at captain discretion, immediately after the impact (avoiding loss of landing lights during flare out).

After impact, when aircraft stopped CABIN CREW (PA).............................................................. NOTIFY AGENTS ................................................................................ DISCH EVACUATION ....................................................................INITIATE Before leaving aircraft BAT........................................................................................ OFF

1.0972

EMERGENCYSEP 04 001

SEVERE ICINGR

MINIMUM ICING SPEED ............................ INCREASE RED BUG by 10 ktPWR MGT .......................................................................................... MCTCL / PL ................................................................................... 100% / MCTAP (if engaged).......FIRMLY HOLD CONTROL WHEEL and DISENGAGESEVERE ICING CONDITIONS .....................................................ESCAPEATC...............................................................................................NOTIFY

n If an unusual roll response or uncommanded roll controlmovement is observed :

Push firmly on the control wheel FLAPS ..................................................................................... 15

n If the flaps are extended, do not retract them until the airframe isclear of ice.

n If the aircraft is not clear of ice :GPWS..........................................................FLAP/GPWS OVRDSTEEP SLOPE APPROACH (≥4.5°).......................PROHIBITEDAPP/LDG CONF.........................................MAINTAIN FLAPS 15

with "REDUCED FLAPS APP/LDG icing speeds" + 5 ktMultiply landing distance FLAPS 30 by 1.91.

DETECTIONVisual cue identifying severe icing is characterized by ice covering all or asubstantial part of the unheated portion of either side window

and / orUnexpected decrease in speed or rate of climb

and / orThe following secondary indications :. Water splashing and streaming on the windshield. Unusually extensive ice accreted on the airframe in areas not normally

observed to collect ice. Accumulation of ice on the lower surface of the wing aft of the protected

areas. Accumulation of ice on propeller spinner farther aft than normally

observed

The following weather conditions may be conducive to severe in-flighticing :. Visible rain at temperatures close to 0°C ambient air temperature (SAT). Droplets that splash or splatter on impact at temperatures close to 0°C

ambient air temperature (SAT)

Eng : PW124

FOLL

OW

ING

PR

OC

ED

UR

ES

2.0172

FOLLOWING FAILURESSEP 10 001

2 - PROCEDURES FOLLOWING FAILURESContent 1/3

POWER PLANTSINGLE ENG OPERATION………………………………………………………. 2.04START FAULT……………………………………………………………………... 2.04X START FAIL……………………………………………………………………… 2.04ABNORMAL PARAMETERS DURING START………………………………… 2.05EXCESSIVE ITT DURING START………………………………………………. 2.05NO ITT DURING START………………………………………………………….. 2.05NO NH DURING START………………………………………………………….. 2.05

R ENG NAC OVHT 2.06ABNORMAL ENG PARAMETERS IN FLIGHT………………………………… 2.06FIRE LOOP FAULT……………………………………………………………….. 2.06ABNORMAL PROP BRK…………………………………………………………. 2.07ENG RESTART IN FLIGHT………………………………………………………. 2.08ENG STALL………………………………………………………………………… 2.08ONE EEC FAULT………………………………………………………………….. 2.09BOTH EEC FAULT………………………………………………………………… 2.09ENG FLAME OUT…………………………………………………………………. 2.10IDLE GATE FAIL…………………………………………………………………… 2.10SYNPHR FAIL (if applicable) ……………………………………………………. 2.10ACL PNEUMATIC ACTUATOR BLOCKING (if applicable) ……………………. 2.10A

R UNCOMMANDED 100% NP ON ONE OR TWO PROPELLERS (if applicable) …………… 2.10APEC SGL CH (if applicable) ……………………………………………………… 2.10APEC FAULT (if applicable) ……………………………………………………….. 2.10ALO PITCH IN FLIGHT……………………………………………………………... 2.11ENG OVER LIMIT…………………………………………………………………. 2.11PROP OVER LIMIT……………………………………………………………….. 2.11ENG OIL TEMP BELOW 45°C…………………………………………………… 2.12ENG OIL TEMP HIGH…………………………………………………………….. 2.12ENG OIL LO PR……………………………………………………………………. 2.12ENG BOOST FAULT (if applicable) …………………………………………….. 2.12A

FUELFUEL ABNORMAL TEMP………………………………………………………… 2.13FUEL CLOG………………………………………………………………………… 2.13FEED LO PR……………………………………………………………………….. 2.13FUEL LEAK ALERT CONDITION……………………………………………….. 2.14FUEL LO LVL………………………………………………………………………. 2.14FUEL LEAK………………………………………………………………………… 2.14

ELECDC BUS 1 OFF ……………………………………………………………………. 2.15AC BUS 1 OFF ……………………………………………………………………. 2.15DC BUS 2 OFF ……………………………………………………………………. 2.15AAC BUS 2 OFF ……………………………………………………………………. 2.15AACW BUS 1 OFF / ACW BUS 2 OFF…………………………………………… 2.16ACW TOTAL LOSS……………………………………………………………….. 2.16ADC ESS BUS OFF………………………………………………………………… 2.17DC EMER BUS OFF………………………………………………………………. 2.17DC GEN FAULT……………………………………………………………………. 2.18INV FAULT…………………………………………………………………………. 2.18ACW GEN FAULT…………………………………………………………………. 2.18DC SVCE/UTLY BUS SHED……………………………………………………… 2.18BAT CHG FAULT………………………………………………………………….. 2.18DUAL BAT CHG LOSS……………………………………………………………. 2.18BAT DISCHARGE IN FLIGHT (if applicable) …………………………………... 2.18

STBY BUSSES AND BAT ONLY LOST EQUIPMENT LISTS………………...2.18A2.18B

ESS BUS AND EMER BUS LOST EQUIPMENT LISTS……………………….Cargo configuration only…..

2.422.42A

2.02

72

FOLLOWING FAILURES OCT 08 001

2 - PROCEDURES FOLLOWING FAILURES Content 2/3 HYDRAULIC HYD LO LVL 2.19 BOTH MAIN HYD PUMPS LOSS 2.19 BOTH HYD SYS LOSS 2.20 HYD LO PR / HYD OVHT 2.20 FLIGHT CONTROL FLAPS UNLK 2.21 FLAPS JAM / UNCOUPLED / ASYM 2.21 REDUCED FLAPS LANDING 2.21

R STICK PUSHER / SHAKER FAULT 2.21 PITCH TRIM ASYM (LOCAL LIGHT) 2.22 PITCH TRIM INOPERATIVE 2.22 RUDDER RELEASABLE CENTER UNIT FAIL 2.22 PITCH DISCONNECT 2.22

R PITCH RECONNECTION ON GROUND (If applicable) 2.22A TLU FAULT 2.22A AIL LOCK LIT (if applicable) 2.22A ELEVATOR JAM 2.23 AILERON JAM / SPOILER JAM 2.23 RUDDER JAM 2.23 LANDING GEAR LDG GEAR GRAVITY EXTENSION 2.24 LANDING WITH ABNORMAL LDG GEAR 2.24 LDG GEAR UNSAFE INDICATION 2.25 LDG GEAR RETRACTION IMPOSSIBLE 2.25 ANTI-SKID FAULT 2.25 BRK TEMP HOT 2.25 AIR BLEED VALVE FAULT 2.26 BLEED OVHT 2.26 BLEED LEAK 2.26 X VALVE OPEN 2.26 PACK VALVE FAULT 2.26 BOTH PACK VALVES FAULT 2.26 RECIRC FAN FAULT 2.26 DUCT OVHT 2.26A EXCESS CAB ALT 2.26A AUTO PRESS FAULT 2.26A

R EXCESS CAB ΔP 2.26A AVIONICS VENT EXHAUST MODE FAULT 2.27 OVBD VALVE FAULT 2.27

2.03

72

FOLLOWING FAILURES SEP 10 001

2 - PROCEDURES FOLLOWING FAILURES Content 3/3 ANTI ICE AFR AIR BLEED FAULT …………………………………………………………. 2.28 DE-ICING AIR FRAME FAULT ………………………………………………….. 2.28 DE-ICING MODE SEL FAULT …………………………………………………… 2.28 MODE SEL AUTO FAULT (if applicable) ………………………………………. 2.28 ICE DETECT FAULT ……………………………………………………………… 2.29 DE- / ANTI-ICING ENG FAULT …………………………………………………. 2.29 ANTI-ICING PROP FAULT ………………………………………………………. 2.29 ANTI-ICING HORNS FAULT …………………………………………………….. 2.29 SIDE WINDOW / WINDSHIELD HTG FAULT …………………………………. 2.29 PROBES HTG FAULT ……………………………………………………………. 2.29 AUTO PILOT

AILERON MISTRIM (ADU message)

or EXCESSIVE LATERAL TRIM REQUIRED ………………………………….. or ABNORMAL FLIGHT CHARACTERISTICS

2.30

PITCH MISTRIM (ADU message) ………………………………………………. 2.30 PITCH TRIM FAIL (ADU message) (if applicable) …………………………….. 2.30 DADC DATA INVALID (ADU message) ………………………………………… 2.30 MPC APM FAULT ……………………………………………………………………….. 2.30A DEGRADED PERF ……………………………………………………………….. 2.30A INCREASE SPEED ………………………………………………………………. 2.30A AVIONICS AUDIO SEL FAULT ……………………………………………………………….. 2.31 AHRS A / ERECT FAIL …………………………………………………………… 2.31 EFIS COMP ………………………………………………………………………... 2.31 ADC SW FAULT …………………………………………………………………... 2.31 ADU FAILURE …………………………………………………………………….. 2.32 ADC FAULT ……………………………………………………………………….. 2.32 AHRS FAIL ………………………………………………………………………… 2.32 SGU FAIL ………………………………………………………………………….. 2.32 CRT FAIL ………………………………………………………………………….. 2.32 MISCELLANEOUS COCKPIT DOOR CONTROL PANEL FAULT (if installed) …………………… 2.32A VOLCANIC ASH ENCOUNTER………………… ………………………………. 2.32A LOSS OF RADIO ALTIMETER INFORMATION ………………………………. 2.33

R SMK DET FANS FAULT …………………………………………………………. 2.33 DOORS UNLK IN FLIGHT ………………………………………………………. 2.33 COCKPIT WINDOW CRACKED ………………………………………………… 2.33 OXYGEN LO PR ………………………………………………………………….. 2.33 MFC MFC 1A FAULT …………………………………………………………………… 2.34 MFC 1B FAULT …………………………………………………………………… 2.34 MFC 2A FAULT …………………………………………………………………… 2.35 MFC 2B FAULT …………………………………………………………………… 2.35 MFC 1A + 1B FAULT ……………………………………………………………... 2.36 MFC 1A + 2A FAULT ……………………………………………………………... 2.37 MFC 1A + 2B FAULT ……………………………………………………………... 2.38 MFC 1B + 2A FAULT ……………………………………………………………... 2.39 MFC 2A + 2B FAULT ……………………………………………………………... 2.40 MFC 1B + 2B FAULT ……………………………………………………………... 2.41

ELEC Section for EMER & ESS BUS lost equipment lists…………….………

Cargo configuration only…… 2.42 2.42A

2.04

72

FOLLOWING FAILURES POWER PLANT

APR 08 500

SINGLE ENG OPERATION

LAND ASAP PWR MGT 1 + 2 .......................................... TO if necessary then MCT FUEL PUMP affected side.............................................................. OFF DC GEN affected side .................................................................... OFF ACW GEN affected side ................................................................. OFF PACK affected side......................................................................... OFF BLEED affected side....................................................................... OFF TCAS (if installed) ................................................................... TA ONLY OIL PRESSURE ON FAILED ENGINE .................................MONITOR Note: In icing conditions, FLAPS 15 will be selected to improve drift down

performances and single engine ceiling. Note: Refer to pages (4.61) and (4.62) to determine single engine gross

ceiling. Note: If during the flight, a positive oil pressure has been noted on the

failed engine for a noticeable period of time, maintenance must be informed.

Note: monitor fuel balance. Recommended operational maximum fuel unbalance is 200 kg (440 lb).

When FUEL CROSS FEED is required FUEL PUMP affected side........................................................... ON FUEL X FEED.............................................................................. ON FUEL PUMP operating engine .................................................. OFF

For approach MAX APPROACH SLOPE for Steep Slope Approach ............... 5.5° BLEED NOT AFFECTED .......................................................... OFF CL live engine...............................................................100% OVRD

APPROACH SPEED ........................... NOT LESS THAN 1.1VMCA Note: Refer to page (4.64) to determine 1.1VMCA.

Note: At touch down, do not reduce below FI before nose wheel is on the ground.

START FAULT

ENG START ROTARY SELECTOR...................OFF / START ABORT

If above 45 % NH START ON LIGHT....................................CHECK EXTINGUISHED START ............................................................. TO BE CONTINUED

X START FAIL

CONTINUE NORMAL ENGINE START INFORM MAINTENANCE

Mod : 3973 or 4371 or 4457

2.0572

FOLLOWING FAILURESPOWER PLANT

OCT 08 001

ABNORMAL PARAMETERSDURING START

If ITT tends to exceed 900°C, or no ITT, or no NHCL affected side ................................................................ FUEL SOENG START ROTARY SELECTOR..............OFF / START ABORT

Then refer to relevant procedure:

EXCESSIVE ITT DURING START procedure (2.05)

NO ITT DURING START procedure (2.05)

NO NH DURING START procedure (2.05)

EXCESSIVE ITT DURING START

When NH below 30 %ENG START ROTARY SELECTOR.....................................CRANKSTART PB ................................................................................... ON

After 15 secondsENG START ROTARY SELECTOR ........OFF / START ABORT

CAUTION: If ITT exceeds 950°C, maintenance action is due.

Note: BLEED VALVE may be selected OFF in order to reduce ITT.

NO ITT DURING START

After 30 seconds, to allow fuel drainingENG START ROTARY SELECTOR.....................................CRANKSTART PB ................................................................................... ON

After 15 secondsENG START ROTARY SELECTOR ........OFF / START ABORT

NO NH DURING START

R

Note: On BAT only, OIL PRESS IND is not available.

ENG START ROTARY SELECTOR...................START A or START B

START PB ........................................................................................ ON

After 10 seconds

If OIL pressure increasesCL ..........................................................................................FTRContinue START procedure, being informed NH indicator isinoperative.

If OIL pressure does not increasesENG START ROTARY SELECTOR ........OFF / START ABORTSuspect starter motor failure. Maintenance action is due.

2.0672


SEP 10 001

R ENG NAC OVHT

RR

R

RR

If during Hotel mode operationPL affected side .............................................................................GICL affected side.............................................. FTR THEN FUEL SO

If during taxiAIRCRAFT...............................................................................STOPPL affected side .............................SLIGHTLY INCREASE POWER

If unsuccessful within 30 secondsPL affected side........................................................................GICL affected side......................................... FTR THEN FUEL SO

ABNORMAL ENG PARAMETERSIN FLIGHT

RRRRRRRRRR

If Intermittent fluctuations or unrealistic steady indicationATPCS....................................................................................... OFF

When adequate flight situationPL affected side…………………………………………………… FIEEC affected side................................................................. OFF If successful

ONE EEC FAULT procedure (2.09) ..............................APPLY If unsuccessful- or - If TQ = 0% and NP<77%

PL affected side..................................................................... FICL affected side......................................................... FUEL SOSINGLE ENG OPERATION procedure (2.04) ..............APPLY

If "- - -" indication on torque digital counter (only for PW127 -PW127F - PW127M)

AVOID SUDDEN PL MOVEMENTS

FIRE LOOP FAULT

LOOP affected ................................................................................ OFF

2.07

72


APR 08 001

ABNORMAL PROP BRK (if applicable)

If on ground

If unexpected propeller rotation – or – If local UNLK and CCAS PROP BRK alert CL 2 .............................................................................. FUEL SO MAINTENANCE ACTION REQUIRED

If CCAS PROP BRK alert only If GUST LOCK ON CL 2 ......................................................................... FUEL SO If DC and AC GPU are not available ENG 1.....................................................................START CL 1..........................................................................AUTO When READY light illuminates PROP BRK................................................................. OFF UNLK LIGHT .............................CHECK EXTINGUISHED PROP BRK PWR SPLY C/B .....................................PULL If GUST LOCK OFF GUST LOCK...................................................................... ON According to operational situation PROP BRK................................................................. OFF ALL PROP BRK LIGHTS ..........CHECK EXTINGUISHED

If in flight CONTINUE NORMAL OPERATION ENG 2 PARAMETERS .....................................................MONITOR After landing CL 2 .............................................................................. FUEL SO MAINTENANCE ACTION REQUIRED

2.08

72


APR 08 500

ENG RESTART IN FLIGHT

FUEL SUPPLY...........................................................................CHECK CL ........................................................................................... FUEL SO PL........................................................................................................ FI CAUTION: After ATPCS sequence, PWR MGT rotary selector must

be set to MCT position before engine restart, in order to cancel propeller feathering.

ENG START ROTARY SELECTOR................................ START A & B EEC PB............. RESET if necessary or DESELECT if FAULT persists START PB ........................................................................................ ON

At 10 % NH CL ...............................................................................................FTR RELIGHT ..........................................................................MONITOR CL ............................................................................................AUTO PL......................................................ADJUST TO OTHER ENGINE ENG START ROTARY SELECTOR....................................AS RQD SYSTEMS AFFECTED.................................................... RESTORE

ENG STALL

PL affected side .................................................................................. FI ENG PARAMETERS .................................................................CHECK

If abnormal engine parameters CL affected side.............................................. FTR THEN FUEL SO SINGLE ENG OPERATION procedure (2.04).......................APPLY

If normal engine parameters DE-/ANTI-ICING ENG ................................................................. ON PL affected side ...............................................SLOWLY ADVANCE If stall recurs Reduce thrust and operate below the stall threshold If stall does not recur Continue engine operation

Mod : 3973 or 4371 or 4457

2.0972


SEP 10 500

ONE EEC FAULT

RR

ATPCS ............................................................................................ OFF

CAUTION: DO NOT DESELECT EEC FLASHING

When adequate flight situationPL affected side ............................... RETARD IN GREEN SECTOREEC affected side ..................................................................RESET

If successfulATPCS.................................................................................... ONPL affected side........................................... RESTORE POWER

If unsuccessfulEEC affected side................................................................. OFFPL affected side .......................................... RESTORE POWER......................................... HANDLING THROTTLE WITH CARE

In the following cases: icing conditions, engine(s) flame out,emergency descent, severe turbulence, heavy rainMAN IGN ........................................................................... ON

In final approachCL 1 + 2 ..............................................................100% OVRD

After landingTAXI WITH THE AFFECTED ENGINE FEATHEREDNote: ACW BTC must be check closed in order to avoid the lossof ACW bus on ground

BOTH EEC FAULT

ATPCS ............................................................................................ OFF

CAUTION: DO NOT DESELECT EEC FLASHING

When adequate flight situationPL 1 + 2 ........................................... RETARD IN GREEN SECTOREEC 1 + 2 ................................................................. OFF THEN ON

If EEC 1+2 recoveredATPCS.................................................................................... ONPL 1 + 2 ....................................................... RESTORE POWER

If only one EEC recoveredONE EEC FAULT procedure (2.09) .................................APPLY

If no EEC recoveredEEC 1 + 2 ............................................................................. OFFPL 1 + 2 ....................................................... RESTORE POWER....................................... HANDLING THROTTLES WITH CARETQ IND ENG 1 + 2.......................................................MONITORLDG DIST ....................................................... MULTIPLY BY 1.5Note: Refer to Part 4 to determine landing distance

In the following cases: icing conditions, engine(s) flame out,emergency descent, severe turbulence, heavy rainMAN IGN ........................................................................... ON

In final approachCL 1 + 2 ..............................................................100% OVRD

After landingBRAKE HANDLE........................................... EMER AS RQDCAUTION: Reverse power is reduced.Both main HYD pumps will be lost at low speed.TAXI ON BOTH ENGINES,HANDLE THROTTLES WITH CARE

Mod : 3973 or 4371 or 4457

2.10

72


APR 08 050

ENG FLAME OUT

PL affected side .................................................................................. FI

If NH drops below 30 % (no immediate relight) CL affected side.............................................. FTR THEN FUEL SO If damage suspected FIRE HANDLE affected side ...............................................PULL SINGLE ENG OPERATION procedure (2.04)..................APPLY If no damage suspected ENG RESTART IN FLIGHT procedure (2.08)..................APPLY If unsuccessful SINGLE ENG OPERATION procedure (2.04) ............APPLY

IDLE GATE FAIL

In flight IDLE GATE LEVER .................................................................PUSH

At touch down IDLE GATE LEVER ..................................................................PULL

Mod : 4111

2.10A

72


SEP 10 500

R

R

UNCOMMANDED 100% NP ON ONE OR

TWO PROPELLERS

RR

CL 1 + 2 .............................................................................100% OVRD

PEC SGL CH

DO NOT RESET PEC IN FLIGHT - NO SPECIAL CREW ACTION ANTICIPATE A PEC FAULT AT LANDING MAINTENANCE IS REQUIRED

PEC FAULT

� If in short final approach (below 400 ft RA) GO AROUND procedure .......................................................APPLY

� Above 400 ft or when adequate CL affected side............................................................100% OVRD PEC affected side ..................................................................RESET � If successful CL affected side..................................................................AUTO � If unsuccessful PEC affected side................................................................. OFF Avoid sudden PL movements � Before landing CL NON AFFECTED..........................................100% OVRD Reverse is not available on affected side. TAXI ON BOTH ENGINES Note: ACW BTC may be check closed in order to avoid the loss of ACW bus on ground

Mod : 3973 or 4371 or 4457

2.11

72


SEP 10 030

LO PITCH IN FLIGHT

PL affected side .................................................................................. FI CL affected side ................................................... FTR THEN FUEL SO SINGLE ENG OPERATION procedure (2.04) ............................APPLY

ENG OVER LIMIT

PL affected side .............. RETARD TO RESTORE NORMAL VALUES

Note: BLEED VALVE may be selected OFF in order to reduce ITT

� If TQ, NH, and/or ITT still over limit and if conditions permit PL affected side ............................................................................. FI CL affected side.............................................. FTR THEN FUEL SO SINGLE ENG OPERATION procedure (2.04).......................APPLY

PROP OVER LIMIT

R R R R R R

PL affected side .......................... RETARD TO SET NP BELOW 101% PEC affected side .............................................................OFF then ON PL affected side .......................................................................AS RQD Note: If conditions do not permit engine shut down, 110% is allowed to

complete the flight. An engine removal has to be done for maintenance action on arrival.

� If NP decreases below 101% CONTINUE NORMAL FLIGHT � If NP remains above 101% and conditions permit PL affected side ............................................................................. FI CL affected side.............................................. FTR THEN FUEL SO SINGLE ENG OPERATION procedure (2.04).......................APPLY

Mod : 4371 Eng : PW124

2.12

72


OCT 08 050

ENG OIL TEMP BELOW 45°C

If icing conditions are expected or present

ENG POWER ...............................................If possible, INCREASE

ENG OIL TEMP HIGH

OIL TEMP between 115°C and 125°C

OIL TEMP AND PRESS ...................................................MONITOR Note: If OIL temperature rise follows PL reduction, advancing PL

may reduce OIL temperature. Note: If OIL temperature rise occurs in steady state conditions, a

power reduction should permit a reduction in OIL temperature.

OIL TEMP between 115°C and 125°C for more than 20 minutes PL affected side ...........RETARD TO SET minimum possible power

CAUTION: Flight plan must be rescheduled to minimize engine operating time in these abnormal conditions.

OIL TEMP above 125°C PL affected side ............................................................................. FI CL affected side.............................................. FTR THEN FUEL SO SINGLE ENG OPERATION procedure (2.04).......................APPLY

ENG OIL LO PR

R

PL affected side .................................................................................. FI

If both OIL LO PR on CAP and local alert are activated CL affected side.............................................. FTR THEN FUEL SO SINGLE ENG OPERATION procedure (2.04).......................APPLY

If local alert only is activated CL affected side.............................................. FTR THEN FUEL SO Once engine is shut off CL affected side..........................................................................FTR If CCAS is activated after 30 seconds CL affected side............................................................ FUEL SO ENG RESTART IN FLIGHT procedure (2.08)..................APPLY If not CL affected side ............................................................ FUEL SO SINGLE ENG OPERATION procedure (2.04)..................APPLY

If OIL LO PR alert on CAP only is activated DISREGARD INFORM MAINTENANCE

If single engine operation required NP of feathered engine.....................................................MONITOR If NP of feathered engine above 10% IAS ...................................... LIMIT NOT TO EXCEED NP 101% APPROACH SPEED .................................INCREASE BY 10 KT

Mod : 4111 Eng : PW124

2.13

72

FOLLOWING FAILURES FUEL

APR 08 001

FUEL ABNORMAL TEMP

If too high (>50°C)

Note: Avoid rapid throttle movement OIL TEMP AND OTHER ENGINES PARAMETERS .......MONITOR

If too low (<0°C) Note: Use anti-icing additive for next refueling if repair can't be done

FUEL CLOG

If both lights are illuminated

ENGINES PARAMETERS................................................MONITOR If abnormal engines parameters

LAND ASAP Note: Fuel contamination may be suspected

MAINTENANCE ACTION REQUIRED

If only one light is illuminated ENGINE PARAMETERS affected side.............................MONITOR

FEED LO PR

PUMP affected side ........................................................ CONFIRM ON ENGINE affected side...........MONITOR FOR POSSIBLE RUN DOWN

If engine runs down or if fuel quantity decreases significantly PL affected side ............................................................................. FI CL affected side.............................................. FTR THEN FUEL SO PUMP affected side ................................................................... OFF FIRE HANDLE affected side ....................................................PULL SINGLE ENG OPERATION procedure (2.04).......................APPLY CAUTION: Do not open X FEED valve

2.14

72

FOLLOWING FAILURES FUEL

APR 08 001

FUEL LEAK ALERT CONDITION

A fuel leak may be detected by either: - sum of fuel on board (FOB), read in steady flight at cruise level, and

fuel used (FU), FOB+FU significantly less than fuel at departure, or - total fuel quantity decreasing (fuel spray from engine or wing tip), or - fuel imbalance, or - a tank emptying too fast (leak from engine or a hole in a tank), or - excessive fuel flow (leak from engine), or - fuel smell in the cabin

FUEL LO LVL

AVOID EXCESSIVE AIRCRAFT ATTITUDES If both LO LVL lights ON

LAND ASAP If LO LVL light on one side only

FUEL LEAK procedure (2.14)................................................APPLY

FUEL LEAK

When a leak is confirmed

LAND ASAP Leak from engine (excessive fuel flow or feed spray from engine) PL affected side........................................................................ FI CL affected side......................................... FTR THEN FUEL SO PUMP affected side.............................................................. OFF FIRE HANDLE affected side ...............................................PULL SINGLE ENG OPERATION procedure (2.04)..................APPLY If excessive fuel flow was identified before engine shutdown FUEL X FEED valve can be opened In all other cases X FEED valve must remain closed Leak not located FUEL X FEED............................................. MAINTAIN CLOSED

Note: the X FEED must remain closed to prevent the leak affecting both sides.

Before landing ATC................................................................................. NOTIFY

2.15

72

FOLLOWING FAILURES ELEC

OCT 08 001

DC BUS 1 OFF

DC GEN 1 ....................................................................................... OFF PF....................................................................................................CM2 MAN RATE KNOB ...............................................................9 O'CLOCK CAB PRESS MODE SEL................................................................MAN DC SVCE/UTLY BUS PB................................................MAINTAIN ON AFFECTED EQUIPMENT .............................................................. OFF DC BUS 1 LOST EQUIPMENT LIST.........................................CHECK

At touch down IDLE GATE LEVER ..................................................................PULL

DC BUS 1 LOST EQUIPMENT LIST

R R

DUCT/COMPT TEMP IND Recirculation Fan #1 AFCS Computer (in flight) Spoilers IND Stick Pusher PWR and CTL CM1 Stick Shaker CAPT and STBY Static Ports LH Side Window Anti-Icing LH Windshield HTG IND Weather Radar / Radio Altimeter

GPWS / G/S IND CM1 EHSI, DME #1 BLEED HP Valve #1 and LEAK IND BLEED X FEED Valve and IND AUTO PRESS Syncrophaser (if applicable) AUTO IDLE GATE Fuel Tank TEMP IND CM1 FF/FU IND CM1 Fuel TEMP and CLOG IND CM1 Oil PRESS and TEMP IND

R

AC BUS 1 OFF

Note: Wait for 10 seconds in order to confirm the failure. DC BTC......................................................................... ISOL THEN ON

If unsuccessful AC BUS 1 LOST EQUIPMENT LIST....................................CHECK

AC BUS 1 LOST EQUIPMENT LIST

R TRIMS IND

BLEED LEAK DET Weather Radar

For more information on BUS EQUIPMENT LISTS see FCOM 1.06.60

2.15A

72


OCT 08 100

DC BUS 2 OFF

DC GEN 2 ....................................................................................... OFF PF....................................................................................................CM1 ADC SW.........................................................................SET TO ADC 1 VHF 1 / ATC 1...........................................................................SELECT AFFECTED EQUIPMENT .............................................................. OFF DC BUS 2 EQUIPMENT LIST ...................................................CHECK

Before descent PAX INSTRUCTIONS.......................................................... USE PA

After touch down TAXI ON BOTH ENGINES

DC BUS 2 LOST EQUIPMENT LIST

R

R

Recirculation Fan #2 AFCS ADU VHF and ATC #2 CM2 Stick Shaker DC AUX HYD Pump CM2 Static Ports, Wiper, Probes IND RH Side Window Anti-Icing RH Windshield HTG IND CM2 Clock

LIGHTS: TAXI / TO / WINGS PAX SIGNS CM2 ADC, EADI, EHSI and SGU ADF, DME and VOR/ILS #2 CM1 RMI BLEED HP Valve #2 DOORS: ALERTS IDLE GATE FAIL IND CM2 FF/FU IND CM2 Fuel TEMP and CLOG IND CM2 Oil PRESS and TEMP IND

R R

AC BUS 2 OFF

Note: Wait for 10 seconds in order to confirm the failure. DC BTC......................................................................... ISOL THEN ON

If unsuccessful PF ..............................................................................................CM1 AC BUS 2 EQUIPMENT LIST ..............................................CHECK

AC BUS 2 LOST EQUIPMENT LIST

R CM2 ASI/VSI/ALTI ADF, ADC OUTPUT #2

GPWS CM1 RMI R


Mod : 4116

2.16

72


OCT 08 001

ACW BUS 1 OFF / ACW BUS 2 OFF

R

ACW GEN affected side ................................................................. OFF LEAVE AND AVOID ICING CONDITIONS AS LONG AS ICING CONDITIONS EXIST ICE ACCRETION ..................................... VISUALLY MONITOR

If ACW BUS 1 OFF PF ..............................................................................................CM2 CM1 AIRSPEED INDICATOR ..........................................MONITOR

If ACW BUS 2 OFF PF ..............................................................................................CM1 CM2 AIRSPEED INDICATOR ..........................................MONITOR AFFECTED EQUIPMENT .............................................................. OFF HYD X FEED .................................................................................... ON ACW BUS 1 or 2 LOST EQUIPMENT LIST ..............................CHECK

If any IAS discrepancy occurs DADC DATA INVALID (ADU message) procedure (2.30) ....APPLY

After touch down TAXI ON BOTH ENGINES

ACW BUS 1 LOST EQUIPMENT LIST

R R

BLUE PUMP PWR CAPT PITOT / ALPHA / TAT ANTI-ICING PROP 1 ANTI-ICING HORNS (LH ELEV, RUD)

LH WINDSHIELD HTG LEFT LDG LIGHT PWR LEFT and REAR STROBES

R

ACW BUS 2 LOST EQUIPMENT LIST

R

GREEN PUMP PWR F/O PITOT / ALPHA / TAT ICE DET ANTI-ICING PROP 2

ANTI-ICING HORNS (RH ELEV, AIL) RH WINDSHIELD HTG TAXI and T/O LIGHTS PWR RIGHT LDG LIGHT PWR RIGHT STROBE

R R

2.16A

72


OCT 08 001

ACW TOTAL LOSS

ACW GEN 1 + 2.............................................................................. OFF HYD X FEED .....................................................................CHECK OFF LEAVE AND AVOID ICING CONDITIONS AS LONG AS ICING CONDITIONS EXIST ICE ACCRETION........................................... VISUALLY MONITOR CM1 and CM2 AIRSPEED INDICATORS........................MONITOR ACW TOTAL LOSS EQUIPMENT LIST ....................................CHECK AFFECTED EQUIPMENT .............................................................. OFF MAIN HYD PUMPS......................................................................... OFF LDG GEAR EXTENSION/RETRACTION..................................... LOST NORMAL BRAKE ......................................................................... LOST LDG DIST .................................................................MULTIPLY BY 1.5 Note: Refer to Part 4 to determine LDG DIST

Before landing LDG GEAR LEVER ............................................................... DOWN BLUE PRESSURE................................................................CHECK FLAPS..................................................................................AS RQD LDG GEAR GRAVITY EXTENSION procedure (2.24)..........APPLY

After touch down REVERSE............................................................................AS RQD BRAKE HANDLE..................................................... EMER AS RQD TAXI ON BOTH ENGINES

ACW TOTAL LOST EQUIPMENT LIST

R

BLUE and GREEN PUMP PWR CAPT and F/O PITOT / ALPHA / TAT ICE DET ANTI-ICING PROP 1 + 2

ANTI-ICING HORNS LH and RH WINDSHIELD HTG TAXI and T/O LIGHTS PWR LEFT and RIGHT LDG LIGHTS PWR LEFT, RIGHT and REAR STROBES

R R


2.1772

FOLLOWING FAILURESELEC

OCT 08 001

DC ESS BUS OFF

DC ESS BUS EQUIPMENT LIST ..............................................CHECK

If Cockpit Securized Door installedCOCKPIT DOOR MANUAL LOCK BOLT(S).....................................

.......................................................... MOVE TO CLOSE POSITION

Note: Cockpit Door Control Panel FAULT LIGHT is inoperative.

Note: When the door is locked with the manual bolt(s), theemergency access to the cockpit is unavailable. It isrecommended that at least two crewmembers remain in thecockpit during that time.

DC ESS BUS LOST EQUIPMENT LIST

RR

See QRH pages 2.42 (all configuration)and 2.42A (for cargo configuration only)

DC EMER BUS OFF

RR

LEAVE AND AVOID ICING CONDITIONSDESCEND TOWARD ........................................................FL100 / MEASTBY PITCH TRIM.......................................................... USE AS RQDADC SW (ADC FAULT lights lost) .................................SET TO ADC 2HYD X FEED .................................................................................... ON If ice accretion builds up on airframe

DE-ICING MODE SEL FAULT procedure (2.28)...................APPLYANTI-ICING PROP FAULT procedure (2.29) ........................APPLYANTI-ICING HORNS FAULT procedure (2.29) .....................APPLYCM1 and STBY IAS ............................................COMPARE to CM2Note: Use CM2 instruments in case of disagreement.

Before landingANTI-SKID ................................................................................. OFFN/W STEERING ........................................................................ OFFANTI-SKID FAULT procedure (2.25).....................................APPLY

DC EMER BUS OFF LOST EQUIPMENT LIST

RSee QRH pages 2.42 (all configuration)and 2.42A (for cargo configuration only)


2.18

72


OCT 08 500

DC GEN FAULT

DC GEN affected side..................................................................... OFF If OAT exceeds ISA + 25

FL........................................................................................200 MAX TAXI ON BOTH ENGINES

INV FAULT

NO SPECIFIC ACTION IN FLIGHT

ACW GEN FAULT

ACW GEN affected side ................................................................. OFF LEAVE AND AVOID ICING CONDITIONS TAXI ON BOTH ENGINES

DC SVCE/UTLY BUS SHED

DC SVCE/UTLY BUS PB..........................................................AS RQD

DC SVCE/UTLY BUS SHED LOST EQUIPMENT LIST

R See FCOM 1.06.60 pages 12 to 14

BAT CHG FAULT

CHG associated.............................................................................. OFF

DUAL BAT CHG LOSS

MFC MODULES, one at a time ....................................... OFF / RESET If RESET unsuccessful

LAND ASAP Note: minimize use of VHF 1 if conditions permit.

BAT DISCHARGE IN FLIGHT

ENG START ROTARY SELECTOR............................................... OFF

If battery(ies) still discharging LAND ASAP

Mod : 3246 + 4111

2.18A

72


APR 08 500

STBY BUS AND BAT ONLY LOST EQUIPMENT LISTS

Mod : 4116

2.18B

72


APR 08 500

STBY BUS AND BAT ONLY LOST EQUIPMENT LISTS

Mod : 4116

2.19

72

FOLLOWING FAILURES HYDRAULIC

OCT 08 001

HYD LO LVL

If blue system affected BLUE PUMP .............................................................................. OFF AUX PUMP ....................................................... OFF (CONFIRMED) REDUCED FLAPS LANDING procedure (2.21)....................APPLY After touch down USE NORMAL BRAKE FOR STEERING TAXI ON BOTH ENGINES

If green system affected GREEN PUMP........................................................................... OFF LDG DIST ............................................................ MULTIPLY BY 1.5 Note: Refer to Part 4 to determine landing distance LDG GRAVITY EXTENSION procedure (2.24) .....................APPLY After touch down TAXI ON BOTH ENGINES REVERSE.......................................................................AS RQD BRK HANDLE..................................................... EMER AS RQD

HYD SYS LOST EQUIPMENT LIST

BLUE GREEN

FLAPS / SPOILERS / N/W STEERING PROP BRK (if applicable) EMER AND PARKING BRK (on accu only)

LDG GEAR EXT / RET NORM BRK

BOTH MAIN HYD PUMPS LOSS

MAIN BLUE AND GREEN PUMPS ................................................ OFF X FEED ..............................................................................CHECK OFF LDG DIST .................................................................MULTIPLY BY 1.5 Note: Refer to Part 4 to determine landing distance

Before landing LDG GEAR LEVER ............................................................... DOWN BLUE PRESSURE................................................................CHECK FLAPS 15 ............................................................................AS RQD LDG GEAR GRAVITY EXTENSION procedure (2.24)..........APPLY FLAPS 30 ............................................................................AS RQD

After touch down TAXI ON BOTH ENGINES REVERSE............................................................................AS RQD BRK HANDLE.......................................................... EMER AS RQD

BOTH MAIN HYD PUMPS LOST EQUIPMENT LIST

R R

BLUE

recovered when LDG GEAR lever is DOWN

GREEN

R R R



2.20

72

FOLLOWING FAILURES HYDRAULIC

OCT 08 050

BOTH HYD SYS LOSS

R

RRR

MAIN AND AUX PUMPS ................................................................ OFF

� Before approach GPWS......... GPWS OVRD or FLAP OVRD (depending on version) LDG GEAR GRAVITY EXTENSION procedure (2.24)..........APPLY APP/LDG SPEED........................VmHB 0 + 5 KT + WIND EFFECT LDG DIST ........................MULTIPLY LDG DIST FLAPS 30 BY 2.6 Note: Refer to Part 4 to determine VmHB and LDG DIST

CAUTION: Tail strike may occur if pitch attitude exceeds 8° during the flare depending upon vertical speed at touch down.

� After touch down REVERSE............................................................................AS RQD BRK HANDLE.......................................................... EMER AS RQD TAXI ON BOTH ENGINES

BOTH HYD SYS LOST EQUIPMENT LIST

R BLUE GREEN

R R R



HYD LO PR / HYD OVHT

PUMP affected side ........................................................................ OFF X FEED ............................................................................................. ON

Mod : 4371 Eng : PW124

2.21

72

FOLLOWING FAILURES FLIGHT CONTROL

APR 08 050

FLAPS UNLK

If before V1

TAKE OFF ............................................................................ ABORT If after V1

VR, V2.............................................................INCREASE BY 10 KT If alarm occurs during approach

GO AROUND procedure .......................................................APPLY VGA ................................................................INCREASE BY 10 KT

When possible FLAPS..............................................................................................0 REDUCED FLAPS LANDING procedure (2.21)....................APPLY

FLAPS JAM / UNCOUPLED / ASYM

FLAPS CONTROL LEVER ..........NEAR FLAPS PRESENT POSITION

When applicable REDUCED FLAPS LANDING procedure (2.21)....................APPLY

REDUCED FLAPS LANDING

GPWS .............. GPWS OVRD or FLAP OVRD (depending on version) STEEP SLOPE APPROACH (≥4.5°) ............................... PROHIBITED

FLAPS LDG DIST FLAPS 30

MULTIPLY BY APP/LDG SPEED

0 1.9 VmHB 0 + WIND EFFECT + 5 KT

15 1.8 VmHB 15 + WIND EFFECT

Note: Refer to Part 4 to determine VmHB and LDG DIST CAUTION: Tail strike may occur if pitch attitude exceeds 8° during the

flare depending upon vertical speed at touch down.

STICK PUSHER / SHAKER FAULT

STICK PUSHER / SHAKER ........................................................... OFF TCAS (if installed) ................................................................... TA ONLY VmHB / VmLB FOR ALL CONFIGURATION ......INCREASE BY 10 KT LDG DIST ...............................................................MULTIPLY BY 1.13 Note: Refer to Part 4 to determine VmHB / VmLB and LDG DIST

Mod : 4371 Eng : PW124

2.22

72


APR 08 001

PITCH TRIM ASYM (LOCAL LIGHT)

AP DISCONNECTION...................................... CONFIRM MANUALLY PITCH TRIM INOPERATIVE procedure (2.22) ..........................APPLY

PITCH TRIM INOPERATIVE

EXISTING CONFIGURATION AND SPEED.......................................... .................................................... MAINTAIN AS LONG AS POSSIBLE

For approach STEEP SLOPE APPROACH (≥4.5°).......................... PROHIBITED FLAPS................ EXTEND AT VFE FOR EACH CONFIGURATION LDG SPEED ...................................................INCREASE BY 10 KT LDG DIST .......................................................... MULTIPLY BY 1.13 Note: Refer to Part 4 to determine VmHB / VmLB and LDG DIST

RUDDER RELEASABLE CENTERING UNIT FAIL

If YD is available

YD ...................................................................................... ENGAGE If YD is not available

KEEP THE FEET ON THE PEDALS

PITCH DISCONNECT

BOTH CONTROL COLUMNS ........................................ CHECK FREE IAS .......................................................................................180 kt MAX LOAD FACTOR ............................................................................... 2 g MAX BANK ANGLE............................ 30° MAX UNTIL FLAPS EXTENSION

AVOID ICING CONDITIONS For approach

STEEP SLOPE APPROACH (≥4.5°).......................... PROHIBITED LAND AT AIRPORT WITH MINIMUM CROSSWIND LDG SPEED ...................................................INCREASE BY 10 KT LDG DIST .......................................................... MULTIPLY BY 1.13 PL 1 + 2 ..................................... REDUCE SMOOTHLY TO FLARE Note: Refer to Part 4 to determine LDG DATA

When on ground and ELEV CLUTCH GUARDED PB installed PITCH RECONNECTION ON GROUND procedure (2.22A) ............ ...............................................................................................APPLY

2.22A

72


APR 08 001

PITCH RECONNECTION ON GROUND

(if applicable)

GUST LOCK ........................................................................... ENGAGE BOTH COLUMNS...................................................... CHECK LOCKED ELEV CLUTCH GUARDED PB .........................DEPRESS AND HOLD

When PITCH DISCONNECT flashes red on CAP ELEV CLUTCH GUARDED PB ........................................RELEASE PITCH DISCONNECT ON CAP ...............CHECK EXTINGUISHED BOTH COLUMNS.............................................. CHECK COUPLED

TLU FAULT

If ADC 1 + 2 are lost

If IAS above 185 kt TLU ...................................................................................HI SPD If IAS below 185 kt TLU ................................................................................. LO SPD DISREGARD TLU FAULT ALERT

If at least one ADC operates If IAS above 185 kt TLU ...................................................................................HI SPD If TLU FAULT alarm persists SPEED ............................................................... 180 KT MAX TLU............................................................................ LO SPD If IAS below 185 kt SPEED..................................................................... 180 KT MAX TLU................................................................................. LO SPD DISREGARD TLU FAULT ALERT If TLU green light is not lit VAPP ....................................................INCREASE BY 10 KT LDG DIST ................................................ MULTIPLY BY 1.13 LAND AT AIRPORT WITH MINIMUM CROSSWIND Note: Maximum demonstrated crosswind (dry runway) with TLU HI SPD

mode : 15 kt.

2.23

72


APR 08 001

ELEVATOR JAM

CONTROL COLUMNS ...................................................... UNCOUPLE

AVOID ICING CONDITIONS IAS ..................................................................................... 180 KT MAX

If one elevator is stuck to full down position IAS ................................................................................ 154 KT MAX

If left elevator is jammed MINIMUM MANEUVER OPERATING SPEEDS..........INCREASE BY 10 KT

If elevator jamming occurs at take off IAS ................................................................................ 161 KT MAX PITCH DISCONNECT procedure (2.22).....................................APPLY

AILERON JAM / SPOILER JAM

BANK ANGLE LIMIT................................................................ 25° MAX BLUE AND AUX HYD PUMPS ....................................................... OFF LAND AT AIRPORT WITH MINIMUM CROSSWIND

For approach STEEP SLOPE APPROACH (≥4.5°).......................... PROHIBITED BLUE AND AUX HYD PUMPS.................................................... ON CAUTION: Do not extend FLAPS in turn

When in landing configuration BLUE AND AUX HYD PUMPS.................................................. OFF

Immediately after touch down BLUE AND AUX HYD PUMPS.................................................... ON

RUDDER JAM

STEEP SLOPE APPROACH (≥4.5°) ............................... PROHIBITED LANDING............................................................................... FLAPS 30 USE DIFFERENTIAL POWER SO AS TO MINIMIZE SIDESLIP LAND AT AIRPORT WITH MINIMUM CROSSWIND

At touch down NOSE DOWN BEFORE REDUCTION BELOW FI

2.24

72

FOLLOWING FAILURES LANDING GEAR

APR 08 001

LDG GEAR GRAVITY EXTENSION

LDG GEAR LEVER..................................................................... DOWN EMER EXTENSION HANDLE .........PULL ABOVE PEDESTAL LEVEL .....................AND MAINTAIN UP TO GREEN LIGHTS ILLUMINATED

CAUTION: Do not twist the handle when operating TCAS (if installed) ................................................................... TA ONLY If unsuccessful

LANDING WITH ABNORMAL LDG GEAR procedure (2.24)............APPLY

LANDING WITH ABNORMAL LDG GEAR

Preparation CABIN CREW (PA).............................................................. NOTIFY ATC / TRANSPONDER...................................... NOTIFY / AS RQD SEAT BELTS / NO SMOKING .................................................... ON GPWS........................................................................................ OFF CABIN AND COCKPIT .................................................... PREPARE LOOSE AND SURVIVAL EQUIPMENT ............ CHECK SECURED BELTS AND SHOULDER HARNESS .................. CHECK LOCKED FUEL WEIGHT .......................................... IF POSSIBLE, REDUCE If abnormal nose LDG GEAR CG LOCATION..............................................IF POSSIBLE, AFT If abnormal main LDG GEAR FUEL UNBALANCE .........................IF POSSIBLE, ESTABLISH Note: Reduced fuel on side with failed LDG GEAR.

Approach LDG GEAR LEVER ............................................. CONFIRM DOWN LDG GEAR EMER EXT HANDLE .....................CONFIRM PULLED ENG START ROTARY SELECTOR..............OFF / START ABORT CABIN REPORT........................................... CONFIRM OBTAINED

Before landing BLEEDS 1 + 2............................................................................ OFF BRACE FOR IMPACT ..........................................................ORDER

At touch down PL 1 + 2 .........................................................................................GI CL 1 + 2 .......................................................... FTR THEN FUEL SO

After touch down FIRE HANDLES 1 + 2 ..............................................................PULL

When aircraft stopped PARKING BRAKE ......................................................................SET CABIN CREW (PA).............................................................. NOTIFY FUEL PUMPS 1 + 2................................................................... OFF AGENTS 1 + 2 ....................................................................... DISCH EVACUATION ....................................................................INITIATE

Before leaving aircraft BAT ............................................................................................ OFF

2.2572

FOLLOWING FAILURESLANDING GEAR

SEP 10 001

LDG GEAR UNSAFE INDICATION

If LDG GEAR selected DOWN If GREEN LIGHT OFF on one panel only

UNSAFE INDICATION ........................................... DISREGARD If GREEN LIGHT OFF on both panels

LDG GEAR GRAVITY EXTENSION procedure (2.24) ....APPLY

If LDG GEAR selected UP If RED LIGHT ON on one panel only

UNSAFE INDICATION ........................................... DISREGARD If RED or GREEN LIGHT ON on both panels

LEAVE AND AVOID ICING CONDITIONSIAS ........................................................................... 160 KT MAXLDG GEAR ....................................................................... DOWNTCAS (if installed)......................................................... TA ONLY

LDG GEAR RETRACTION IMPOSSIBLE

LEAVE AND AVOID ICING CONDITIONSLDG GEAR LEVER..................................................................... DOWNIAS ..................................................................................... 185 KT MAXCCAS .............................................................................................. RCLTCAS (if installed) ................................................................... TA ONLYIDLE GATE ............................................................................MONITOR

ANTI-SKID FAULT

R ANTI SKID ...................................................................................... OFFLDG DIST ................................................................. MULTIPLY BY 1.4Note: Refer to Part 4 to determine LDG DIST

At touch downREVERSE............................................................................AS RQDNORMAL BRAKE .................................................USE WITH CAREBRAKE HANDLE ..................................................... EMER AS RQD

BRK TEMP HOT

If BRK TEMP HOT occurs before take offTAKE OFF .............................................................................DELAY

If BRK TEMP HOT occurs in flightLEAVE LDG GEAR DOWN FOR 1 MINUTE AFTER TAKE OFFFOR COOLING EXCEPT IN CASE OF EMERGENCY

2.26

72

FOLLOWING FAILURES AIR

APR 08 001

BLEED VALVE FAULT

PACK VALVE affected side ............................................................ OFF BLEED VALVE affected side .......................................................... OFF MAX FL ..................................................................................200 / MEA AVOID LARGE QUICK POWER CHANGES AT HIGH ALTITUDES

BLEED OVHT

PACK VALVE affected side ............................................................ OFF BLEED VALVE affected side .......................................................... OFF MAX FL ..................................................................................200 / MEA AVOID LARGE QUICK POWER CHANGES AT HIGH ALTITUDES

BLEED LEAK

PACK VALVE affected side ............................................................ OFF BLEED VALVE affected side .......................................................... OFF MAX FL ..................................................................................200 / MEA AVOID LARGE QUICK POWER CHANGES AT HIGH ALTITUDES CAUTION: System must not be restored in flight. Note: If a bleed leak occurs on ground during taxi, go back to parking.

X VALVE OPEN

CAUTION: Do not supply both packs from one single bleed.

PACK VALVE FAULT

PACK VALVE affected side ............................................................ OFF MAX FL ..................................................................................200 / MEA AVOID LARGE QUICK POWER CHANGES AT HIGH ALTITUDES

BOTH PACK VALVES FAULT

MAX FL ..................................................................................100 / MEA When ΔP < 1 PSI

OVBD VALVE ............................................................... FULL OPEN MAN RATE KNOB..........................................................9 O'CLOCK CAB PRESS MODE SEL...........................................................MAN MAN RATE KNOB................................................. MAX INCREASE

RECIRC FAN FAULT

RECIRC FAN affected side ............................................................ OFF

2.26A

72


OCT 08 001

DUCT OVHT

TEMP SEL affected side.................................................................MAN COMPT TEMP SELECTOR affected side....................................COLD CAUTION: Monitor DUCT TEMP and make sure it remains positive to

avoid possible pack turbine damage due to freezing. If alert persists

PACK VALVE affected side....................................................... OFF MAX FL.............................................................................200 / MEA AVOID LARGE QUICK POWER CHANGES AT HIGH ALTITUDES

EXCESS CAB ALT

R

CABIN PRESS IND....................................................................CHECK

If rapid decompression EMERGENCY DESCENT procedure (1.07A) .......................APPLY

If Z cabin > 10000 ft confirmed MAN RATE KNOB..........................................................9 O'CLOCK CAB PRESS MODE SEL...........................................................MAN MAN RATE KNOB.........................................................DECREASE

If unsuccessful CREW OXYGEN MASKS............................................................ ON CREW COMMUNICATIONS .........................................ESTABLISH OXYGEN PAX SUPPLY......................................................AS RQD OXYGEN PRESSURE..........................................................CHECK DESCENT.................................................................AS RQD / MEA

AUTO PRESS FAULT

MAN RATE KNOB ...............................................................9 O'CLOCK CAB PRESS MODE SEL................................................................MAN MAN RATE KNOB ...............................AS RQD TO SET CABIN RATE

FL 140 170 200 250

TARGET CAB ALT (ft) 0 2000 4000 6750

Note: Minimum TARGET CAB ALT is landing elevation

EXCESS CAB ΔP

MAN RATE KNOB ...............................................................9 O'CLOCK CAB PRESS MODE SEL................................................................MAN MAN RATE KNOB ...................................................... MAX INCREASE

If unsuccessful DESCENT TO A COMPATIBLE FL....................................INITIATE

2.27

72


APR 08 001

AVIONICS VENT EXHAUST MODE FAULT

EXHAUST MODE ........................................................................ OVBD

OVBD VALVE FAULT

CAUTION: Do not select OVBD valve FULL OPEN if ΔP > 1 PSI.

If engine 1 running, in flight or on ground OVBD VALVE ............................................................. FULL CLOSE

If engine 1 not running, on ground OVBD VALVE ............................................................... FULL OPEN

2.28

72

FOLLOWING FAILURES DE/ANTI ICE

APR 08 070

AFR AIR BLEED FAULT

LEAVE AND AVOID ICING CONDITIONS AFR AIR BLEED............................................................................. OFF

If DE-ICING ENG FAULT light illuminates after 10 s DE-ICING ENG affected side .................................................... OFF AFR AIR BLEED.......................................................................... ON AFR AIR BLEED light ....................................CHECK EXTINGUISH

If DE-ICING ENG FAULT light does not illuminate on any side DE-ICING AIR FRAME FAULT procedure (2.28)..................APPLY

DE-ICING AIR FRAME FAULT

DE-ICING AIR FRAME ................................................................... OFF LEAVE AND AVOID ICING CONDITIONS MINIMUM ICING SPEEDS ................................... INCREASE BY 10 kt

If in icing conditions LDG DIST .......................................................... MULTIPLY BY 1.13 Note: Refer to Part 4 to determine SPEEDS and LDG DIST

If ice accretion STEEP SLOPE APPROACH (≥4.5°).......................... PROHIBITED

DE-ICING MODE SEL FAULT

OVRD........................................................................................SELECT MONITOR DE-ICING

In case of engine flame out OVRD................................................................................RELEASE

Mod : 1368 + (3973 or 4371)

2.29

72

FOLLOWING FAILURES DE/ANTI ICE

OCT 08 500

ICE DETECT FAULT

ICE ACCRETION................................................ VISUALLY MONITOR

DE-/ANTI-ICING ENG FAULT

LEAVE AND AVOID ICING CONDITIONS ENGINE PARAMETERS affected side..................................MONITOR

ANTI-ICING PROP FAULT

LEAVE AND AVOID ICING CONDITIONS ANTI-ICING PROP affected side.................................................... OFF

If propeller unbalance due to ice becomes excessive CL 1 + 2 ......................... MOVE TO 100% OVRD FOR 5 MINUTES

ANTI-ICING HORNS FAULT

LEAVE AND AVOID ICING CONDITIONS

If in icing conditions, every 5 minutes FLIGHT CONTROLS.............CHECK FREEDOM OF MOVEMENT

SIDE WINDOW / WINDWHIELD HTG FAULT

SIDE WINDOW / WINDSHIELD HTG affected side....................... OFF

PROBES HTG FAULT

R

If One PROBE HTG ALPHA illuminated

STICK PUSHER / SHAKER .............................................MONITOR If Two PROBE HTG ALPHA illuminated

STICK PUSHER / SHAKER ...................................................... OFF STICK PUSHER / SHAKER procedure (2.21).......................APPLY

If PROBE HTG other than ALPHA illuminated ADC non affected side................................................... SELECTED Associated INDICATION ..................................................MONITOR

Mod : 3973 or 4371 or 4457

2.30

72

FOLLOWING FAILURES AUTO PILOT

OCT 08 500

AILERON MISTRIM (ADU message)

– or – EXCESSIVE LATERAL TRIM REQUIRED

– or – ABNORMAL FLIGHT CHARACTERISTICS

FLIGHT CONTROLS ...............................................HOLDING FIRMLY AP ...................................................................................DISCONNECT

Note: FLY MANUALLY PRIOR TO ADJUSTING THE LATERAL TRIMS Note: The autopilot may be reengaged following adjustment of the lateral

trims

PITCH MISTRIM (ADU message)

FLIGHT CONTROLS ...............................................HOLDING FIRMLY AP ...................................................................................DISCONNECT Note: FLY MANUALLY UNTIL RESUMING NORMAL CONDITIONS

PITCH TRIM FAIL (ADU message)

FLIGHT CONTROLS ...............................................HOLDING FIRMLY AP ...................................................................................DISCONNECT Note: FLY MANUALLY UNTIL RESUMING NORMAL CONDITIONS

DADC DATA INVALID (ADU Message)

INSTRUMENTS............................................................CROSSCHECK FAULTY ADC......................................................................... IDENTIFY ADC SW............................................................... SELECT VALID ADC

If ADC 1 is wrong C/B ADC 1 ................................................................................PULL

If ADC 2 is wrong C/B ADC 2 ................................................................................PULL ADC FAULT procedure (2.32) ...................................................APPLY

Mod : 3168

2.30A

72

FOLLOWING FAILURES AND ABNORMAL

MPC APR 08 100

APPLICABLE TO AIRCRAFT FITTED WITH MODIFICATION 5567 or 8392 or 8442

APM FAULT

APM ..................................................................................................OFF

For troubleshooting see FCOM 2.02.21.

DEGRADED PERF

Mainly appears in level flight after CRUISE SPEED LOW or in climb, to inform the crew that an abnormal drag increase induces a speed decrease or a loss of rate of climb

The most probable reason is an abnormal ice accretion

AIRFRAME DE-ICING ON.........................................................CHECK IAS > RED BUG + 10 KT.......................................................MONITOR AP (if engaged) ................HOLD FIRMLY CONTROL WHEEL and DISENGAGE

If SEVERE ICING conditions confirmed – or – If impossibility to maintain IAS > RED BUG + 10 KT in level flight – or – If abnormal aircraft handling feeling

SEVERE ICING procedure (1.09) .........................................APPLY

If not

SCHEDULED FLIGHT....................................................CONTINUE ICING CONDITIONS and SPEED....................................MONITOR

INCREASE SPEED

Appears after DEGRADED PERF to inform the crew that the drag is abnormally high and IAS is lower than RED BUG + 10 KT

If abnormal conditions confirmed

IMMEDIATELY PUSH THE STICK TO INCREASE SPEED TO RECOVER MINIMUM IAS = RED BUG + 10 KT

SEVERE ICING procedure (1.09) .........................................APPLY

2.31

72

FOLLOWING FAILURES AVIONICS

APR 08 001

AUDIO SEL FAULT

AUDIO SEL affected side ............................................................. ALTN

AHRS A / ERECT FAIL

ATT / HDG PB affected side................................................. DEPRESS

When possible AIRCRAFT.................................... STABILIZE SPEED AND LEVEL AHRS affected side, PUSH TO ERECT PB ......................................

.................................................DEPRESS FOR 15 SECONDS

EFIS COMP

BOTH EADI, STBY HORIZON ..................................... CROSSCHECK WRONG INSTRUMENT ........................................................ IDENTIFY ATT / HDG PB affected side................................................. DEPRESS

If AHRS 1 is wrong C/B AHRS 1 NORM SPLY........................................................PULL C/B AHRS 1 AUX SPLY ...........................................................PULL

If AHRS 2 is wrong C/B AHRS 2 NORM SPLY........................................................PULL C/B AHRS 2 AUX SPLY FLT....................................................PULL

If LOC / GS / ILS caution appears on EFIS NAV SOURCES....................................................................CHECK VOR / ILS PB affected side .............................. DEPRESS AS RQD

ADC SW FAULT

ADC SW........................................................ SET TO OPPOSITE ADC

2.32

72

FOLLOWING FAILURES AVIONICS

APR 08 050

ADU FAILURE

IAS / VS MODE.......................................................................USE TCS Note: ALT SEL mode is lost

If amber "AP MSG" appears on EADI – or – If in composite mode FLIGHT CONTROLS................................................ HOLD FIRMLY AP ..............................................................................DISCONNECT

ADC FAULT

VALID ADC ...............................................................................SELECT PF..............................................................................NON affected side AP COUPLING .........................................................NON affected side ATC.................................................................NON affected equipment

If ADC 1 is lost LANDING ELEVATION ...................... PRESSURE ALTITUDE SET GPWS........................................................................................ OFF

If ADC 1 + 2 are lost STBY INST ................................................................................ USE MAN RATE KNOB..........................................................9 O'CLOCK CAB PRESS MODE SEL...........................................................MAN ENGINE PARAMETERS ..................................................MONITOR TCAS (if installed).................................................................... STBY GPWS........................................................................................ OFF TLU ................................................................................MAN MODE TLU FAULT procedure (2.22A) .............................................APPLY

AHRS FAIL

ATT / HDG PB affected side................................................. DEPRESS Periodically compare remaining AHRS outputs to STBY INST

SGU FAIL

EFIS SG PB affected side .................................................... DEPRESS

CRT FAIL

CRT affected................................................................................... OFF

Mod : 5205

2.32A

72

FOLLOWING FAILURES MISCELLANEOUS

APR 08 100

COCKPIT DOOR CONTROL PANEL FAULT (if installed)

COCKPIT DOOR MANUAL LOCK BOLT(S).......................................... ............................................................... MOVE TO CLOSE POSITION Note: when the door is locked with the manual bolt(s), the emergency

access to the cockpit is unavailable. It is recommended that at least two crewmembers remain in the cockpit during that time.

2.3372

FOLLOWING FAILURESMISCELLANEOUS

SEP 10 001

LOSS OF RADIO ALTIMETER INFORMATION

GPWS ............................................................................................. OFFTCAS (if installed) ......................................................................... STBY

CAUTION: LDG GEAR NOT DOWN undue warning may begenerated when reducing PL; this alarm may becancelled by using EMER AUDIO CANCEL.

R SMK DET FANS FAULT

FAN............................................................................................... ALTN

DOORS UNLK IN FLIGHT

If any door except FWD COMPTSIGNS.......................................................................................... ONASSOCIATED DOOR.........................................VISUALLY CHECK

If unlocked or check not feasibleLANDING ELEVATION .....................................................9000 ftMAX FL........................................................................100 / MEA

If FWD COMPTNO ACTION

COCKPIT WINDOW CRACKED

WINDOW HEAT affected................................................................ OFFLANDING ELEVATION................................................................9000 ftMAX FL ..................................................................................100 / MEA

OXYGEN LO PR

OXY MAIN SUPPLY ...................................................... OFF THEN ON

If OXYGEN LO PR light remains illuminatedMAIN SUPPLY........................................................................... OFFOXYGEN PORTABLE UNIT.......... INSTALL IN COCKPIT AS RQD

2.34

72

FOLLOWING FAILURES MFC

OCT 08 001

MFC 1A FAULT

R R

MODULE 1A .................................................................... OFF / RESET MFC 1A MODULE LOST EQUIPMENT LIST............................CHECK

R MFC 1A MODULE LOST EQUIPMENT LIST

MECHANIC CALL IND DC BUS 1 OFF WARNING AC BUS 1 SPLY INV 1 FAULT LIGHT

LDG GEAR PRIMARY UNLK IND BLEED HP VALVE 1 FWD COMPT DOOR UNLK IND EMER HATCH UNLK IND RIGHT AFT DOOR UNLK IND, if

applicable

MFC 1B FAULT

R R

MODULE 1B .................................................................... OFF / RESET MFC 1B MODULE LOST EQUIPMENT LIST............................CHECK

If failure during take off PACK 1 ...................................................................................... OFF OVBD VALVE ............................................................... FULL OPEN Prior take off PACK 2 ................................................................................. OFF After take off PACKS.................................................................................... ON OVBD VALVE........................................................ FULL CLOSE LDG GEAR ......LEAVE DOWN FOR COOLING FOR 1 MINUTE ..........AFTER TAKE OFF EXCEPT IN CASE OF EMERGENCY

After landing PACK 1 ...................................................................................... OFF OVBD VALVE ............................................................... FULL OPEN

CAUTION : Before opening any door, PACKS 1 and 2 must be selected OFF and cockpit communication hatch must be open.

R MFC 1B MODULE LOST EQUIPMENT LIST

GROUND FAN 1 OUTFLOW VALVE OPENING AFTER

LANDING OVBD VALVE AUTO

FUNCTIONING CVR ERASE

DC STBY BUS UNDV DETECT INV 1 FAULT LIGHT GREEN PUMP LO PR IND BRAKE OVERTEMP ALERTS LH / RH BLEED VALVE 1 FAULT IND

2.35

72


OCT 08 001

MFC 2A FAULT

R R

MODULE 2A .................................................................... OFF / RESET AVIONICS VENT EXHAUST MODE ........................................... OVBD MFC 2A MODULE LOST EQUIPMENT LIST............................CHECK

If failure during taxi out OVBD VALVE ............................................................... FULL OPEN After take off IDLE GATE......................................................................CHECK OVBD VALVE.....................................................................AUTO

At touch down IDLE GATE .......................................................................MONITOR

After landing OVBD VALVE ............................................................... FULL OPEN

R MFC 2A MODULE LOST EQUIPMENT LIST

AIR X VALVE OVBD VALVE AUTO FUNCTIONING EXTRACT FAN HOSTESS CALL IND CREW CALL IND DC BUS 2 OFF WARNING AC BUS 2 SPLY INV 2 FAULT LIGHT

RH SIDE WINDOW ANTI-ICING LDG GEAR Secondary UNLK IND LDG GEAR Secondary GREEN

ARROWS BLEED HP VALVE 2 LEFT DOORS UNLK IND IDLE GATE AMBER WARNING

MFC 2B FAULT

R R

MODULE 2B .................................................................... OFF / RESET MFC 2B MODULE LOST EQUIPMENT LIST............................CHECK

Failure during take off PACK 2 ...................................................................................... OFF OVBD VALVE ............................................................... FULL OPEN Prior take off PACK 1 ................................................................................. OFF After take off PACK 1 + 2............................................................................. ON OVBD VALVE........................................................ FULL CLOSE LDG GEAR ......LEAVE DOWN FOR COOLING FOR 1 MINUTE ..........AFTER TAKE OFF EXCEPT IN CASE OF EMERGENCY

After landing PACK 2 ...................................................................................... OFF OVBD VALVE ............................................................... FULL OPEN

CAUTION: Before opening any door, PACKS 1 and 2 must be selected OFF and cockpit communication hatch must be open.

R MFC 2B MODULE LOST EQUIPMENT LIST

GROUND FAN 2 OUTFLOW VALVE OPENING AFTER

LANDING OVBD VALVE AUTO FUNCTIONING INV 2 FAULT LIGHT RH SIDE WINDOW ANTI-ICING and

associated FAULT IND

LDG GEAR Secondary UNLK IND LDG GEAR Secondary GREEN

ARROWS RH BRAKE OVERTEMP ALERTS BLEED VALVE 2 FAULT IND

2.36

72


OCT 08 001

MFC 1A+1B FAULT

R R

MODULES 1A+1B ........................................................... OFF / RESET PROP 1 ANTI-ICING ...................................................................... OFF PROP ANTI-ICING FAULT procedure (2.29) .............................APPLY DE-ICING MODE SEL .................................................. OVRD AS RQD PACK 1 ........................................................................................... OFF BLEED 1 ......................................................................................... OFF BLEED VALVE FAULT procedure (2.26) ...................................APPLY RADAR ........................................................................................... OFF GPWS ............................................................................................. OFF MFC 1A+1B MODULES LOST EQUIPMENT LIST...................CHECK

Before landing ATPCS....................................................................................... OFF



R MFC 1A+1B MODULES LOST EQUIPMENT LIST

PACK 1 / PACK 1 FAULT IND GROUND FAN 1 OUTFLOW VALVE OPENING AFTER

LANDING OVBD VALVE AUTOFUNCTIONING MECHANIC CALL IND CVR ERASE DC STBY BUS UNDV DETECT DC BUS 1 OFF WARNING AC BUS 1 SPLY INV 1 FAULT LIGHT LEFT PFTS STICK PUSHER TRIPLE TRIM IND GREEN PUMP LO PR INDICATION ANTI-ICING PROP 1 and associated

FAULT IND

DE-ICING AIRFRAME (BOOTS A) DE-ICING AIRFRAME (BOOTS B) LH SIDE WINDOW ANTI-ICING and

associated FAULT IND PRIMARY UNLK IND PRIMARY GREEN ARROWS BRAKE OVERTEMP ALERTS LH / RH BLEED HP VALVE 1 BLEED VALVE 1 and associated

FAULT IND FWD COMPT DOOR UNLK IND EMER HATCH UNLK IND RIGHT AFT DOOR UNLK IND, if

applicable ENG 1 UPTRIM ENG 1 AUTO FEATHER LEFT AUTO CL

2.3772

FOLLOWING FAILURESMFC

OCT 08 001

MFC 1A+2A FAULT

R

R

R

MODULES 1A+2A ........................................................... OFF / RESETTLU .....................................................................................MAN MODEAVIONICS VENT EXHAUST MODE ........................................... OVBDRADAR ........................................................................................... OFFGPWS ............................................................................................. OFFMFC 1A+2A MODULES EQUIPMENT LIST .............................CHECKNote : Airframe FAULT amber alert is lost.Note : When airframe de-icing is used, monitor boots inflation.Note : As AP OFF alert is lost, use of AP below 1000 ft AGL is prohibited.Note : VOR 2, ADF 2, CRS 2 information are lost. ADC 2 outputs are not

available.

Before landingLDG GEAR LEVER ............................................................... DOWNEMER EXTENSION HANDLE..................................................PULL

CAUTION : LDG GEAR cannot be retracted.

At touch downIDLE GATE .......................................................................MONITOR

After landingOVBD VALVE ................................................................FULL OPEN

R MFC 1A+2A MODULES LOST EQUIPMENT LIST

AIR X VALVEOVBD VALVE AUTOFUNCTIONINGEXTRACT FANAP OFF WARNING LIGHTALTITUDE ALERT LIGHTGUIDANCE LIGHTMECHANIC CALL INDHOSTESS CALL INDCREW CALL INDRECORDERS (START/STOP)DC BUS 1 + 2 OFF WARNINGAC BUS 1 + 2 SPLYINV 1 + 2 FAULT LIGHTEMER BAT CHG CTLFLAPS UNLK WARNINGSTICK PUSHER / SHAKER FAULTReleasable Centering Unit AUTO

DISCONNECT after YAW TRIMaction or YD engagement

TLU FAULT LIGHT

TRIPLE TRIM INDAIL LOCK LIGHT (if installed)DE-ICING AIRFRAME FAULTRH SIDE WINDOW ANTI-ICINGCCAS WARNING ALERT (FLAP

UNLK)LDG GEAR CONTROLLDG GEAR PRIMARY UNLK INDLDG GEAR Secondary UNLK INDLDG GEAR Secondary GREEN

ARROWSLIGHT TESTBLEED HP VALVE 1 + 2LEFT DOORS UNLK INDFWD COMPT DOOR UNLK INDEMER HATCH UNLK INDRIGHT AFT DOOR UNLK IND, if

applicableRIGHT FWD DOOR UNLK INDIDLE GATE and associated AMBER

WARNING

2.3872


OCT 08 001

MFC 1A+2B FAULT

R

R

R

MODULES 1A+2B ........................................................... OFF / RESETMAIN BLUE HYD PUMP................................................................. OFFHYD X FEED .................................................................................... ONDE-ICING MODE SEL .................................................. OVRD AS RQDMFC 1A+2B MODULES EQUIPMENT LIST .............................CHECKNote : AP does not disconnect after STBY PITCH TRIM activation.

Before landingNote : Flaps control is lost.REDUCED FLAPS LANDING procedure (2.21)....................APPLYLDG GEAR LEVER ............................................................... DOWNEMER EXTENSION HANDLE..................................................PULL


After landingPACK 2 ...................................................................................... OFFOVBD VALVE ................................................................FULL OPEN

CAUTION : Before opening any door, PACKS 1 and 2 must be selectedOFF and cockpit communication hatch must be open.


GROUND FAN 2OUTFLOW VALVE OPENING AFTER

LANDINGOVBD VALVE AUTOFUNCTIONINGMECHANIC CALL INDDC BUS 1 OFF WARNINGAC BUS 1 SPLYINV 1 + 2 FAULT LIGHTFLAPS CONTROLBLUE HYD PUMP CTLDE-/ANTI-ICING ENG 1DE-/ANTI-ICING ENG 2 FAULT

RH SIDE WINDOW ANTI-ICING andassociated FAULT IND

LDG GEAR CONTROLLDG GEAR PRIMARY UNLK INDLDG GEAR Secondary UNLK INDLDG GEAR Secondary GREEN

ARROWSBRAKE OVERTEMP ALERT RHBLEED HP VALVE 1BLEED VALVE 2 FAULT INDFWD COMPT DOOR UNLK INDEMER HATCH UNLK INDRIGHT AFT DOOR UNLK IND, if

applicable

2.3972


OCT 08 001

MFC 1B+2A FAULT

R

RR

MODULES 1B+2A ........................................................... OFF / RESETDE-ICING MODE SEL .................................................. OVRD AS RQDAVIONICS VENT EXHAUST MODE ........................................... OVBDMFC 1B+2A MODULES EQUIPMENT LIST .............................CHECKNote : VOR 2, ADF 2, CRS 2 information are lost. CM2 IAS is not

available.

Before landingNote : Flaps control is lost.REDUCED FLAPS LANDING procedure (2.21)....................APPLYLDG GEAR LEVER ............................................................... DOWNEMER EXTENSION HANDLE..................................................PULL


At touch downIDLE GATE .......................................................................MONITOR

After landingPACK 1 ...................................................................................... OFFOVBD VALVE ................................................................FULL OPEN

CAUTION : Before opening any door, PACKS 1 and 2 must be selectedOFF and cockpit communication hatch must be open.

R MFC 1B+2A MODULES LOST EQUIPMENT LIST

GROUND FAN 1AIR X VALVEOUTFLOW VALVE OPENING AFTER

LANDINGOVBD VALVE AUTOFUNCTIONINGEXTRACT FANHOSTESS CALL INDCREW CALL INDCVR ERASEDC STBY BUS UNDV DETECTDC BUS 2 OFF WARNINGAC BUS 2 SPLYINV 1 FAULT LIGHTINV 2 FAULT LIGHT

FLAPS CONTROLGREEN PUMP LO PR INDICATIONDE-/ANTI-ICING ENG 1 FAULTDE-/ANTI-ICING ENG 2RH SIDE WINDOW ANTI-ICINGLDG GEAR CONTROLLDG GEAR Secondary UNLK INDLDG GEAR Secondary GREEN

ARROWSBRAKE OVERTEMP ALERTS LH / RHBLEED HP VALVE 2BLEED VALVE 1 FAULT INDLEFT DOORS UNLK INDIDLE GATE AMBER WARNING

2.40

72


OCT 08 001

MFC 2A+2B FAULT

R R

MODULES 2A+2B ........................................................... OFF / RESET AVIONICS VENT EXHAUST MODE ........................................... OVBD ANTI-ICING PROP 2 ...................................................................... OFF ANTI-ICING PROP FAULT procedure (2.29) .............................APPLY DE-ICING MODE SEL .................................................. OVRD AS RQD PACK 2 ........................................................................................... OFF BLEED 2 ......................................................................................... OFF BLEED VALVE FAULT procedure (2.26) ...................................APPLY MFC 2A+2B MODULES EQUIPMENT LIST .............................CHECK

Before landing ATPCS....................................................................................... OFF

At touch down IDLE GATE .......................................................................MONITOR




PACK 2 PACK 2 FAULT IND GROUND FAN 2 AIR X VALVE OUTFLOW VALVE OPENING AFTER

LANDING OVBD VALVE AUTOFUNCTIONING EXTRACT FAN HOSTESS CALL IND CREW CALL IND DC BUS 2 OFF WARNING AC BUS 2 SPLY INV 2 FAULT LIGHT STICK PUSHER ANTI-ICING PROP 2 ANTI-ICING PROP 2 FAULT DE-ICING AIRFRAME (BOOTS B)

RH SIDE WINDOW ANTI-ICING and associated FAULT IND

LDG GEAR Secondary UNLK IND LDG GEAR Secondary GREEN

ARROWS BRAKE OVERTEMP ALERT RH BLEED HP VALVE 2 BLEED VALVE 2 BLEED VALVE 2 FAULT IND LEFT DOORS UNLK IND ENG 2 UPTRIM ENG 2 AUTO FEATHER PROP BRAKE BRAKING if applicable PROP BRAKE RELEASING if

applicable IDLE GATE AMBER WARNING RIGHT AUTO CL

2.41

72


OCT 08 001

MFC 1B+2B FAULT

R R

MODULES 1B+2B ........................................................... OFF / RESET OVERHEAD PANEL..............................................................MONITOR MFC 1B+2B MODULES EQUIPMENT LIST .............................CHECK

Before landing NOSE WHEEL STEERING ....................................................... OFF ANTI-SKID ................................................................................. OFF ANTI-SKID FAULT procedure (2.25).....................................APPLY LDG GEAR LEVER ............................................................... DOWN EMER EXTENSION HANDLE..................................................PULL


At touch down IDLE GATE ...............................................................................PULL DIFFERENTIAL BRAKING........................................................ USE

After landing PACK 1 + 2 ................................................................................ OFF ANTI-ICING HORNS ................................................................. OFF PROBES HTG ........................................................................... OFF OVBD VALVE ............................................................... FULL OPEN Note : ATPCS ARM light is not available. Autofeather light is lost. Note : External power cannot be used.


R MFC 1B+2B MODULES LOST EQUIPMENT LIST

GROUND FAN 1 GROUND FAN 2 AIR X VALVE OUTFLOW VALVE OPENING AFTER

LANDING OVBD VALVE AUTOFUNCTIONING CVR ERASE DC STBY BUS UNDV DETECT INV 1 FAULT LIGHT INV 2 FAULT LIGHT MAIN BAT CHG CTL BAT DISCHARGE IN FLIGHT FLAPS ASYMMETRY DETECTION STICK PUSHER INHIBITION STICK SHAKER STALL WARNING PITCH TRIM WHOOLER PITCH TRIM ASYMWARNING AIL LOCK LIGHT if applicable GREEN PUMP LO PR INDICATION RH SIDE WINDOW ANTI-ICING and

associated FAULT IND INHIBITION OF HORNS ANTI-ICING

ON GROUND

CCAS MASTER WARNING CCAS MASTER CAUTION CCAS AURAL ALERTS CCAS AMBER ALERTS ON CAP CCAS WARNING ALERTS (CONFIG,

PROP BRK, ENG OIL) LDG GEAR CONTROL LDG GEAR Secondary UNLK IND LDG GEAR Secondary GREEN

ARROWS BRAKE OVERTEMP ALERTS LH / RH LDG GEAR LEVER LOCKED DOWN

ON GROUND NOSE WHEEL STEERING ANTI-SKID "LANDING GEAR NOT DOWN"

WARNING BLEED VALVE 1 FAULT IND BLEED VALVE 2 FAULT IND ARM LIGHT IND PROP BRAKE RED UNLK LT if

applicable LEFT and RIGHT AUTO CL

2.42

72


APR 08 100

DC EMER BUS LOST EQUIPMENT LIST

DC ESS BUS LOST EQUIPMENT LIST

AIR CONDITIONING OVBD and Underfloor Valves CTL OVBD and Underfloor Valves IND AIR COOLING high flow IND PRESS IND / EXCESS ALT IND Pneumatic Outflow Valves FWD COMPT Ventilation Valve (*) COMMUNICATIONS VHF / RCAU CM2 Cockpit Amplifier ELECTRICAL POWER AC BUS OFF 1 + 2 IND ACW BUS OFF 1 + 2 IND INV 1 FAULT IND DC BUS OFF 1 + 2 IND DC STBY BUS IND (UNDV/OVRD) EMER BAT CHG IND FIRE PROTECTION FIRE HANDLE IND ENG 1 + 2 FIRE DETECTION ENG 1 + 2 FLIGHT CONTROLS PITCH TRIM NORMAL COMMAND RUDDER TRIM AILERON TRIM HYDRAULIC POWER BLUE PUMP CTL and IND GREEN PUMP IND ICE AND RAIN PROTECTION AAS CTL, IND and ALERTS WING, EMPENNAGE BOOTS A ENG 1 BOOTS A and B PROP 1 + 2 ANTI-ICING CTL PROP 1 + 2 ANTI-ICING IND HORNS ANTI-ICING IND and CTL INDICATING / RECORDING CM1 CLOCK FDAU on ground LANDING GEAR ANTI-SKID Outboard NOSE WHEEL STEERING WOW 1 CTL LIGHTS CM1 PANELS PYLON STBY COMPASS LAVATORY (EMER) NAVIGATION ATC 1 PROPELLERS A/F AUX PUMPS CTL TQ IND 1 + 2 ENGINES CL FIRE IND 1 + 2 (*): if applicable

AIR CONDITIONING PACK and RECIRC FAN 1 + 2 IND PACK 1 + 2 Valve EXTRACT FAN CTL Landing Elevation IND Cockpit and Cabin Automatic and Manual TEMP CTL and IND AUTO PILOT AP OFF IND and DISC by Quick Disconnect COMMUNICATIONS CM1+2 Flight Interphones CM1+2 Audio Control Panels CM1 Cockpit Amplifier CVR / Passenger Address Mechanical CALL Cockpit and Cabin Crew CALL ELECTRICAL POWER DC SVCE/UTLY BUS 1 + 2 CTL MAIN BAT CHG IND INV 2 FAULT IND FIRE PROTECTION Avionics / Toilets SMK DET FWD and AFT COMPT SMK DET AFT COMPT and FWD COMPT /Toilets DET FANS CTL and IND FWD COMPT Fire Extinguishing CTL, IND and TEST (*) AUX AFT COMPT (*) See 2.42A for Cargo Operations FLIGHT CONTROLS Clutch Reengagement System (*) AILERON Locking CTL FUEL FQI 1 + 2 X FEED Valve Starting Pumps 1 + 2 Motive Flow Valves 1 + 2 HYDRAULIC GREEN PUMP CTL ICE AND RAIN PROTECTION DE-ICING ISOL Valves Side Windows ANTI-ICING IND CAPT/STBY/TAT PROBES IND CM1 Wiper INDICATING / RECORDING FDAU in flight LIGHTS Landing CTL NAVIGATION TAS TEMP IND OXYGEN PRESS IND Pilots and Pax Valves CTL Pax Masks DROP CTL PNEUMATIC BLEED Valves PWR and IND 1 + 2 PROPELLERS NP IND 1 + 2 PROP BRK PWR, CTL and IND ENGINES IGNITION and STARTING 1 + 2 NH/NL, ITT IND 1 + 2

Mod : 4116

NO

RM

AL

PR

OC

ED

UR

ES

3.0172

NORMAL PROCEDURESSEP 10 001

3 - NORMAL PROCEDURESAll steps have to be performed before the first flight of the day orfollowing a crew change or maintenance action. In other cases,start at FINAL COCKPIT PREPARATION.

PROCEDURE LISTED INCLUDE THE USE OF A GPUREFER TO PAGE 3.01A FOR HOTEL MODE.

EXTERIOR INSPECTION

CM1 CM2

Exterior walk around performed

PRELIMINARY COCKPIT PREPARATION

CM1 CM2CARGO DOOR CTL panel cover (ifinstalled)............................. CLOSEDEMER EQPT........................ CHECKGEAR PINS ...................ON BOARDC/Bs ..................................... CHECKBAT ..............................................ONMFC ..................................... CHECKPARKING BRK ............................ONPL 1 + 2 ...................CHECK AT G.I.GUST LOCK ......................ENGAGECL 1 + 2..............................FUEL SOFLAPS LEVER..................... CHECKEEC 1 + 2.....................................ONLDG GEAR.............................DOWNWIPERS .....................................OFFDC EXT PWR P/B........................ON

OVERHEAD PANEL ..............SCANANY WHITE LIGHT....EXTINGUISH

ANN LIGHT..............................TESTENG 1 FIRE.............................TESTPROP BRK (if installed) ..........ON / LOCKEDCVR .........................................TESTSIGNS PANEL..................... CHECKEMER EXIT LIGHT................... ARMEMER LOCK XMTR ...............AUTOCOMPT SMK (if installed)........TESTEXHAUST MODE .................RESETOVBD VALVE .........................AUTOOXYGEN PRESS ................ CHECKENG 2 FIRE.............................TEST

R

3.01A

72

NORMAL PROCEDURES APR 08 001

3 - NORMAL PROCEDURES

All steps have to be performed before the first flight of the day or following a crew change or maintenance action. In other cases, start at FINAL COCKPIT PREPARATION.

HOTEL MODE

EXTERIOR INSPECTION

CM1 CM2

Exterior walk around performed

PRELIMINARY COCKPIT PREPARATION

CM1 CM2

CARGO DOOR CTL panel cover (if installed)............................. CLOSED EMER EQPT........................ CHECK GEAR PINS ...................ON BOARD C/Bs ..................................... CHECK BAT ..............................................ON MFC ..................................... CHECK PARKING BRK ............................ON PL 1 + 2 ............................... CHECK GUST LOCK ..................... ENGAGE CL 1 + 2 ............................ FUEL SO FLAPS LEVER..................... CHECK EEC 1 + 2 ....................................ON LDG GEAR ............................DOWN WIPERS.....................................OFF ENG 2 FIRE.............................TEST PROP BRK (if installed)..........ON / LOCKED ATPCS.....................................TEST OVERHEAD PANEL ..............SCAN ANY WHITE LIGHT....EXTINGUISH ENG 2 START IN HOTEL MODE ANN LIGHT..............................TEST ENG 1 FIRE.............................TEST CVR .........................................TEST SIGNS PANEL..................... CHECK EMER EXIT LIGHT...................ARM EMER LOC XMTR..................AUTO AIR BLEED PANEL: ENG 1 BLEED FAULT and, X VALVE OPEN....................... ........... CHECK ILLUMINATED COMPT SMK (if installed)........TEST EXHAUST MODE .................RESET OVBD VALVE .........................AUTO OXYGEN PRESS ................ CHECK

3.02

72


PRELIMINARY COCKPIT PREPARATION (CONT'D)

CM1 CM2

LEFT LATERAL CONSOLE N/W STEERING.......................... ON OXYGEN MASK (once a day) . CHECK MKR .........................................TEST GPWS ....................................NORM

LEFT INSTRUMENT PANEL NO FLAGS........................... CHECK CLOCK............................. SET TIME RMI / EHSI.......... CROSSCHECK HEADING ADC SW ..............SET TO ADEQUATE ADC

PEDESTAL FDEP (if applicable)............. CHECK TRIMS.................................. CHECK ATPCS (except ENG 2 in Hotel mode).......................................TEST TCAS (if installed)....... STBY / TEST VHF / NAV ...................................ON XPDR.......................................STBY IDLE GATE .......................... CHECK EMER AUDIO CANCEL ...... CHECK AIL LOCK LIGHT (if installed)................. CHECK EXTINGUISHED EFIS .............................................ON RADAR.....................................STBY

CENTRAL PANEL PWR MGT....................................TO PEC 1 + 2 ....................................ON HYD PRESS ........................ CHECK CAB PRESS MODE SEL.......NORM

RIGHT LATERAL CONSOLE OXYGEN MASK (once a day). CHECK

RIGHT INSTRUMENT PANEL NO FLAGS........................... CHECK CLOCK............................. SET TIME RMI / EHSI..........CROSSCHECK HEADING

Mod : 3973 or 4371 or 4457

3.02A

72


COCKPIT DOOR DAILY CHECK (if applicable)

COCKPIT DOOR LOCKING SYSTEM SW .................................................ON In the cargo compartment, on the DOOR CALL panel: EMER PB................................................................................................ON CHECK OPEN LIGHT flashes In the cockpit: CHECK BUZZER CHECK OPEN LIGHT flashes If correct In the cockpit: TOGGLE SW ON COCKPIT DOOR CTL panel ...........................DENY CHECK BUZZER stops CHECK OPEN LIGHT extinguishes In the cargo compartment, on the DOOR CALL panel: CHECK OPEN LIGHT extinguishes and DENIED LIGHT illuminates If correct TOGGLE SW...........................................................................OPEN COCKPIT DOOR LOCKING SYSTEM SW................................OFF COCKPIT DOOR CTL panel FAULT LIGHT........................ CHECK FUNCTIONAL CHECK OF THE MANUAL LOCK BOLT(S)

3.03

72


R FINAL COCKPIT PREPARATION

CM1 CM2

PARKING BRK ............ON / PRESS CHECK ALTIMETERS.............................SET COM / NAV / GPS......................SET FUEL QTY............................ CHECK MEMO PANEL ..................... CHECKPWR MGT....................................TO

ALTIMETERS.............................SET LANDING ELEVATION..............SET COM / NAV / GPS......................SET ENG F/U................................RESET

BEFORE PROPELLER ROTATION

CM1 CM2

TAIL PROP.................... ON BOARDDOORS ..............................CLOSED TO BUGS / APM * ............SET AND CHECK SEAT BELTS............................... ON BEACON ..................................... ON

TO BUGS / APM *.............SET AND CHECK TRIMS........................................SET CDLS * .........................................ON

BEFORE TAXI

CM1 CM2

PROP BRK.................................OFFCOCKPIT COM HATCH ................. CLOSED

CL 1 + 2 ..................................AUTO ANTI-ICING......................... AS RQD ANTI-SKID ...............................TEST FLAPS........................................SET

TAXI

CM1 CM2

TAXI & TO LIGHTS..................... ONBRAKES............................... CHECK RUDDER CAM...................CENTER TAKE OFF BRIEFING...COMPLETE

BRAKES............................... CHECK AFCS..........................................SET TO CONFIG .............................TEST TAKE OFF BRIEFING .. COMPLETE

* : if applicable

Mod : 3973 or 4371 or 4457

3.04

72


R BEFORE TAKE OFF

CM1 CM2

FLIGHT CONTROLS ........... CHECK CCAS ...................................TO INHI EXT LIGHTS ............................... ON FD BAR (When lined up) ........... CENTERED

BLEED VALVES ................. AS RQD AIR FLOW..............................NORM GUST LOCK .................... RELEASE FLIGHT CONTROLS ........... CHECK XPDR / TCAS * ............. ALT / AUTO FD BAR (When lined up)............CENTERED

AFTER TAKE OFF

PF PNF

ALTIMETERS...... SET AND CHECK

LDG GEAR ..................................UP FLAPS............................................. 0 PWR MGT / NP.......... CLB / CHECK BLEED VALVES ..........................ON TAXI AND TO LIGHTS ..............OFF ALTIMETERS.......SET AND CHECK

ICING CONDITIONS

SEE 3.05

DESCENT

PF PNF

CCAS .........................................RCL LDG BUGS.......... SET AND CHECK ARRIVAL BRIEFING.....COMPLETE

LDG BUGS...........SET AND CHECK LDG ELEVATION.......................SET ARRIVAL BRIEFING..... COMPLETE

* : if applicable

Mod : 4111

3.05

72


ENTERING ICING CONDITIONS

ANTI-ICING (PROP - HORNS - SIDE WINDOWS) .....................................ON

PROP MODE SEL.................................................................According to SAT NP .........................................................................................CONFIRM ≥ 86% PWR MGT ROTARY SELECTOR, if in cruise ......................CONFIRM CRZ 1

MINIMUM MANEUVER/OPERATING ICING SPEEDS..................BUGGED AND OBSERVED ICE ACCRETION .............................................................................MONITOR

AT FIRST VISUAL INDICATION OF

ICE ACCRETION AND AS LONG AS ICING CONDITIONS EXIST

ANTI-ICING (PROP - HORNS - SIDE WINDOWS) ...................CONFIRM ON ENG 1 + 2 DE-ICING ...................................................................................ON AIRFRAME DE-ICING .................................................................................ON ENG AND AIRFRAME MODE SEL.......................................According to SAT

MINIMUM MANEUVER/OPERATING ICING SPEEDS..................BUGGED AND OBSERVED BE ALERT TO SEVERE ICING DETECTION In case of severe icing, refer to 1.09

If significant vibrations occur BOTH CL ........................................100 OVRD for not less than 5 minutes

LEAVING ICING CONDITIONS

DE-ICING AND ANTI-ICING MAY BE SWITCHED OFF

WHEN THE AIRCRAFT IS VISUALLY VERIFIED CLEAR OF ICE

ICING AOA CAPTION MAY BE CANCELLED AND NORMAL SPEEDS MAY BE USED

Mod : 3973 or 4371

3.05A

72

NORMAL PROCEDURES MPC

APR 08 100

R

APPLICABLE TO AIRCRAFT FITTED WITH MODIFICATION 5567 or 8392 or 8442

APM TEST

DAILY CHECK MUST BE PERFORMED

APM PTT PB..................................PUSH and MAINTAIN for test duration

- CRUISE SPEED LOW lights on 13 VU (both sides) illuminate - over 1 second later, DEGRADED PERF lights on 13 VU (both sides) illuminate, with

CAUTION light and SC, with CRUISE SPEED LOW lights still illuminated - over 1 second later, INCREASE SPEED lights on 13 VU (both sides) illuminate flashing,

with CAUTION light and SC, with CRUISE SPEED LOW and DEGRADED PERF lights still illuminated

- over 1 second later, FAULT light on the 5VU illuminates, with CAUTION light, SC and ANTI-ICING (on CAP), with CRUISE SPEED LOW, DEGRADED PERF and INCREASE SPEED lights still illuminated

- end of test, the crew stop action on APM PTT TEST pushbutton, all lights shall extinguish.

CRUISE SPEED LOW

Appears in cruise only, to inform the crew that an abnormal drag increase induces a speed decrease of more than 10 KT compared with the expected speed

ICING CONDITIONS and SPEED .........................................MONITOR

3.06

72


R APPROACH

PF PNF

ALTIMETERS...... SET AND CHECK

SEAT BELTS ...............................ON ALTIMETERS ......SET AND CHECK CABIN ALTITUDE................ CHECK

BEFORE LANDING

PF PNF

LDG GEAR........................ 3 GREEN FLAPS.................................. CHECK PWR MGT....................................TO TLU ......................................LO SPD ICING AOA LIGHT............... CHECK EXT LIGHTS ................................ON

AFTER LANDING

CM1 CM2

XPDR / TCAS * / RADAR ........STBY FLIGHT CONTROLS ......... LOCKED FLAPS............................................0° TRIMS...................................RESET LAND LIGHTS / STROBES .......OFF ANTI-/DE-ICING.........................OFF ENG START ROT SEL ..............OFF

After at least one minute CL 1 ..............FTR THEN FUEL SO

PARKING

CM1 CM2

PARKING BRK............................ ONTAXI & TO LIGHTS....................OFFCL 2............................................FTR PROP BRK (if installed) .............. ONBEACON ....................................OFFSEAT BELTS..............................OFF TAIL PROP................ ON POSITION

When leaving the aircraft OXYGEN MAIN SUPPLY........OFF ICE AND RAIN PROTECTION ............OFF EXT LIGHTS............................OFF EMER EXIT LIGHT...........DISARM EFIS / RADAR / COM / NAV................OFF CL 2 .................................FUEL SO FUEL PUMPS 1 + 2.................OFF CDLS *.....................................OFF BAT..........................................OFF

* : if applicable

OP

S D

ATA

4.0172

OPS DATASEP 04 001

4 – OPS DATA

COMMENTS :

- T/O SPEEDS COMPUTATIONValid for non limiting runways only

- LANDING SPEEDS COMPUTATIONThe approach speeds have been computed with 1.23 VS1G oflanding configuration or VMCL, whichever is higher

- GROSS CEILING COMPUTATION

For operational reasons, gross ceilings have been established withCG position : 25%

Eng : PW124/PW127

4.1172

OPS DATASEP 04 001

TAKE OFF TORQUE COMPUTED FOR VC = 50. KT

SAT (oC) PROPELLER SPEED 100 %

PRESSURE ALTITUDE (FT)AIRCOND.

OFF

1250$/

AIRCOND.

ON

HIGHAIR

COND.ON

-1000. 0. 1000. 2000. 3000. 4000. 5000. 6000. 7000. 8000. 8500.

- 40.- 10.- 8.- 6.- 4.

- 63.- 27.- 24.- 22.- 19.

90.090.090.090.090.0

90.090.090.090.090.0

90.090.090.090.090.0

90.090.090.090.090.0

90.090.090.090.090.0

90.090.090.090.090.0

90.090.090.090.090.0

90.090.090.090.090.0

90.090.090.090.090.0

90.090.090.090.089.0

90.090.089.288.287.2

- 2. 0. 2. 4. 6.

- 17.- 14.- 12.- 10.- 7.

90.090.090.090.090.0

90.090.090.090.090.0

90.090.090.090.090.0

90.090.090.090.090.0

90.090.090.090.090.0

90.090.090.090.090.0

90.090.090.090.090.0

90.090.090.090.090.0

90.090.089.688.587.4

88.087.085.984.983.8

86.285.184.183.182.1

8.10.12.14.16.

- 5.- 2. 0. 3. 5.

90.090.090.090.090.0

90.090.090.090.090.0

90.090.090.090.090.0

90.090.090.090.090.0

90.090.090.090.090.0

90.090.090.090.090.0

90.090.090.090.088.9

90.088.987.886.585.2

86.385.384.283.081.7

82.881.780.779.578.4

81.180.079.077.976.7

18.20.22.24.26.

8. 10. 13. 15. 18.

90.090.090.090.090.0

90.090.090.090.090.0

90.090.090.090.090.0

90.090.090.090.090.0

90.090.090.089.888.0

90.089.587.886.184.5

87.485.884.282.681.0

83.982.380.879.377.7

80.478.977.576.074.5

77.175.774.372.971.4

75.574.172.771.369.9

28.30.32.34.36.

20. 23. 25. 28. 30.

90.090.090.090.090.0

90.090.090.090.090.0

90.090.090.088.386.6

89.988.286.584.883.1

86.384.783.081.479.8

82.881.279.778.176.5

79.577.976.474.973.4

76.274.873.371.970.4

73.171.770.368.967.5

70.168.767.466.164.7

68.667.366.064.763.4

38.40.42.44.46.

33. 36. 38. 41. 43.

90.090.088.286.384.4

88.386.584.782.981.1

84.883.181.379.677.9

81.479.778.176.474.7

78.176.574.973.371.7

75.073.471.970.468.8

71.970.469.067.5

69.067.666.2

66.164.8

63.4 62.1

48.50.52.54.55.

46. 48. 51. 53. 54.

82.680.778.876.976.0

79.377.575.773.973.0

76.174.472.7

73.171.4

70.1

The part in bolt is the flat rated zone ; engine mechanical limit.

The part below is the area where the thermodynamical limit is reached first.

Note : Applicable for 0 < Vc < 60 kt

Eng : PW124

4.1272

OPS DATASEP 04 001

RESERVE TAKE OFF TORQUE COMPUTED FOR Vc = 50 KT

SAT (oC) PROPELLER SPEED 100 %


OFF

1250$/

AIRCOND.

ON

HIGHAIR

COND.ON

-1000. 0. 1000. 2000. 3000. 4000. 5000. 6000. 7000. 8000. 8500.

- 40.- 10.- 8.- 6.- 4.

- 63.- 27.- 24.- 22.- 19.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.98.9

100.100.99.198.096.9

- 2. 0. 2. 4. 6.

- 17.- 14.- 12.- 10.- 7.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.100.

100.100.99.698.497.2

97.896.695.594.393.1

95.794.693.592.391.2

8.10.12.14.16.

- 5.- 2. 0. 3. 5.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.98.7

100.98.897.596.194.7

95.994.793.592.290.8

92.090.889.788.487.1

90.188.987.886.585.3

18.20.22.24.26.

8. 10. 13. 15. 18.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.99.797.8

100.99.497.695.793.8

97.295.493.691.890.0

93.291.589.888.186.3

89.487.786.184.482.8

85.784.182.581.079.4

83.982.380.879.377.7

28.30.32.34.36.

20. 23. 25. 28. 30.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.98.296.2

99.998.096.194.292.3

95.994.192.390.488.6

92.090.388.586.885.0

88.386.684.983.381.6

84.783.181.579.878.2

81.279.778.176.675.0

77.876.474.973.471.9

76.274.873.371.970.4

38.40.42.44.46.

33. 36. 38. 41. 43.

100.100.98.095.993.8

98.196.194.192.190.1

94.292.390.488.486.5

90.588.686.784.983.0

86.885.083.381.579.7

83.381.679.978.276.5

79.978.376.675.0

76.675.173.5

73.572.0

70.5 69.0

48.50.52.54.55.

46. 48. 51. 53. 54.

91.789.687.685.584.5

88.186.184.182.181.1

84.682.780.8

81.279.4

77.9



Note : Applicable for 0 < Vc < 60 kt

Eng : PW124

4.1372

OPS DATASEP 04 001

GO AROUND TORQUE APPLICABLE FOR 0 ≤ Vc ≤ 125 kt

TAT (oC) PROPELLER SPEED 100. %


OFF

1250$/

AIRCOND.

ON

HIGHAIR

COND.ON

-100.0. 0. 100.0. 2000. 3000. 4000. 5000. 6000. 7000. 8000. 8500.

- 40.- 10.- 8.- 6.- 4.

- 63.- 27.- 24.- 22.- 19.

- 71.- 35.- 32.- 30.- 27.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.99.2

100.100.99.398.297.1

- 2. 0. 2. 4. 6.

- 17.- 14.- 12.- 10.- 7.

- 25.- 22.- 19.- 17.- 14.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.100.

100.100.99.898.697.4

98.096.995.794.693.4

96.094.893.792.691.4

8.10.12.14.16.

- 5.- 2. 0. 3. 5.

- 12.- 9.- 7.- 4.- 1.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.99.0

100.99.097.896.495.0

96.295.093.892.591.1

92.291.189.988.787.4

90.389.288.086.885.5

18.20.22.24.26.

8. 10. 13. 15. 18.

2. 4. 7. 10. 13.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.100.98.2

100.99.897.996.194.2

97.595.794.092.290.4

93.591.890.188.486.7

89.788.186.484.883.2

86.084.582.981.379.7

84.282.781.279.678.1

28.30.32.34.36.

20. 23. 25. 28. 30.

16. 18. 21. 24. 27.

100.100.100.100.100.

100.100.100.100.100.

100.100.100.98.596.5

100.98.496.594.692.7

96.394.492.890.889.0

92.490.688.987.185.4

88.687.085.383.681.9

85.083.481.880.278.6

81.580.078.576.975.4

78.276.775.273.872.3

76.675.173.772.270.8

38.40.42.44.46.

33. 36. 38. 41. 43.

30. 32. 35. 38. 41.

100.100.98.396.394.2

98.596.594.592.590.5

94.692.690.788.886.9

90.889.087.185.383.4

87.285.483.681.880.1

83.781.980.278.576.8

80.378.677.075.473.7

77.075.473.972.3

73.872.370.8

70.869.4

69.367.9

48.50.52.54.56.

46. 48. 51. 53. 55.

43. 46. 49. 52. 54.

92.190.087.985.983.8

88.586.584.582.580.5

84.983.081.179.2

81.679.777.9

78.376.5

75.1



Note : Add 0.8% for each 10 kt above 125 kt without exceeding 100% torque

Eng : PW124

4.3172

OPS DATASEP 04 010

13 tSpeeds Normal Icing

NON LIMITING RWYTAKE-OFFFLAPS 15

V1 = VRV2

100105

100105

FINAL TAKE OFF 108(Flaps 0)

107(Flaps 15)

DRIFT DOWN 107(Flaps 15)

MINI EN ROUTEVmLB 108

(Flaps 0) 132(Flaps 0)

FINALAPPROACH

VmHB(Flaps 30) 87 92

MAX CRUISE 2 ENGINES∆ ISA

FLIGHTLEVEL -10 -5 0 +5 +10 +15 +20

80100.2 102.3

438 413252 245275 267

101.1 102.3443 416252 244278 269

101.2 102.3446 418251 243279 270

99.1 102.3442 421248 242279 272

93.4 102.3426 423242 241274 273

88.3 96.9412 408236 235270 269

83.4 91.6396 392230 229266 264

100101.2 102.3

431 403251 243282 273

101.2 102.3434 406250 242284 274

100.5 102.3434 408249 241285 276

95.2 102.3418 411243 239281 277

89.8 98.2402 400236 235276 274

84.8 92.9388 386230 230271 270

80.1 87.9375 372225 224267 266

120101.2 102.3

427 397249 240288 278

100.1 102.3425 399247 239289 280

95.6 102.3409 402242 238286 281

91.1 99.3395 393237 235282 280

86.2 94.0380 378231 229278 276

81.3 88.9366 364225 224273 272

76.8 84.1354 351219 218269 267

14098.0 102.3412 396243 238290 284

94.5 102.3398 397240 236289 285

90.8 98.5385 384235 232287 283

86.5 94.2371 370230 228283 280

82.4 89.8359 357225 223279 277

77.9 85.0346 343219 218274 273

73.5 80.3334 331214 213270 269

16091.8 99.8385 386235 233289 287

88.9 96.5373 374232 229288 285

85.5 93.0361 361228 225286 283

82.0 89.1349 348224 221284 280

78.2 85.2337 336219 217280 277

74.4 81.1326 324213 212276 274

70.3 76.8314 312208 207271 270

18085.8 93.2359 360227 225288 286

83.1 90.4348 349224 222287 284

80.4 87.3338 338220 218286 282

77.3 84.1327 327217 214284 280

74.0 80.5316 315212 210280 277

70.6 77.0306 305207 205277 274

67.1 73.1296 294202 201272 270

20079.9 86.9333 336219 217287 285

77.5 84.2324 325216 214286 283

75.0 81.7314 316213 210284 282

72.6 78.8306 306209 207283 280

69.7 75.8296 296205 203280 277

66.7 72.5287 286200 198276 274

63.5 69.3278 276195 194272 270

22074.1 80.7310 313211 209285 283

72.0 78.3302 303208 206284 282

69.9 76.0293 294204 202283 280

67.6 73.6285 286201 199281 278

65.3 70.9277 277197 195279 276

62.7 68.2268 268193 191275 273

59.9 65.2260 259188 186271 269

24068.7 74.7290 292202 201283 281

66.7 72.6282 284199 198282 280

64.8 70.4274 275196 194280 278

62.8 68.3266 267193 191279 276

60.8 66.1259 260189 187277 274

58.5 63.6252 251185 183273 270

56.2 61.1244 244181 179270 266

25066.1 71.8281 283198 197282 280

64.2 69.8272 275195 193280 279

62.3 67.8265 267192 190279 277

60.4 65.7258 258188 186277 274

58.5 63.6251 251185 183275 272

56.5 61.4244 244181 179272 269

54.3 59.0237 236177 174269 265

TQ % NP = 86 % TQ % NP = 77 %KG/H/ENG KG/H/ENGIAS IASTAS TAS

127�7+(502�/,0,7('

Mod : 1368 Eng : PW124

4.3272

OPS DATASEP 04 010



V1 = VRV2

100105

100105


111(Flaps 15)




FINALAPPROACH



FLIGHTLEVEL -10 -5 0 +5 +10 +15 +20

80100.5 102.3

439 413252 244275 267

101.2 102.3444 416252 243278 268

101.2 102.3447 418251 243279 270

99.1 102.3442 421248 242278 271

93.4 102.3426 423241 241273 273

88.3 96.9412 408236 235269 268

83.4 91.6396 392230 229265 264

100101.2 102.3

431 404251 243282 273

101.2 102.3434 406250 242284 274

100.4 102.3434 408248 240285 275

95.2 102.3418 411242 239280 277

89.8 98.1403 400236 235275 274

84.7 92.9389 386230 229271 270

80.1 87.8375 372225 223267 265

120101.2 102.3

427 397249 240288 278

100.1 102.3425 400247 239289 279

95.6 102.3409 402242 238285 281

91.0 99.2395 393236 234282 279

86.1 94.0380 378230 229277 275

81.2 88.8367 364224 223272 271

76.7 84.1354 351219 218268 267

14098.0 102.3412 396243 237290 283

94.4 102.3398 398239 236288 285

90.7 98.5385 384235 232286 282

86.5 94.2371 370230 227283 280

82.4 89.8359 357225 223279 276

77.8 85.0346 343219 217274 272

73.4 80.3334 331213 212269 268

16091.7 99.8384 386235 233289 286

88.8 96.4373 373231 229288 284

85.5 92.9361 361228 225286 282

82.0 89.1349 348223 221283 280

78.2 85.2337 336218 216279 277

74.4 81.0326 324213 211275 273

70.3 76.7314 312207 206271 269

18085.7 93.1358 360227 225288 285

83.0 90.3348 349223 221287 284

80.3 87.2338 338220 217285 282

77.2 84.0327 327216 213283 279

74.0 80.4316 315211 209280 277

70.5 76.9306 305206 205276 273

67.0 73.0296 294201 200271 269

20079.8 86.8333 336218 217286 284

77.4 84.1324 325215 213285 282

74.9 81.6314 315212 210284 281

72.5 78.7306 305209 206282 278

69.6 75.7296 295204 202279 276

66.6 72.4286 285199 197275 273

63.4 69.2278 276194 193271 269

22074.0 80.5310 312210 208284 282

71.9 78.2301 303207 205283 281

69.7 75.8293 294204 202282 279

67.5 73.5285 286200 198280 277

65.2 70.8277 276196 194277 274

62.5 68.0268 268192 190274 271

59.8 65.0260 259187 185270 267

24068.5 74.5289 292201 200281 280

66.6 72.4281 283198 197280 278

64.7 70.3274 275195 193279 276

62.7 68.1266 267192 190277 274

60.6 65.9259 259188 186275 271

58.4 63.4252 251184 181271 268

56.1 60.9244 244179 177268 264

25066.0 71.6281 282197 196280 279

64.0 69.6272 274194 192279 277

62.2 67.6265 266191 189277 275

60.3 65.5258 258187 185275 272

58.3 63.4250 251183 181273 269

56.4 61.1244 244180 177270 266

54.1 58.8237 236175 172266 262


127�7+(502�/,0,7('

Mod : 1368 Eng : PW124

4.3372

OPS DATASEP 04 010



V1 = VRV2

100105

100105


115(Flaps 15)




FINALAPPROACH



FLIGHTLEVEL -10 -5 0 +5 +10 +15 +20

80100.8 102.3

440 414252 244275 267

101.2 102.3444 416252 243277 268

101.2 102.3447 419251 242279 270

99.1 102.3442 421248 241278 271

93.4 102.3426 423241 240273 272

88.3 96.8412 408235 234269 268

83.3 91.5396 391230 229265 263

100101.2 102.3

432 404251 242282 273

101.2 102.3434 406250 241283 274

100.4 102.3434 409248 240284 275

95.2 102.3418 411242 239280 276

89.7 98.1403 400236 234275 274

84.7 92.8389 386230 229271 269

80.0 87.8375 372224 223266 265

120101.2 102.3

427 397248 240287 278

100.0 102.3425 400247 239288 279

95.5 102.3409 402241 237285 280

91.0 99.2395 393236 234281 279

86.1 93.9380 378230 228277 275

81.2 88.8367 364224 223272 271

76.7 84.0354 351218 217268 266

14097.9 102.3412 396243 237290 283

94.4 102.3398 398239 236288 284

90.7 98.4385 384235 232286 282

86.4 94.1371 370229 227282 279

82.3 89.7359 357224 222278 276

77.8 84.9346 343218 217273 272

73.4 80.2334 331213 211269 267

16091.7 99.7384 386235 232289 286

88.7 96.4373 373231 228287 284

85.4 92.8361 361227 224285 282

81.9 89.0349 347223 220282 279

78.1 85.1337 336217 215278 276

74.3 81.0326 324212 211274 272

70.2 76.6315 312207 205270 268

18085.6 93.0358 360226 224287 285

82.9 90.2348 349223 220286 283

80.3 87.1338 338219 217284 281

77.1 83.9327 327215 213282 278

73.9 80.3316 315211 208278 275

70.4 76.8306 305205 204274 272

66.9 72.9296 294200 199270 268

20079.7 86.6333 335218 216285 283

77.3 84.0323 325214 212284 281

74.8 81.4314 315211 209283 280

72.4 78.5305 305208 205281 277

69.5 75.6296 295203 201278 275

66.5 72.3286 285198 196273 271

63.3 69.0278 276193 191270 267

22073.9 80.4309 312209 208283 281

71.8 78.0301 303206 204282 279

69.6 75.7293 293203 200280 277

67.4 73.3284 285199 197279 275

65.0 70.6277 276195 193276 272

62.4 67.9268 267190 188272 269

59.7 64.9260 259186 183268 264

24068.4 74.3289 291200 199280 278

66.4 72.2281 283197 195279 277

64.5 70.1273 274194 192277 274

62.5 67.9266 266190 188275 272

60.4 65.7259 259186 184272 269

58.2 63.2252 251182 179269 265

55.9 60.7244 244178 174265 261

25065.8 71.4280 282196 194279 277

63.8 69.4271 274192 191277 275

62.0 67.4264 266189 187275 273

60.1 65.2257 257186 183273 269

58.1 63.1250 251182 179270 266

56.2 60.9244 243178 174267 262

53.9 58.5237 236173 170263 258


127�7+(502�/,0,7('

Mod : 1368 Eng : PW124

4.3472

OPS DATASEP 04 010



V1 = VRV2

100105

100105


120(Flaps 15)




FINALAPPROACH



FLIGHTLEVEL -10 -5 0 +5 +10 +15 +20

80101.1 102.3

441 414252 244275 266

101.2 102.3444 416251 243277 268

101.2 102.3447 419250 242278 269

99.0 102.3442 421247 241278 271

93.4 102.3426 423241 240273 272

88.3 96.8412 408235 234269 267

83.3 91.5396 391229 228264 263

100101.2 102.3

432 404250 242281 272

101.2 102.3434 406249 241283 273

100.4 102.3434 409248 240284 275

95.1 102.3418 411242 238279 276

89.7 98.1403 400235 234274 273

84.7 92.8389 386229 228270 269

80.0 87.7375 372224 222266 264

120101.2 102.3

427 398248 239287 277

100.0 102.3424 400246 238288 279

95.5 102.3409 402241 237285 280

90.9 99.1395 393236 233281 278

86.1 93.9380 378229 228276 274

81.2 88.7367 364223 222271 270

76.6 84.0354 351218 216267 265

14097.9 102.3412 396242 237289 282

94.3 102.3398 398238 235287 284

90.6 98.4385 384234 231285 281

86.4 94.0371 370229 226281 278

82.2 89.6359 357223 221277 275

77.7 84.8346 344217 216272 271

73.3 80.1334 331212 210268 266

16091.6 99.6384 386234 232288 285

88.7 96.3372 373231 228287 283

85.3 92.7361 361227 224284 281

81.8 88.9349 347222 219281 278

78.0 85.0337 336217 215277 275

74.2 80.9326 324211 210273 271

70.1 76.5315 312206 204269 267

18085.5 92.9358 360226 223286 284

82.8 90.1347 348222 220285 282

80.2 87.0337 337219 216283 280

77.0 83.7327 326214 212281 277

73.8 80.2316 315210 207277 274

70.3 76.7306 305204 203273 271

66.9 72.8296 294199 197269 266

20079.5 86.5332 335217 215284 282

77.1 83.8323 324214 211283 280

74.7 81.3314 315210 208281 278

72.2 78.4305 305207 204279 276

69.3 75.4296 295202 200276 273

66.3 72.1286 285197 195272 269

63.2 68.9278 276192 190268 265

22073.7 80.2309 312208 206282 280

71.6 77.9301 302205 203280 278

69.5 75.5292 293201 199279 276

67.2 73.1284 285198 195277 273

64.8 70.4276 276193 191273 270

62.2 67.7268 267189 186270 266

59.5 64.7260 259184 181266 261

24068.2 74.1289 291199 197278 276

66.2 72.0280 282196 194277 274

64.3 69.8273 274192 190275 272

62.3 67.6265 266189 186273 269

60.2 65.4258 259185 182270 266

58.0 62.9251 251180 177267 261

55.7 60.4244 243176 172262 256

25065.6 71.1280 281194 193276 275

63.6 69.1271 273191 189275 272

61.7 67.1264 265187 185273 270

59.9 64.9257 257184 181271 266

57.9 62.8250 250180 176268 262

55.9 60.5243 243176 171264 258

53.7 58.2236 236171 166260 253


127�7+(502�/,0,7('

Mod : 1368 Eng : PW124

4.3572

OPS DATASEP 04 010



V1 = VRV2

100105

104108


124(Flaps 15)




FINALAPPROACH



FLIGHTLEVEL -10 -5 0 +5 +10 +15 +20

80101.2 102.3

442 414252 243275 266

101.2 102.3444 416251 242277 267

101.2 102.3447 419250 242278 269

99.0 102.3442 421247 241277 270

93.3 102.3426 424240 240272 271

88.2 96.8412 409235 233268 267

83.3 91.5396 391229 227264 262

100101.2 102.3

432 404250 242281 272

101.2 102.3434 406249 240283 273

100.3 102.3434 409247 239283 274

95.1 102.3418 411241 238279 275

89.7 98.0403 400235 233274 272

84.6 92.7389 386229 228269 268

80.0 87.7375 371223 221265 263

120101.2 102.3

427 398248 239287 277

99.9 102.3424 400246 238287 278

95.4 102.3409 402241 237284 279

90.9 99.1395 393235 233280 277

86.0 93.8380 378229 227275 273

81.1 88.7367 364223 221270 269

76.6 83.9354 351217 215266 264

14097.8 102.3411 396242 236289 282

94.2 102.3398 398238 235287 283

90.5 98.3385 384234 230284 281

86.3 94.0371 370228 226280 277

82.1 89.5359 357223 221276 274

77.7 84.8346 344217 215271 270

73.3 80.1334 331211 209267 265

16091.5 99.5384 386233 231287 284

88.6 96.2372 373230 227286 282

85.2 92.6361 361226 223284 280

81.7 88.8349 347221 218280 277

77.9 84.9337 336216 214276 274

74.2 80.8326 324210 209272 270

70.1 76.4315 313205 203267 265

18085.4 92.8358 360225 223285 283

82.7 89.9347 348221 219284 281

80.0 86.8337 337218 215282 279

76.9 83.6327 326213 211279 276

73.6 80.1316 315208 206276 273

70.2 76.5306 305203 201271 269

66.8 72.7296 294198 196267 264

20079.4 86.3332 335216 214283 281

77.0 83.7323 324213 210282 279

74.6 81.1313 314209 207280 277

72.1 78.2305 305205 203278 274

69.2 75.3295 295200 198274 271

66.2 72.0286 285196 193270 267

63.1 68.7278 276191 188266 262

22073.6 80.0308 311207 205280 278

71.5 77.6300 302203 201279 276

69.3 75.2292 293200 198277 274

67.0 72.9284 285196 194274 271

64.7 70.2276 276192 189271 267

62.1 67.4268 267187 184267 263

59.3 64.4260 259182 179263 258

24068.0 73.8288 290197 196276 274

66.0 71.7280 282194 192275 272

64.1 69.5272 273190 188273 269

62.0 67.3265 265187 183270 265

60.0 65.1258 258183 179267 262

57.8 62.6251 250178 174263 257

55.5 60.1244 243173 168259 251

25065.3 70.8279 280192 191274 272

63.3 68.7270 272189 187272 269

61.5 66.7263 264185 182270 266

59.6 64.5256 256182 178267 262

57.6 62.4249 249178 173264 258

55.7 60.1243 242173 168260 252

53.4 57.7236 235168 162255 246


127�7+(502�/,0,7('

Mod : 1368 Eng : PW124

4.3772

OPS DATASEP 04 010



V1 = VRV2

107111

111115


131(Flaps 15)




FINALAPPROACH



FLIGHTLEVEL -10 -5 0 +5 +10 +15 +20

80101.2 102.3

442 414251 242274 265

101.2 102.3445 417250 241276 266

101.2 102.3447 419249 240277 267

98.9 102.3442 422246 239276 269

93.2 102.2426 424239 238271 270

88.1 96.6412 409234 232267 265

83.2 91.3396 391227 226262 260

100101.2 102.3

432 404249 241280 271

101.2 102.3435 407248 239282 272

100.2 102.3434 409246 238282 273

95.0 102.3418 412240 237277 274

89.6 97.9403 400233 232272 271

84.5 92.6389 386227 226268 266

79.9 87.5375 371221 220263 261

120101.2 102.3

428 398247 238286 275

99.8 102.3424 401245 237286 277

95.2 102.3408 403239 235282 278

90.7 98.9395 393233 231278 276

85.8 93.6380 378227 226273 271

81.0 88.5367 364221 219269 267

76.5 83.7354 351215 213264 261

14097.6 102.3411 397241 235287 280

94.1 102.1398 398237 234285 282

90.3 98.0385 383232 229282 279

86.1 93.7371 370226 224278 275

81.9 89.3359 357221 219274 272

77.5 84.5346 344215 213269 267

73.1 79.8334 332209 207264 261

16091.2 99.2383 385232 229285 282

88.3 95.9372 372228 225284 280

85.0 92.3360 360224 221281 278

81.5 88.5349 347219 216278 274

77.6 84.6337 336213 211273 271

73.9 80.5326 324208 206269 266

69.9 76.1315 313202 200264 261

18085.1 92.4357 359223 221283 280

82.4 89.6346 347219 217281 278

79.7 86.5336 337216 212279 276

76.5 83.2326 326211 208276 273

73.4 79.7316 315206 203272 269

69.9 76.1306 305201 198268 264

66.5 72.3297 295195 192263 259

20079.0 85.9331 334214 211280 277

76.6 83.2322 323210 207278 275

74.2 80.6313 314206 204276 273

71.7 77.8304 304202 199273 270

68.8 74.7295 294197 194270 265

65.9 71.5286 285192 188265 260

62.7 68.2278 276187 182260 255

22073.1 79.4307 310204 202276 274

71.0 77.1299 301200 198274 271

68.8 74.6291 291197 193272 268

66.5 72.2283 283192 189269 264

64.2 69.5275 275188 183266 259

61.6 66.7267 267183 178261 254

58.9 63.7260 258177 171256 247

24067.4 73.1286 288193 191271 268

65.4 70.9278 280190 186269 264

63.5 68.7271 271186 182266 260

61.4 66.4263 263182 176263 255

59.3 64.1257 257177 171259 250

57.2 61.6250 249172 165254 244

54.8 59.2243 242166 159248 238

25064.7 69.9277 278188 185268 264

62.7 67.8268 270184 180265 260

60.8 65.7261 262180 175262 255

58.9 63.4254 254175 169259 249

56.8 61.3248 247170 163254 244

54.9 59.2242 241165 159249 239

52.7 56.8235 234159 152242 231


127�7+(502�/,0,7('

Mod : 1368 Eng : PW124

4.3872

OPS DATASEP 04 040



V1 = VRV2

111114

115118


135(Flaps 15)




FINALAPPROACH



FLIGHTLEVEL -10 -5 0 +5 +10 +15 +20

80101.2 102.3

442 415250 242273 264

101.2 102.3445 417249 241275 265

101.2 102.3448 420249 240277 267

98.8 102.3442 422245 239275 268

93.2 102.1427 424239 238270 269

88.1 96.6412 409233 231266 264

83.1 91.2396 391227 225261 259

100101.2 102.3

433 405249 240280 270

101.2 102.3435 407248 239281 271

100.1 102.3434 410246 237281 272

94.9 102.3418 412239 236277 273

89.5 97.8403 400233 231272 270

84.4 92.5389 386227 225267 265

79.8 87.4375 371221 218262 260

120101.2 102.3

428 399246 237285 275

99.7 102.3424 401244 236285 276

95.1 102.3408 403238 235282 277

90.6 98.8395 393233 230277 275

85.8 93.5381 378226 225272 270

80.9 88.4367 364220 218267 265

76.4 83.6354 351214 212262 260

14097.5 102.3411 397240 234286 280

93.9 102.0397 398236 233284 280

90.2 97.9385 383231 228281 278

86.0 93.6371 370225 223277 274

81.8 89.2359 357219 217272 270

77.4 84.4346 344214 211268 265

73.0 79.7334 331208 205262 259

16091.1 99.0383 385231 228284 281

88.2 95.7371 372227 224283 279

84.8 92.1360 360223 220280 276

81.3 88.4348 347217 215276 273

77.5 84.4337 336212 210272 269

73.8 80.3326 324207 204267 264

69.7 76.0315 313201 197262 258

18084.9 92.2356 358222 219282 279

82.2 89.3346 347218 215280 276

79.5 86.3336 336214 211277 274

76.3 83.0326 325209 206274 270

73.2 79.5315 314204 201270 266

69.8 75.9306 305199 195266 261

66.4 72.1297 294193 189260 255

20078.8 85.6331 333212 210278 275

76.4 82.9322 323208 206276 273

73.9 80.3312 313204 201274 270

71.4 77.4304 304200 197271 266

68.6 74.4295 294195 191267 262

65.7 71.2286 285190 185263 256

62.5 67.8278 276184 179257 249

22072.8 79.1306 309202 200274 271

70.7 76.7298 300198 195272 267

68.5 74.2290 290194 190269 264

66.2 71.8282 283190 186266 260

63.9 69.0275 274185 180262 254

61.3 66.2267 266180 173257 248

58.6 63.3260 258174 167251 241

24067.1 72.5286 287191 188268 263

65.0 70.3277 278187 183265 259

63.1 68.0270 270183 177262 254

61.0 65.7262 262178 171258 248

58.9 63.5256 256173 166253 243

56.8 61.2250 248167 160248 237

54.3 58.6242 241161 152240 228

25064.4 69.3276 276185 181264 258

62.2 67.1267 268181 175261 253

60.3 64.9260 260176 169257 247

58.4 62.8253 253171 164252 242

56.3 60.7247 247165 158247 236

54.3 58.4241 240160 151241 227

51.9234150229


127�7+(502�/,0,7('

Mod : 1368 + 2735 Eng : PW124

4.3972

OPS DATASEP 04 040



V1 = VRV2

114117

118121


138(Flaps 15)




FINALAPPROACH



FLIGHTLEVEL -10 -5 0 +5 +10 +15 +20

80101.2 102.3

443 415250 241273 263

101.2 102.3445 418249 240274 265

101.2 102.3448 420248 239276 266

98.8 102.3442 422244 238274 267

93.1 102.0427 424238 237270 268

88.0 96.5412 409232 230265 263

83.0 91.1395 391226 224260 258

100101.2 102.3

433 405248 239279 269

101.2 102.3435 408247 238280 270

100.0 102.3434 410245 237281 271

94.8 102.3418 412238 235276 272

89.4 97.7403 400232 230271 269

84.4 92.4389 386226 224266 263

79.7 87.3375 371219 217261 258

120101.2 102.3

428 399246 236285 274

99.6 102.3424 401243 235284 275

95.0 102.3408 403237 234280 276

90.5 98.7394 393232 229276 274

85.7 93.4381 378225 223271 269

80.8 88.3367 365219 217266 263

76.3 83.5354 351213 210261 258

14097.3 102.3410 398239 233286 279

93.8 101.8397 397235 232283 279

90.0 97.8384 383230 227280 276

85.8 93.4370 370224 222275 272

81.7 89.1359 357218 216271 268

77.3 84.3346 344212 210266 263

72.9 79.6334 331206 203261 257

16090.9 98.8383 384230 227283 280

88.0 95.5371 372226 223281 277

84.6 91.9360 360221 218278 274

81.2 88.2348 347216 213274 271

77.4 84.2337 336211 208270 266

73.7 80.2326 324205 202265 261

69.6 75.8315 312199 195260 255

18084.7 92.0356 358221 218280 277

82.0 89.1345 346217 214278 274

79.2 86.0336 336212 209275 271

76.2 82.7325 325207 204272 268

73.0 79.2315 314202 199268 263

69.6 75.6306 305197 193263 258

66.2 71.8297 294191 186258 251

20078.5 85.3330 332210 208276 273

76.2 82.6321 322207 204274 270

73.6 79.9311 312202 199271 267

71.2 77.1303 303198 194268 262

68.3 74.0294 294193 188264 257

65.4 70.7286 285187 181259 251

62.2 67.4277 275181 174252 244

22072.5 78.6305 308200 197271 267

70.4 76.2298 299196 192269 263

68.2 73.7289 289192 187266 259

65.9 71.2281 282187 181262 254

63.6 68.5275 274182 175258 247

60.9 65.8267 265176 169252 241

58.2 62.9259 257169 162244 234

24066.7 71.9284 285188 183264 257

64.6 69.6276 277184 178260 252

62.6 67.3269 268179 171257 246

60.5 65.1261 261174 166252 241

58.3 62.8255 254168 160246 234

56.2 60.2249 247161 151239 224

53.4241149223

25063.9 68.5275 274182 176259 251

61.7 66.3266 266176 169255 244

59.7 64.3259 259171 164250 240

57.8 62.0252 251166 157245 232

55.6 59.5245 245158 147236 219

53.1239146221


127�7+(502�/,0,7('

Mod : 1368 + 2735 Eng : PW124

4.4072

OPS DATASEP 04 040

21.5 tSpeeds Normal Icing


V1 = VRV2

115118

120123


140(Flaps 15)




FINALAPPROACH



FLIGHTLEVEL -10 -5 0 +5 +10 +15 +20

80101.2 102.3

443 415250 241273 263

101.2 102.3445 418249 240274 264

101.2 102.3448 420248 239275 266

98.7 102.3442 423244 238274 267

93.1 102.0427 424238 236269 268

88.0 96.4412 409232 230265 262

83.0 91.1395 391225 223260 257

100101.2 102.3

433 405248 239278 268

101.2 102.3435 408247 238280 270

99.9 102.3434 410244 236280 271

94.7 102.3418 413238 235275 272

89.4 97.6403 400231 230270 268

84.3 92.3389 386225 223265 263

79.7 87.3375 371219 216260 257

120101.2 102.3

428 399245 236284 273

99.5 102.3424 401243 235284 274

95.0 102.3408 404237 233280 276

90.4 98.6394 393231 229275 273

85.6 93.4381 378225 223270 268

80.8 88.2367 365218 216265 263

76.2 83.4354 351212 209260 257

14097.3 102.3410 398239 233285 278

93.7 101.7397 397235 231283 279

89.9 97.7384 383229 226279 275

85.7 93.3370 370223 221274 272

81.6 89.0359 357218 215270 267

77.3 84.2346 344212 209265 262

72.8 79.5334 331205 202260 255

16090.8 98.7382 384230 227282 279

87.9 95.4371 372226 222281 276

84.5 91.8359 359221 218277 273

81.1 88.0348 347215 212273 270

77.3 84.1337 335210 207269 265

73.6 80.0326 325204 201264 260

69.5 75.7315 312198 194258 253

18084.6 91.8356 357220 217279 276

81.9 88.9345 346216 213277 273

79.1 85.9335 336211 208274 270

76.0 82.6325 325206 203270 266

72.9 79.1315 314201 197267 261

69.5 75.4306 305196 191262 256

66.1 71.7297 294189 184256 248

20078.4 85.1330 332210 207275 272

76.0 82.4321 321206 202273 268

73.5 79.7311 312201 198270 265

71.1 76.9303 303197 192267 260

68.2 73.8294 294192 186262 255

65.3 70.5286 284186 179257 248

62.1 67.3277 274179 172250 241

22072.3 78.4305 307199 195269 265

70.2 75.9297 298195 190267 261

68.0 73.4289 289190 185264 256

65.7 70.9281 281186 179260 250

63.4 68.2274 273180 172255 244

60.7 65.5266 265174 166248 238

58.0 62.5259 256167 158241 228

24066.5 71.5284 284186 181261 254

64.3 69.2275 276182 175258 248

62.3 67.0268 268177 169253 243

60.2 64.7261 260171 163248 236

58.0 62.3254 253165 155241 227

55.6248155230

25063.6 68.0274 273180 172256 246

61.4 65.9265 265174 167251 241

59.4 63.7258 258169 160246 234

57.3 61.3251 250161 151238 223

54.9244151225


127�7+(502�/,0,7('

Mod : 1368 + 2735 Eng : PW124

4.4172

OPS DATASEP 04 040

22 tNever exceed certified weight limitations

Speeds Normal Icing


V1 = VRV2

117120

121124


142(Flaps 15)




FINALAPPROACH



FLIGHTLEVEL -10 -5 0 +5 +10 +15 +20

80101.2 102.3

443 415249 240272 262

101.2 102.3445 418248 239274 264

101.2 102.3448 420247 238275 265

98.7 102.3442 423244 237274 266

93.1 101.9427 424237 236269 267

87.9 96.4412 408231 229264 262

83.0 91.0395 391225 222259 256

100101.2 102.3

433 405247 238278 268

101.2 102.3436 408246 237280 269

99.9 102.3434 410244 236279 270

94.7 102.3418 413237 235274 271

89.3 97.6403 401231 229270 267

84.3 92.2389 386225 222264 262

79.6 87.2375 371218 216259 256

120101.2 102.3

428 399245 235284 273

99.4 102.3424 402242 234283 274

94.9 102.3408 404236 233279 275

90.3 98.5394 393230 228275 272

85.6 93.3381 378224 222270 267

80.7 88.1367 365218 215265 262

76.2 83.3354 351211 208259 256

14097.2 102.3410 398238 232284 277

93.6 101.6397 397234 230282 278

89.8 97.6384 383229 226278 275

85.7 93.2370 369222 220274 271

81.6 88.9359 357217 214269 266

77.2 84.1346 344211 208264 260

72.8 79.4334 331204 201258 254

16090.7 98.6382 384229 226282 278

87.8 95.3371 372225 222280 276

84.4 91.7359 359220 217276 272

81.0 87.9348 347214 211272 268

77.2 84.0337 335209 206268 264

73.5 79.9326 325203 200263 258

69.4 75.5315 312197 192257 251

18084.5 91.7355 357219 216278 275

81.7 88.8345 346215 212276 272

79.0 85.7335 335210 207273 269

75.9 82.4325 325205 202269 264

72.8 78.9315 314200 196265 259

69.4 75.3306 304195 189260 253

65.9 71.5296 293188 182254 245

20078.2 84.9329 331208 206274 270

75.9 82.2320 321205 201271 266

73.4 79.5311 312200 196268 263

70.9 76.6303 303196 190265 258

68.0 73.5294 293190 184260 252

65.1 70.3286 283184 177254 244

61.9 67.1277 274177 170247 238

22072.1 78.1305 306197 193268 262

70.0 75.6297 297193 188265 258

67.8 73.0289 288189 182262 252

65.5 70.5281 281184 176257 246

63.1 67.9274 272178 170252 241

60.5 65.1266 264171 163245 233

57.7 61.9258 255162 151234 219

24066.2 71.1283 283184 178259 250

64.0 68.8275 275179 172255 244

62.0 66.6267 267174 166250 239

59.9 64.2260 259168 158244 230

57.5 61.0253 250159 142234 209

25063.3 67.7273 272177 170253 242

61.0 65.4264 264171 163247 236

58.9 63.1257 256164 154240 226

56.6250155229


127�7+(502�/,0,7('

Mod : 1368 + 2735 Eng : PW124

4.6172

OPS DATASEP 04 001

For weight in KG, use white boxes.For weight in LB, use shaded boxes.

SINGLE ENGINE GROSS CEILING (FT)

NORMAL CONDITIONS (FLAPS 0)

:(,*+7[��NJ ,6$�� ,6$ ,6$�� ,6$�� ,6$��

:(,*+7[��OE

��

��

��

��

��

��

��

��

��

��

��

Eng : PW124

R

4.6272

OPS DATASEP 05 040

For weight in KG, use white boxes.For weight in LB, use shaded boxes.

SINGLE ENGINE GROSS CEILING (FT)

ICING CONDITIONS (FLAPS 15)

WEIGHTx 1000 kg ISA - 10 ISA ISA + 10 ISA + 15 ISA + 20 WEIGHT

x 1000 lb

13.0 25000 25000 24800 24500 23500 23200 22800 22500 22200 21900 29

14.0 24100 24000 22700 22500 21300 21200 20700 20500 19800 19700 31

15.0 22000 22100 20600 20700 19200 19300 18500 18500 17600 17600 33

16.0 20000 20200 18600 18800 17200 17400 16300 16600 15600 15800 35

17.0 18100 18500 16700 17100 15200 15700 14400 14800 15100 15100 37

18.0 16400 16900 15000 15500 13400 13900 12700 13200 - 15100 39

19.0 14800 15400 13400 14000 11700 12400 12600 12600 - - 41

20.0 13300 14000 11900 12600 10000 10900 12600 12600 - - 43

21.0 11800 12700 10300 11200 10000 10000 - - - - 45

21.5 11100 11300 9500 9700 10000 10000 - - - - 47

22.0 10300 10300 8600 8600 10000 10000 - - - - 48.5

Note : When bolt-underligned figures, icing conditions do not exist.

R

Mod : 1368 + 2735 Eng : PW124

4.6372

OPS DATASEP 04 001

REDUCED FLAPSLANDING CONFIGURATION

VAPP (kt)NOTE : For a go around flaps 15 configuration increase speed up to VmLB0

before selecting flaps 0

FLAPS 0VmHB0 + 5 kt

FLAPS 15VmHB15

.*

WEIGHT(x 1000kg) Normal Icing Normal Icing

13 118 141 96 11214 122 145 99 11715 126 151 103 12216 130 156 106 12617 134 161 109 13018 138 165 113 13419 142 170 116 13720 146 174 119 14121 149 178 123 145

21.350 149 178 125 147

FLAPS 0VmHB0 + 5 kt

FLAPS 15VmHB15

/E

WEIGHT(x 1000Lb) Normal Icing Normal Icing

29 119 142 96 11331 122 146 99 11733 126 151 103 12235 130 156 106 12537 133 160 109 12939 137 164 112 13341 141 168 115 13743 144 173 118 14045 147 176 121 14347 150 179 124 146

Eng : PW127EEng : PW124

4.6472

OPS DATASEP 04 001

1.1 VMCA IAS * OAT °C

ZP (ft)-30 -20 -10 0 + 10 + 20 +30 + 40 + 50

0 105 105 104 103 102 102 101 99 95

2000 104 103 102 102 101 100 99 96 92

4000 103 102 101 100 100 98 96 92 89

6000 101 100 100 99 97 95 92 89 86

8500 99 98 97 95 93 91 88 85 82

* Conservative values calculated for the maximum landing weight.

Eng : PW124

R

4.65

72

OPS DATA SEP 10 600

PW127F / PW127M ACTUAL LANDING DISTANCE (M) - SEA LEVEL

NORMAL CONDITIONS - FLAPS 30 WEIGHT (1000 KG) 13 14 15 16 17 18 19 20 21 22 22.5 23

DRY 570 570 570 570 570 590 610 630 650 670 680 700

WET 690 690 690 690 700 730 760 780 810 840 850 860

WATER OR

SLUSH <1/2 in

640 680 710 750 780 820 860 900 940 980 1000 1020

COMPACT SNOW 690 720 760 790 830 860 900 930 970 1000 1020 1030 R

UN

WA

Y C

ON

DIT

ION

CO

NT

AM

INA

TE

D B

Y

ICE 1010 1070 1120 1170 1230 1280 1340 1390 1450 1500 1530 1560

ICING CONDITIONS – FLAPS 30

WEIGHT (1000 KG) 13 14 15 16 17 18 19 20 21 22 22.5 23

DRY 610 610 620 620 620 640 670 690 710 740 750 770

WET 760 760 760 760 770 800 830 860 890 920 940 950

WATER OR

SLUSH <1/2 in

700 740 780 820 860 900 950 990 1040 1080 1100 1130

COMPACT SNOW 760 800 840 880 920 960 1000 1040 1080 1120 1140 1160 R

UN

WA

Y C

ON

DIT

ION

CO

NT

AM

INA

TE

D B

Y

ICE 1140 1200 1260 1320 1390 1450 1520 1580 1640 1710 1740 1770

CORRECTION ON LANDING DISTANCES

-Wind : • dry or wet runway add 10% per 5 kt tailwind. subtract 2% per 5 kt headwind. • contaminated runway add 16% per 5 kt tailwind. subtract 2% per 5 kt headwind. -Airport elevation : • dry or wet runway add 3% per 1000 ft above sea level. • contaminated runway add 5% per 1000 ft above sea level.

-Effect of reverse : landing distances are decreased by : • 2% on dry runway. • 4% on wet runway. • 8% on runway contaminated by water or slush. • 10% on runway contaminated by compact snow. • 30 % on runway contaminated by ice.

CAUTION: On contaminated runway, performances without reverser only are to be used for flight preparation.

NOTE: Landing on damp runway.

A runway is damp when it is not perfectly dry, but when the water which is on it does not give it a shiny appearance. For damp runway, we consider no performance limitation.

Mod : 5561 Model : 212A

R

5.01

72

CHECK LIST L.T.R.

List of Temporary Revisions MAY 11 089

NO

TR EDITION DATE DESTROYED INSERTION

DATE REASON

01 MAR 07 AT REV 27 DATED SEP 07 TR 11 ENV

02 12DEC07 AT REV 28 DATED APR 08 MOD 5561

03 JUN 08 AT REV 29 DATED OCT 08 TR 13 ENV

04 31MAY10 AT REV 33 DATED SEP 10 Cockpit door

05 MAY 11 TR 16 ENV

5.05

72

CHECK LIST

L.N.R. List of Normal Revisions SEP 10 001

REV EDITION DATE

INSERTION DATE REMARKS

00 OCT 89

01 DEC 89

02 MAR 90

03 NOV 90

04 MAY 91

05 NOV 91

06 MAY 92

07 NOV 92 TOTAL EDITION

08 MAY 93 TOTAL EDITION

09 NOV 93 TOTAL EDITION

10 JUN 94

11 DEC 94

12 JUN 95

13 DEC 95

14 JUN 96

15 DEC 96

16 JUN 97

17 DEC 97

18 JUL 98

19 JUL 99

20 JUL 00

21 JUL 01

22 SEP 02

23 SEP 03

24 SEP 04 TOTAL WORD EDITION

25 SEP 05

26 SEP 06

27 SEP 07

28 APR 08

29 OCT 08

30 OCT 09

31 SEP 10

5.06

72

CHECK LIST

R.N.R. Reason of Normal Revisions SEP 10 001

REV EDITION DATE REASON FOR ISSUE CHAP

INVOLVED

31 SEP 10 EMERGENCY PROCEDURES AIR COND SMOKE: amber engine “caution”. RECOVERY AFTER STALL or ABNORMAL ROLL CONTROL: procedure reviewed. PROCEDURES FOLLOWING FAILURES Contents page updated. ENG NAC OVHT: wording improvement. ABNORMAL ENG PARAMETERS IN FLIGHT: procedure reviewed. ONE EEC FAULT: wording correction “UNCOMMANDED 100%NP ON ONE OR TWO PROPELLERS”: content and title changed (instead of “ONE PROPELLER REMAINING….POWER SELECTION”). PROP OVER LIMIT: procedure reviewed. DC GEN FAULT: correction of a missing item. ANTI SKID FAULT: anti skid set to OFF item added. SMK DET FANS FAULT: content and title changed to generalize. PRELIMINARY COCKPIT PREPARATION : PL 1+2: check at ground idle. Speeds adjusted and 23T performances completion.

1.05A 1.10

2.01, 2.03 2.06

2.09 2.10A

2.11 2.18 (_550variant)

2.25

2.33

3.01 & 6.01

4.63 & 4.65

QRH QUICK REFERENCE HANDBOOK 5-07 page 1-089

ATR72

S.N.N.P.Shipping Note Normal Pages

SEP 10

Action P CH SE Page Seq Date Validation Criteria

Turn NO

" ADD " = Add "DESTROY" = Destroy " …….." = Revised

"SEE VAL" = See Validation

DESTROY TR 004

...... 1 05A 001 SEP 10

...... 1 09 001 SEP 04 PW1241 10 001 SEP 10

...... 1 09 100 APR 08 PW127-127F-127M1 10 001 SEP 10

...... 2 01 001 SEP 102 02 001 OCT 09

...... 2 03 001 SEP 102 04 500 OCT 09 MOD 3973 or 4371 or 4457

...... 2 05 001 OCT 082 06 001 SEP 10

...... 2 09 500 SEP 10 MOD 3973 or 4371 or 44572 10 050 OCT 09 MOD 4111

...... 2 10A 500 SEP 10 MOD 3973 or 4371 or 4457

...... 2 11 030 SEP 10 PW124 MOD 43712 12 050 OCT 08 PW124 MOD 4111

...... 2 11 500 SEP 10 PW127F-127M2 12 500 OCT 08 PW127F-127M

...... 2 25 001 SEP 102 26 001 APR 08

...... 2 33 001 SEP 102 34 001 OCT 08

...... 3 01 001 SEP 10

5.02

72

CHECK LIST

R.T.R. Reason of Temporary Revisions SEP 10 001

ENV

TR EDITION DATE REASON AFFECTED PAGES

01 OCT 98 Single engine gross ceiling 4.61 - 4.62

02 FEB 99 DUAL DC GEN LOSS 1.06

03 MAR 99 SEVERE ICING : improvement of

detection and procedure 1.09 - 3.04

04 NOV 99 Spring tab MOD 4373 or 8167 ENG FLAME OUT AT TO

2.03 - 2.20 - 2.21

05 NOV 00 Introduction of FAA AD Missing page for 212A

Various

3.05 - 3.06 - 3.07 4.64 2.37

06 FEB 02 Introduction of modification 5313 EGPWS

1.07 - 1.08

07 FEB 03 Introduction of modifications 5377+5434

CDLS Models 102-202-212-212A 1 - 2 - 3 - 6

08 OCT 03 Introduction of modifications 5377+5434 CDLS Models 101-201-211

1 - 2 - 3 - 6

09 FEB 05

Correction of content 2.02 Introduction of BOTH ELEVATORS RECONNECTION ON GROUND

Correction of Cockpit Door Daily Check Single Eng Gross Ceiling Flaps 15 for

Icing Conditions

2.02 2.22A

3.02A 4.62

10 APR 06 FUEL LO LVL Procedure Updating

Introduction of Mod 5561 : Messier--Bugatti Wheels and Brakes

2.13 4.65

11 MAR 07 DITCHING and FORCED LANDING

Procedure Updating MISSING PAGE 2.14

1.08 – 1.08A 2.14

12 MAY 07 MPC : indicating/recording system, install MPC with QAR Thales

2.29A

13 JUN 08

Contents page correction (deletion of EEC SELECT IN FLIGHT and ATPCS

FAIL) ENG OIL LO PR : (Only for Aircraft with

Man Ignition), Procedure updating

2.01

2.12 (sequences 050, 150

and 500 only)

14 JUL 08 PW127M impact including BOOST

function Part 4

15 AUG 08 ENG BOOST FAULT procedure

introduction 2.01 – 2.12A


ATR 72

S.N.T.P. Shipping Note Temporary Pages MAY 11

Please find below the list of the temporary pages created, suppressed or revised

Temporary revision N° 05 (MAY 11).

Action P CH SE Page Seq Date Label Modification expression

End NO

"F"=Facing "ADD"=Add "DESTROY" = Destroy "A" = After "……" = Revised "SEE VAL" = See Validation

ADD 1 ** ** 010 050 MAY 11 MOD (3973 or 4371 or 4457) ADD 1 ** ** 010 500 MAY 11 ADD 1 ** ** 011 050 MAY 11 MOD (3973 or 4371 or 4457) ADD 1 ** ** 011 500 MAY 11 ..... 5 01 ** 001 089 MAY 11 NO ..... 5 02 ** 001 001 MAY 11 ..... 5 04 ** 001 089 MAY 11 NO


ATR 72

L.E.T.P. List of EffectiveTemporary Pages MAY 11

You must hold in your manual the following temporary pages Issue P CH SE Page Seq Date Label Modification expression Validity expression

End NO

TR05 1 ** ** 010 050 MAY 11 MOD (3973 or 4371 or 4457) NO0001-0003 TR05 1 ** ** 010 500 MAY 11 NO0051-0059 TR05 1 ** ** 011 050 MAY 11 MOD (3973 or 4371 or 4457) NO0001-0003 TR05 1 ** ** 011 500 MAY 11 NO0051-0059 TR05 5 01 ** 001 089 MAY 11 NO ALL TR16 5 02 ** 001 001 MAY 11 ALL TR05 5 04 ** 001 089 MAY 11 NO ALL

NO

RM

AL

CH

EC

KLI

ST

6.01

72


* : if applicable

R

Mod : 3973 or 4371 or 4457

FINAL COCKPIT PREPARATION PARKING BRK ............... ON / PRESS CHECKALTIMETERS .............................................SETLANDING ELEVATION ..............................SETCOM / NAV / GPS ......................................SET FUEL QTY ............................................ CHECKENG F/U ................................................RESETMEMO PANEL...................................... CHECKPWR MGT ....................................................TO

DESCENT

CCAS..........................................................RCL LDG BUGS ...........................SET AND CHECK LDG ELEVATION ..................................CHECK ARRIVAL BREIFING ..................... COMPLETE

BEFORE PROPELLER ROTATION

TAIL PROP.................................... ON BOARDDOORS ..............................................CLOSEDT/O BUGS / APM* ............... SET AND CHECKTRIMS ........................................................SET CDLS*.......................................................... ONSEAT BELTS............................................... ONBEACON ..................................................... ON

BEFORE TAXI

PROP BRK *.............................................. OFFCOCKPIT COM HATCH.....................CLOSEDCL 1 + 2 ...................................................AUTOANTI-ICING .........................................AS RQD ANTI-SKID............................................... TESTFLAPS ........................................................SET

TAXI

TAXI & T.O LIGHTS .................................... ONBRAKES ............................................... CHECKAFCS ..........................................................SETRUDDER CAM ...................................CENTER TO CONFIG............................................. TESTTAKE OFF BRIEFING ...................COMPLETE

BEFORE TAKE OFF

BLEED VALVES..................................AS RQDAIR FLOW ..............................................NORMGUST LOCK..................................... RELEASEFLIGHT CONTROLS............................ CHECK CCAS................................................... TO INHIXPDR / TCAS*............................... ALT / AUTOEXT LIGHTS................................................ ONFD BAR (When lined up) ....................CENTER

AFTER TAKE OFF

LDG GEAR ...................................................UPFLAPS ........................................................... 0°PWR MGT / NP .......................... CLB / CHECKBLEED VALVES.......................................... ON TAXI & T.O LIGHTS .................................. OFFALTIMETERS ...................... SET AND CHECK

APPROACH

SEAT BELTS................................................ON ALTIMETERS ....................... SET AND CHECK CABIN ALTITUDE .................................CHECK

BEFORE LANDING

LDG GEAR .........................................3 GREEN FLAPS ...................................................CHECK PWR MGT .................................................... TO TLU....................................................... LO SPD ICING AOA LIGHT ................................CHECK EXT LIGHTS.................................................ON

AFTER LANDING

XPDR / TCAS* / RADAR..........................STBY FLIGHT CONTROLS...........................LOCKED FLAPS ............................................................0° TRIMS ........................................................ SET LAND LIGHTS / STROBES........................ OFF ANTI-/DE-ICING ......................................... OFF ENG START ROT SEL............................... OFF

After at least one minute CL 1............................ FTR THEN FUEL SO

PARKING

PARKING BRK ............................................ ON TAXI & T.O LIGHTS ...................................OFF CL 2 ...........................................................FTR PROP BRK *................................................ ON BEACON ....................................................OFF SEAT BELTS..............................................OFF TAIL PROP................................ ON POSITION

When leaving aircraft OXYGEN MAIN SUPPLY.....................OFF ICE AND RAIN PROTECTION ............OFF EXT LIGHTS ........................................OFF EMER EXIT LIGHT .......................DISARM EFIS / RADAR / COM / NAV................OFF CL 2............................................. FUEL SO FUEL PUMPS 1 + 2 .............................OFF CDLS* ..................................................OFF

BAT ......................................................OFF

IN CASE OF ICING CONDITIONS REFER TO 3.05 IN CASE OF SEVERE ICING REFER TO 1.09

ON GROUND EMER EVACUATION AIRCRAFT / PARKING BRAKE ............................................................ STOP / ENGAGE ATC (VHF 1)......................................................................................................... NOTIFY CL 1 + 2........................................................................................... FTR THEN FUEL SO MIN CAB LIGHT........................................................................................................... ON CABIN CREW (PA) .............................................................................................. NOTIFY FIRE HANDLES 1 + 2 ...............................................................................................PULL AGENTS...............................................................................................................AS RQD ENG START ROTARY SELECTOR .............................................. OFF / START ABORT FUEL PUMPS 1 + 2 ................................................................................................... OFF EVACUATION ..................................................................................................... INITIATE

Before leaving aircraft, BAT................................................................................. OFF

QRH 202-PEC

Documents

Transcript of QRH 202-PEC