ENGINE FAILURE IN CRUISE PF PNF (WITH NO DAMAGE)no_damage).pdfFCOM 3.06.30 LRC ceiling Diversion...

PFPF PNFPNFCommon LR

ENGINE FAILURE IN CRUISE (WITH NO DAMAGE)

Detection

ENGINEFAILURE !

ECAMactions

SDanalysis

STATUS

STANDARD

OBSTACLE

SITUATIONASSESSMENT

STRATEGYDECISIONS

LR - Version 02a

LR

LR

FIXEDSPEED

(A330 only)


ECAM PROCEDURE

ECAM ACTIONS

1. ENG 1 FAIL

DETECTION

PFCOMMUNICATES

FLIES THE AIRCRAFT

NAVIGATES LAND ASAP…Short term decision

CONSIDER AUTOMATION USE

THRUST LEVERS………………………….MCT

A/THR………………………………………..OFF

OrOrAndAnd

STOP ECAM actions when :

Deceleration Not below Green Dot


For descent :

M.82/300 KT………………………..SET AND PULL

LRC CEILING ALT……..………….SET AND PULL

2. STANDARD STRATEGY

Check LRC CEILING

During descent to LR ceiling ...

MCT

Speed controlled by the elevator

Thrust MCTLR

L R

A330 A340

EO

QRH

4.00

A330

A340

REC MAX = EO LRC Ceiling EO CLR Prompt


ORDER…………….………..…..…”CONTINUE ECAM” ECAM ACTIONS……………………..……CONTINUE

ECAM PROCEDURE

ECAM ACTIONSDAMAGE ?

SYSTEM DISPLAY

STATUS

DECISION

RETURN TO NORMAL TASK SHARING

LDG DISTLDG DIST

WEATHERWEATHER

OPERATIONAL ANDCOMMERCIAL

CONSIDERATIONS

OPERATIONAL ANDCOMME RCIAL

CONSIDERATIONS

NOT IFYNOT IFY

DECISIONDECISION

OPS …OPS …

PURSER / PAXPURSER / PAX

ATCATC

STAT US, or

SUMMARY

APU normal flight envelope :

Consider APU Start DIST & FUEL computations to Landing

QRH

4.00

++•••• •••• •••

••••••••••••••••

FCOM

3.06.30

FCOM

3.01.49

, RELIGHTQRH

2.00

3. ENGINE RELIGHT

PFPF PNFPNFCommon LR4. STANDARD STRATEGY

Reaching LRC ceiling

LR SPEED………………………………………….SETA/THR…………………………….………………….ON

Descent to landing

RESUME MANAGED MODES

T/D

Thrust IDLEA/THR

At LRC ceiling ...

LR SPEED

LONGRANGECRUISE

LR

LR

LR

L R

QRH

4.00


ECAM PROCEDURE

ECAM ACTIONS

1. ENG 1 FAIL

DETECTIONFLIES THE AIRCRAFT

NAVIGATES LAND ASAP…Short term decision

CONSIDER AUTOMATION USE

THRUST LEVERS………………………….MCT

A/THR………………………………………..OFF

OrOrAndAnd

STOP ECAM actions when :

Deceleration Not below Green Dot

A/THR is set to OFF immediately to avoidthrust reduction to IDLE

A/THR is set to OFF immediately to avoidthrust reduction to IDLE

PFCOMMUNICATES


For descent :

M.82/300 KT………………………..SET AND PULL



Check LRC CEILING


MCT

Speed is controlledby the elevator

Thrust is MCTLR

L R

A330 A340

EO CLR Prompt CAUTION :

if pressed, predictionsrevert to dual enginepredictions

REC MAX value is now the EOLRC Ceiling

EO

QRH

4.00

A330

A340

STANDARD

No obstacle and time constraint

OBSTACLE

To ensure the margins over obstacles

STRATEGY

FIXED SPEED

ETOPS constraint

As establishedbefore dispatch,

use:

M.82 / 330 KT

Or

M.82 / 310 KT


For descent :

M.82/300 KT………………………..SET AND PULL



Check LRC CEILING


MCT


Thrust is MCTLR

L R

A330 A340




EO

QRH

4.00

A330

A340

STANDARD

No obstacle and time constraint

OBSTACLE

To ensure the margins over obstacles

STRATEGY


For descent :

M.82/300 KT………………………..SET AND PULL


2. STANDARD STRATEGY A330 A340

Check LRC CEILING


MCT


Thrust is MCTLR

L R




EO

QRH

4.00

A330

A340

GW at ENG FAIL

LRCCeilingLRC

Ceiling ExternalTemperature

Green DotGrossCeiling


QRH

4.00

LRC AND GREEN DOT GROSS CEILING QUICK CHECK


For descent :

M.82/300 KT………………………..SET AND PULL


2. STANDARD STRATEGY A330 A340

Check LRC CEILING


MCT


Thrust is MCTLR

L R




EO

QRH

4.00

A330

A340

LRC AND GREEN DOT GROSS CEILING QUICK CHECK

QRH

4.00

GW at ENG FAIL

LRCCeilingLRC

Ceiling

ExternalTemperature




For descent :

M.82/300 KT………………………..SET AND PULL



Check LRC CEILING


MCT

LR

L R

A330 A340

EO

QRH

4.00

A330

A340

EO CLR Prompt

Speed controlled by the elevator

Thrust MCT

REC MAX = EO LRC Ceiling

if pressed, predictions revertto all engines operativepredictions

!


DAMAGE OR NO DAMAGE ?

CONSIDER ENGINE DAMAGE IF YOU NOTICE :

High vibration prior to engine stopped, loud noise

Stall

Any Abnormal Indication on ENG Page (such as N1 or N2 ~ 0)

No attempt of RELIGHT


Descent to LR CRZceilingcomputations

1

FCOM

3.06.30

LRC ceiling

Diversion Airport

Initial FL

ΔDistΔFuelΔTime

Descent from LR CRZceiling to landingcomputations

2

Remaining distance to diversion airportFuel used in LRC FL Down to LandingTime in LRC FL Down to Landing

PERFORMANCE CHECK

QRH

4.00

A330

A340



1

FCOM

3.06.30

LRC ceiling

Diversion Airport

Initial FL

ΔDistΔFuelΔTime


2


PERFORMANCE CHECK

QRH

4.00

A330

A340

Descent to LR CRZcomputations

LRCCeiling

CRZ FL atFailure ΔDist

ΔFuelΔTime

ΔDistΔFuelΔTime

GW at ENG FAIL

FCOM

3.06.30



1

FCOM

3.06.30

LRC ceiling

Diversion Airport

Initial FL

ΔDistΔFuelΔTime


2


PERFORMANCE CHECK

QRH

4.00

A330

A340

LR Cruise to Landing computationsQRH

4.00

DiversionAirport

LR CRZ Ceiling

Fuel used in LRCFL, down to Landingbased on ref weight


Correctionaccording toΔcomparedto reference

weight


weight

+ =Time in LRC FLdown to landingTime in LRC FLdown to landing

Fuel used in LRC FLDown to Landing


Remaining distance

QRH

4.00



1

FCOM

3.06.30

LRC ceiling

Diversion Airport

Initial FL

ΔDistΔFuelΔTime


2


PERFORMANCE CHECK

QRH

4.00

A330

A340

LR Cruise to Landing computations

DiversionAirport

LR CRZ Ceiling




weight


weight

+ =Time in LRC FLdown to landingTime in LRC FLdown to landing



Remaining distance

QRH

4.00

ENGINE FAILURE IN CRUISE PF PNF (WITH NO DAMAGE)no_damage).pdfFCOM 3.06.30 LRC ceiling Diversion...

Documents

Transcript of ENGINE FAILURE IN CRUISE PF PNF (WITH NO DAMAGE)no_damage).pdfFCOM 3.06.30 LRC ceiling Diversion...