AOM JS32

.!: u

Q) -~ a:

SA.4-3100/MOM/258 COPY No. ________________ _

BAE SYSTEMS

Jetstream Series 3200

Manufacturers Operating Manual Part 1

STATEMENT OF INITIAL CERTIFICATION This manual complies with British Civil Airworthiness Requirements, Section A, Chapter A 7-3.

Signe

N

BRl7'SH AEROSPACE

JETSTREA/111 SERies l200

MANUFACTURERS OPERATING MANUAL PART 1

CERTIFICATION

This Manual complies with British Civil Airworthiness Requirements, Chapter A6-7. The technical accuracy of this Manual has been verified and is certified as correct.

The inclusion of an uncertified amendment will invalidate this certif ication.

Design Authority. Signed ~Date lfr.~~.>O f or BRITISH AEROSPACE PLC

CIVIL AIRCRAFT DIVISION

PRESTWICK AIRPORT, AYRSHIRE

SCOTLAND KA9 2RW

C.A.A. Design Approval No DAI/1011/55

DISCLAIMER

The extent of liabilities of the Constructor for any defect in or failure of an aircraft or any part thereof is no wider than that set out in the Warranty Clause contained in the contract subject to the provision of which such aircraft was sold.

Nothing in the Manual is to be taken as a representation condition or Warranty so as to affect such liabilities or to impose any such or other liability on British Aerospace PLC, Civil Aircraft Division.

The manual is issued specif ically for Jetstream Series 3200 Customer model defined on the title page. The manual has no technical validity in relation to any other aircraft.

EMBODIMENT OF MODIFICATIONS AFTER DEI.IVERY OF THE LAST PRODUCTION AIRGRAFT OF THE TYPE

To ensure that the information contained in this Manual is compatible with the modification state of the aircraft, no information relating to modifications issued after delivery of the last production aircraft of the type will be incorporated in this Manual without the written assrance of the operator that he intends to install a particular modification.

The only exception to the above will be e.A.A. - req~ired Mandatory Modifications.

Certif ication

Page 1/2

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JETSTREANI SeRies J200


RECORD OF REVISIONS

The incorporation of each Revision must be recorded below

IMPORTA.NT: The inclusion of an uncertified Revision will invalidate the initial certification of this manual.

Rev Issue Inserted Date Rev Issue Inserted Date No Date by Inserted No Date by Inserted

1 fe'~->! ~ ~.e 1> 7.s.~'7 21 2 ~fi r>/~ c_c; :t) ~-~-~ 22

.)V( 1-)~ t. 7. r;;p., ~ -3 a .c, . .b 23 4 s_,?rl~ ~-~ ,]> 18 ,e?~ 24 5 NOVlr~ t; t; }, /2.. ,z . 5"' 25 . 6 _oo:-i5m

'i .c.. l.l i'2,. \ ~ 26 7 R::B ~r J JJ 02-\~\qo. 27 1Sfl\o 8 HA'f l5A qc

-c..r.il.. \\r,.,~.(l~ 28 9 ~~ Sl' t:\Q~ OC'\ '2.3 /!!Jo 29

10 ~~ ~, i, r~ M ~,:.sj~ 30 11 ... _.~IS' ,Q .r ld.2 -:::r~ -:H 91). . 31 ~ ... 12 0C' ~ ~ 2.1 /qlt 32 6(a.3 -13 -:ni~ , \tJt - D :r(,)tJ ,. Jq7 33 rs/11

- V, .

14 ~hJ ~~"'~~ :S

Rev Issue No Date

41

42

43

44

4S

46

47

48

49

so

Sl

S2

53

S4

SS

56

S7

58

S9

60

61

62

63

64

B_T_,, AEROSPACE

JETSTREAAll SeRies }200


Date Rev Issue Inserted by Inserted No Date Inserted by

6S

66

67

68

69 ' 70 '

71

72

73

74

7S

76

77

78

79

80

81 -

82

83

84

85

86

87

88

Record of Revisions

Page 2

Date Inserted

.

-

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o o o a a

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~AEROt#WCE

JETSTREANI SERiES J200

MANUFACTURERS OPERATING MANUA L PART 1

RECORD OF TEMPORARY REVI SIONS

The incorporation and subsequent cancellation of each Temporary Revision must be r ecor ded below .

IMPORTANT: The inc l usion of an uncerti f ied Te mporary Revision wi ll invalidate the i ni t i al certification of thi s manual .

Da te Cance lled by Date No Inserted by Inserted (Rev No) Cancell ed Signatur e

17 - / 4- . Gr-.J) zq.11 .~ ----~ 5 -.... 1

No

\ "".\ -~ \'"\~ ,i_ ~

\~-i ,i .:5> lb-2-lb-~ (J_( /

J ~ . I ( ~-1

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Date Cancelled by Date Inserted by Inserted (Rev No) Cancelled

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BRl77SH A6ROSFfllCI!!

JETSTREANI SERiES 1200


1 ;'i,

PRELIMINARY PAGES

LIST OF EFFECTIVE PAGES

TITLE PAGE CERTIFICATION RECORD OF REVISIONS 1

2 RECORD OF TEMP. REVISIONS 1

2 RECORD OF SERVICE BULLETINS AND MODIFICATIONS 1/2 Jun 1/93

LIST OF EFFECTIVE PAGES 1 Sep 15/02

CONTENTS 1/2 Jan 1/92 INTRODUCTION 1 Sep 15/02

2 Nov 15/98 3 Nov 15/98 4 Sep 15/02 5 Sep 15/02 6 Sep 15/02

GLOSSARY CONTENTS 1 Sep 15/02 GLOSS-1 (ABBREVIATIONS) 1 Nov 15/98

2 Nov 15/98 3 Nov 15/98 4 Nov 15/98 5 Nov 15/98 6 Nov 15/98

7/8 Nov 15/98 GLOSS-2 (DEFINITIONS) 1/2 Jan 15/00 GLOSS-3 (CONVERSIONS) 1 Feb 15/89

2 Feb 15/89 3 Feb 15/89 4 Aug 1/88 5 Aug 1/88 6 Aug 1/88 7 Aug 1/88 8 Aug 1/88 9 Nov 15/98'

10 Nov 15/98

PRELIMINARY: LIST OF EFFECTIVE PAGES

Page 1

21006891 Sep 15/02

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1 BRITISH AEROSPACE

JETSTREANI SERiEs J200


RECORD OF INCORPORATED SERVICE BULLETINS/MODIFICATIONS

Service Bulletins and Modif ications incorporated at original build of aircraft to which this manual relates are similarly incorporated into the manual and are not separately listed at initial issue of this manual. Reference should be made to the Manufacturer's records for the build standard at delivery.

Service Bulletins and Modif ications listed below have been incorporated by revisions as indicated. It should be noted that only Mandatory Service Bulletins and Modif ications effective at the time of the revision have been automatically

incorpo~ated. Non-Mandatory Bulletins will only be incorporated following written advice from the Operator concerned to the Technical Publications Department, Prestwick.

Service Issue Bulletin/ No/Date Modif ication No.

73JA891146 1 Nov 73JA900141 1 Feb 34JK2562A 1 Feb

8028. G Jan 8100 D Jan

3399 1 Aug

30/89 ) 6/90 ) 6/90 )

) 11/89 ) 13/89 )

) 28/89 )

Incorporated by:-Revision Date

6 Dec 15/89

SERVICE BULLETINS

Page 1/2

Feb 15/90

l~-- '

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BRITISH AEROSPACE



MANUFACTURERS OPERATING MANUAL

PART 1 FLYING

CONTENTS LIST

INTRODUCTION

GLOSSARY & TABLES

l. GENERAL

2. AIRFRAME & FLIGHT CONTROLS

3. AIR COND & PRESS

4. EMER EQUIP & OXYGEN 5. ELECTRICS

6. ENGINES & PROPS

7. FUEL

8. FIRE PROTECTION

9. HYDRAULICS

10. ICE & RAIN PROTECTION

11. INSTRUMENTS, FCS

12. COMMS & RECORDING

13. LOADING

14. FLIGHT PLANNING

15. PERFORMANCE

16. FLIGHT GUIDE

17. NORMAL PROCEDURES

18. DRILLS

19. M. E . L.

20. GROUND HANDLING MOM PART 1 CONTENTS

Page 1/2 Aug 1/88

l!IRJ/77SHAEROSPACI/!

JETSTREAIW SEIES J200


MANUFACTURER'S OPERATING MANUAL (M.O.M.) INTRODUCTION

1 . AUTHORITY

This manual is prepared in accordance with British Civil Airworthiness Requirements, CHAPTER A6-7 and it conforms with the relevant parts of CAA publication CAP 450.

It may be used by the operator, together with the operator's own material, to create an Operations Manual as required by the appropriate regulating authority.

Every ef fort has been made to ensure that the contents of this manual do not conflict with the information in the approved Flight Manual. If such a conflict of data is discovered, the Flight Manual must be accepted as the overriding authority.

2. CONTENTS

The M.O.M. provides information on the technical, handling and performance characteristics of the Jetstream 3200 for use by the Flight Crew.

The manual is divided into three volumes.

Part 1 - Flying, contains:

Limitations, Flight Planning, Loading, Performance, M.E.L., Ground Handling, Flight Technical, Flight Guide and Notice to Aircrew.

This is intended for use on the Flight Deck.

Part 2 - Technical, contains:

Description of the function and operation of the Airframe,Power Plant and Aircraft Systems. It is intended for use as a Technical Study Guide on the ground.

Part 3 - Emergency and Abnormal Drills, contains:

All relevant Emergency and Abnormal Drills. It is intended for use on the flight deck.

INTRODUCTION

Page 1

1 21006883 Sep 15/02

SRl77SH Al!RDSPACI



3. LIST OF EFFECTIVE PAGES

Inserted at the front of each chapter, following the contents page, is a "List of Effective Pages" listing all pages contained within the chapter.

This enables the operator to establish that the manual is complete and that all pages are to the correct revision standard. The LEP's are revised and re-issued whenever the pages of the relevant chapter are affected by a revision.

All pages of the manual are recorded on the LEP's, each page identified by Chapter, Section and Page number, followed by the date of issue.

The page date on the LEP must be the same as the date on the corresponding page in the manual:-

~5-~-6 ~ Chapter Section Page No.

4. NORMAL REVISIONS

May 1/88 1

Date of Issue

Revisions to the contents of this manual will be issued when necessary to keep the manual up-to-date.

Each revision will comprise a number of revised pages accompanied by a Transmittal Letter. The transmittal letter carries the authority for the revision and instructions for its incorporation.

Each revision transmittal after the original issue will be numbered in sequence, show the issue date of the revision and the page date of the revised pages.

The incorporation of each revision must be recorded on the Record of Revision page at the front of the manual.

It is recommended that the Transmittal letters are retained within the manual to provide a revision history.

Only revisions of technical content are identified.

Changed text is identif ied by a vertical line on the lef t hand margin.

INTRODUCTION

Page 2 21006104

Nov 15/98

l!1Rll77SH AEHOS'PJAC6

JETSTREANI SEIES J200


Note: When this manual is issued solely for training purposes. each page will be annotated "FOR TRAINING PURPOSES ONLY" and revisions will not be issued.

5. TEMPORARY REVISIONS Information requiring urgent incorporation, or temporary instructions are published on yellow paper as Temporary Revisions (TR) . Transmittal information is contained within the TR. When a TR is incorporated or withdrawn, the details should be recorded on the Record of Temporary Revisions page at the front of the manual.

6. AIRCRAFT IDENTIFICATION The information contained in this manual applies only to the Aircraft Model No. specified on the title page.

7. AIRCRAFT EFFECTIVITY CAUTION: BEFORE USING THE INFORMATION CONTAINED ON A WHITE PAGE

IN THIS MANUAL, ENSURE THAT THE PAGE IS NOT AFFECTED BY GREEN OR BLUE PAGES WITH EFFECTIVITY TO IDENTIFY THE AIRCRAFT FOR WHICH THE INFORMATION IS REQUIRED.

7.1 In all chapters except CHAP 18 the following applies: White Pages are not identified by effectivity. Those not af fected by corresponding green or blue pages are applicable to all aircraft in the fleet. Green pages are used where a technical dif f erence occurs between aircraft. The page carries the constructor's number of the aircraft to which it applies and is usually inserted to follow the corresponding white page. If a signif icant number of pages are affected, then the green pages will be inserted at the end of the relevant Chapter or Section. Blue pages are used to give Pre-Service Bulletin (SB) information, in the manual pending fleet incorporation of the SB. The page is usually inserted following the page affected by the SB, and identified by constructor's number (if required). If a significant number of pages are af fected, then the blue pages will be inserted at the end of the relevant Chapter or Section. Blue pages should be removed and destroyed af ter complete embodiment of the SB.

INTRODUCTION

Page 3 21006141

Nov 15/98

BIN77SH AITRDSRll&E JETSTREAllll SERiES }200


7.2 A Notice to Aircrew (NTA) is issued on orange paper and will be retained in ascending order.

7.3 In CHAP 18 pages containing technical differences will be issued as white pages, inserted following the original white page. Both the original and the change page will carry the constructor's number of the aircraft to which they apply.

8. MANUAL LAYOUT (MOM PART 1) 8.1 This manual is divided into four sections.

The f irst section contains details of the aircraft systems and the chapters are identif ied by yellow tabbed divider cards. Each chapter contains limitations and essential data followed by the Conditional, Abnormal and Emergency procedures applicable to that chapter.

The second section identified by white tabbed divider cards generally covers items for pre-flight preparation.

The third section, identified by a red tabbed divider card lists all Normal Drills. Emergency and Abnormal Drills are detailed in MOM Part 3.

The fourth section identified by white tabbed divider cards contains the MEL, Ground Handling and NTAs.

8.2 Procedures and Drills

In those chapters dealing with Procedures it is assumed that the captain will deal with the more serious problem first by reference to the drill.

For example, if a C.A.P.' (Red) caption comes on at the same time as a C.A.P. (Amber) caption, it is assumed that the captain will deal first with the Red caption, by reference to the Emergency Drill, and when that drill is completed any remaining Arnber captions should lead him into the appropriate Abnormal Drill.

INTRODUCTION

Page 4

Sep 15/02 21006884

l!!IRl7TSH AIRDSF'ACl!I JETSTREAAll SetiES J200


8.3 Warning and Indicator Lights

Warning and indicator lights take various forros on the Jetstream aircraft. For clarity the lights are described in the text as follows:

8.3.1 A C.A.P. caption is a caption on the Central Annunciator Panel and will be identified in this manual by boxed letters or within square brackets, preceded by the abbreviation C.A.P.

For example C.A.P. [HYD] {amber) caption or

C.A.P. ~ {amber) caption. 8.3.2 A caption signifies a series of letters

illuminated from behind.

8.3.3 A light is a lamp without lettering on it.

9 . MANUAL LAYOUT (MOM Part 2) The MOM Part 2 is divided into Chapters describing the aircraft systems and equipment.

Each Chapter is sub-divided into text, system schematics and illustrations showing the controls and indications.

10. MANUAL LAYOUT (MOM Part 3) The MOM Part 3 is in f lip-card f ormat and details the Emergency and Abnormal Drills.

INTRODUCTION

Page 5

21006885 Sep 15/02

SRl77SH AERDSPJlll::6



11. ASSOCIATED PUBLICATIONS

The associated publication to this manual is the:

HP4.16 FLIGHT MANUAL

A set of manuals to ATA 100 specif ication complete the support publications for Jetstream aircraft and consist of:

Weight and Balance Manual Maintenance Manual Wiring Manual Component Maintenance Manual Structural Repair Manual Illustrated Parts Catalogue Maintenance Schedule Illustrated Tool and Equipment Manual

INTRODUCTION

Page 6

Sep 15/02 21006893

BIW77SH AERO.BPAC/6



ABBREVIATIONS, GLOSSARY AND CONVERSION TABLES

LIST OF CONTENTS

1-1 ABBREVIATIONS

1-2 DEFINITIONS

1-3 CONVERSION GRAPHS AND TABLES QNH-QFE-Pressure Altitude Pounds to Kilogramrnes Kilogranunes to Pounds Feet to Metres Metres to Feet Temp. ISA/Amb. Temp./Press. Altitude

1

1

1

2

3 4

5 6

Wind Component 7 C - F 8 Determination of Temp. In Relation to ISA 9 Indicated Outside Air Temperature Corrections 10

GLOSSARY. LIST OF CONTENTS

Page 1

1 21006912 Sep 15/02

ll!IRl77SHAIRDSPACE

JETSTREAllll SEIUES J200


ABBREVIATIONS

Abbreviations used in the text, have the following meanings:-

A AAL ac Acc ACP ADF ADI ADS AFCS AGL Ah ALT AMSL AOA A/P APPR APR APR ASDA ASDR ASI ATC AUW

BC BCAR BCF BITE BTC

ampere above aerodrome level alternating current accumulator audio control panel automatic direction f inder attitude director indicator air data system automatic f light control system above ground level ampere-hour altitude above mean sea level angle of attack autopilot approach (flight director) approach (engine) automatic performance reserve accelerate-stop distance available accelerate-stop distance required airspeed indicator air traf f ic control all up weight

back course British Civil Airworthiness Requirements bromo chloro di-fluoromethane built-in test equipment bus-tie connector

21006105

1-1

Page 1

Nov 15/98

CAA C.A.P. CAS C/B ces ccw CDL CDU CG CLG CTRL CVR cw

de o

C F DG DME DV

EAS ECAC ECS EDA/EMD

EDP EGT ELT EPNdB ESS

1-1

Page 2

Nov 15/98

BRl77BH AIROSPAC6

JETSTREANI SEIES 'J200


ABBREVIATIONS (cont)

United Kingdom Civil Aviation Authority central annunciator panel calibrated airspeed circuit breaker communication control system counter-clockwise conf iguration deviation list control display unit centre of gravity ceiling control cockpit voice recorder clockwise

direct current degrees (angular) degrees Celsius {Centigrade) degrees Fahrenheit directional gyro distance measuring equipment direct vision

equivalent airspeed european civil aviation conference e1:.vironmental control system emergency distance available

{accelerate/stop at take-off) engine-driven pump exhaust gas temperature emergency locator transmitter effective perceived noise decibels essential

21006106

FAA FAR FD FDR FL FM FSII FSOV f t ft/min f wd

g gal GPS GPU GPWS GS

HAT HDG HF HP hr HSI H/W

IAS ICAO ICO I/F IFR ILS IMC IMN IMP in IOAT ISA

BRll77BHAEROSPACI

JETSTREANI SEIES J200



Federal Aviation Administration Federal Aviation Regulations (US) f light director f light data recorder f light level f light manual fuel system icing inhibitor fuel shut-off valve (HP fuel cock) f eet f eet per minute f orward

accelerations due to gravity gallons global positioning system ground-power unit ground proximity warning system glideslope

height above (Runway) threshold heading high frequency. Long waveband radio communication high pressure hour horizontal situation indicator head wind

indicated airspeed International Civil Aviation Organisation instinctive cut-out switch instrument f lying instrument f light rules instrument landing system instrument meteorological conditions indicated mach number Imperial in ches indicated outside air temperature International Standard Atmosphere

21006107

1-1

Page 3

Nov 15/98

JAA JAR JPl JP4 JP8 Kg Kt

L 1 lb LDA LDR LFLR LG LH LOC LP

M MAC Max MDA MDH MEL MFLI MIN mi ns MLG MLW mm

MMO MSA MSF M/SW MTOW MZFW

1-1

Page 4

Nov 15/98

SRl77SH .AIROSRllCE JETSTREAllll SEIES J200


ABBREVIATIONS (cont}

Joint Aviation Authorities Joint Aviation Requirements kerosene wide cut gasoline kerosene fuel with icing inhibitor FSII kilograrnmes knots

lef t litre pounds landing distance available landing distance required landing f ield length required landing gear lef t hand localiser (ILS} low pressure

me tres mean aerodynamic chord maximum minimum decision altitude (altimeter set to QNH} minimum decision height (altimeter set to QFE) minimum equipment list magnetic fuel level indicator minimum minutes main landing gear maximum landing weight millimeters maximum operating mach speed minimum safe altitude minimum sector fuel micro switch maximum take-of f weight maximum zero-fuel weight

21006108

NDB NLG n mile no NRV NTOFP NTS NU NWS

OAT OCL OM Ops ORS OSG

PEC PF PG PNF ppm psi psid psig PTT PWR AUG

QDM QFE QNH QTY

R RAIM RH RMI RMU RNAV

.SRl77SN Al1ROSPACE

JETSTREAIW SERiES J200



non-directional beacon nose landing gear nautical mile number non-return valve (check valve) net take-of f f light path negative torque sensing (system) nose up nosewheel steering

outside air temperature obstacle clearance limit outer marker operations operational revision status overspeed governor

position error correction pilot f lying propeller governor pilot not f lying parts per million pounds per square inch pounds per square inch dif ferential pounds per square inch gage press to test power augmentation

magnetic bearing airf ield elevation atmospheric pressure sea-level atmospheric pressure quantity

right receiver autonomous integrity monitoring right hand radio magnetic indicator radio management unit radio navigation

21006109

1-1

Page 5

Nov 15/98

RPM R/T RTOW R/W RVR

SAT SB SE sec

SG SHP SMC SOP sq SRL Stn

Tamb TAS TAT TCAS TCS temp TIT TMA T/0 TOD TODA TODR TOR TORR TORA TOW TSI TTL

UHF UK ULB

1-1

Page 6

Nov 15/98

BIN77SH AIRDSFJllCE JETSTREAllll SERES J200



revolutions per minute radio telephone regulated take-off weight runway runway visual range

static air temperature service bulletin single engine seconds symbol generator shaf t horsepower standard mean chord standard operating procedure square single red line (computer) fuselage or wing station

ambient temperature from external source (C) true air speed total air temperature traf fic alert and collision avoidance system touch control steering temperature turbine inlet temperature terminal manoeuvring area (controlled air space) take-of f take-of f distance take-of f distance available take-of f distance required take-of f run take-of f run required take-of f run available take-of f weight turn and slip indicator torque and temperature limiting

ultra high frequency United Kingdom underwater locator beacon

21006110

~. ' '

us USG uvs V V1 V2 V4 VA VFR VHF VLE VLO VMCA VMCG VMCL

VMO VMS VOR VR VRA VREF VRL Vs Vsr VsTOP Vx Vy WAT W/C wow WRS W/S Wt W/V YD ZFW

BRl77SHAERDSPACE

JETSTREAllll SEIES J200



United States of America underspeed governor (fuel governor) under voltage sensor volts decision speed take-of f safety speed design manoeuvring speed design manoeuvring speed visual f light rules very high frequency radio communication landing gear extended limit speed landing gear operating limit speed minimum control speed in the air minimum control speed on the ground minimum control speed in the approach and landing conf iguration maximum operating limit speed minimum speed in the stall very high f requency omni directional range rotation speed rough air speed final approach and landing speed variable red line stall speed vertical speed indicator decision to stop speed on icy or slippery runway

one engine inoperative best angle of climb speed (equal to V2) one engine inoperative best rate of climb speed weight, altitude, temperature wind component weight-on-wheels weather radar system windshield weight wind velocity yaw damper zero-fuel weight

1-1

Page 7/8 21006111

Nov 15/98

BRl77SH AllROSPACE



DEFINITIONS

- Take-of f decision speed, the speed to be used as a reference, in the event of an engine or other failure at take-of f in deciding whether to continue or abandon the take-off.

- Rotation speed, the target speed at which the pilot initiates a change in the attitude of the aircraft with the intention of leaving the ground.

- Take-off safety speed, the initial climb out speed, one engine inoperative.

- Steady initial climb speed, the initial climb out speed, all engines operating.

VMcA- Minimum control speed in the air, in a take-off configuration. The mimimum speed at which it is possible to suf fer an engine failure and still maintain directional control within the set limits.

VMcG- The minimum control speed on the ground. The minimum speed at which it is possible to maintain adequate directional control af ter an engine failure during the take-off run.

VAT - Target threshold speed. The speed at which the pilot aims to cross the runway threshold when landing. A numerical suf f ix , 1 or O , indicates the number of engines inoperative.

1-2

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Jan 15/00

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o o -N

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-~ .. ~ JETSTREAWI SERiES }200


QNH-QFE pressure altitude Fig. 1

t ~

;;: I

, .. '

' , , 1 -!.: ' t! ; ~ 1 ~ ,..~ t t

1, ~ : ',, ! 1r1

' ~ ' .

r r ' ... t ., , . .. 1

1-3

Page 1

Feb 15/89

-~A-.-..0.

JETSTREAAH . SERiES 1200

MANUFACTURERS OPEFJATING MANUAL PART 1

EXAMPLE CONVERT 12535 lb to kg 12500 lb = 5670 kg 35 lb = 16 kg 12535 lb = 5686 kg lb X 0.4536 = kg

LB o 100 200 300 400 500 600 700 800 900

10000 4536 4581 4627 4672 4717 4763 4808 4854 4899 4944

11000 4990 5035 5080 5126 5171 5216 5262 5307 5352 5398

12000 5443 5489 5534 5579 5625 5670 5715 5761 5806 5851

13000 5897 5942 5987 6033 6078 6124 6169 6214 6260 6305

14000 6350 6396 6441 6486 6532 6577 6623 6668 6713 6759

o 1 2 3 4 5 6 7 8 9

o o o 1 1 2 2 3 3 4 4

10 5 5 5 6 6 7 7 8 8 9

20 9 10 10 10 11 11 12 12 13 13

30 14 14 15 15 15 16 16 17 17 18

40 18 19 19 20 20 20 21 21 22 22

so 23 23 24 24 24 25 25 26 26 27

60 27 28 28 29 29 29 30 30 31 31

70 32 32 33 33 34 34 34 35 35 36

80 36 37 37 38 38 39 39 39 40 40

90 41 41 42 42 43 43 44 44 44 45

Conversion - Pounds (lbs) to Kilogrammes (kgs) Figure 2

1-3

Page 2

Feb 15/89

\',

N -o o -co N N

< .., -

f"'} N c:o

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EXAMPLE CONVERT 5686 kg to lb 5650 kg = 12456 lb 36kg = 79.37 lb 5686 kg = 12535 lb kg X 2.20462 : 16

KG o

4000 8818

4500 9921

5000 11023

5500 12125

6000 13228

6500 14330

o

o o

10 22

20 44

30 66

40 88

so 100 150 200 250 300 350

8929 9039 9149 9259 9370 9480 9590

10031 10141 10251 10362 10472 10582 10692

11133 11244 11354 11464 11574 11684 11795

12236 12346 12456 12566 12677 12787 12897

13338 13448 13558 13669 13779 13889 13999

14440 14550 14661 14771 14881 14991 15102

1 2 3 4 5 6 7

2 4 7 9 11 13 15

24 26 29 31 33 35 37

46 49 51 53 55 57 60

68 71 73 75 77 79 82

90 93 95 97 99 101 104

Conversion - Kilogrammes (kgs) to Pounds (lbs) Figure 3

400 450

9700 9811

10803 10913

11905 12015

13007 13117

14110 14220

15212 15322

8 9

18 20

40 42

62 64

84 86

106 108

1-3

Page 3

Feb 15/89

-~ JETSTREAAll . SERiES }200

MANUFACTURERS OPERATING MANUAL PART 1 EXAMPLE CONVERT 5656 ft to m 5600 ft = 1707 m 56ft = 17 m 5656 ft = 1724 m ft x 0.3048 = m

FT

o

1000

2000

3000

4000

5000 6000 7000

8000

9000'

10000

o

10

20

30 40

so

60 70

80

90 1-3

Page 4

Aug 188

o

o

305 610

914 1219

1524 1829 2134

2438

2743

3048

o

o

3

6 9

12

15 18

21

24

27

100 200 300 400 500 600

30 61 91 122 152 183

335 366 396 427 457 488

640 671 701 732 762 792

945 975 1006 1036 1067 1097

1250 1280 1311 1341 1372 1402 1554 1585 1615 1646 1676 1707 1859 1890 1920 1951 1981 2012 2164 2195 2225 2256 2286 2316 2469 2499 2530 2560 2591 2621 2774 2804 2835 2865 2896 2926

. 3078 3109 '3139 3170 3200 3231 1 2 3 4 5 6 o 1 1 1 2 2

3 4 4 4 5 5

6 7 7 7 8 8 9 10 10 10 11 11

12 13 13 13 14 14 16 16 16 16 17 17 19 19 19 20 20 20 22 22 22 23 23 23 25 25 25 26 26 26 28 28 28 29 29 29

CONVERSION-feet (ft) to metres (M) Fig. 4

700 800 900

213 244 274

518 549 579

823 853 884

1128 1158 1189

1433 1463 1494

1737 1768 1798 2042 2073 2103

2347 2377 2408

2652 2682 2713

2957 2987 3018

3261 3292 3322 7 8 9

2 2 3

5 5 6

8 9 9 11 12 12

14 15 15 17 18 18

20 21 21

23 24 24 27 27 27

30 30 - 30

1 ~

N -o o -

-

--o o -N

BRITl$H AERO~E

JETSTREANI SERiEs }200


EXAMPLE CONVERT 1724 m to ft 1700 m = 5577 ft 24 m = 79 ft 1724 m = 5656 ft m X 3.208 = ft

M o

o o

500 1640

1000 3281

1500 4921

2000 6562

2500 8202

3000 9843

o

o o

10 33

20 66

30 98

40 131

so 100 150 200 250 300 350

164 328 492 656 820 984 1148

1804 1969 2133 2297 2461 2625 2789

3445 3609 3773 3937 4101 4265 4429

5085 5249 5413 5577 5741 5906 6070

6726 6890 7054 7218 7382 7546 7710

8366 8530 8694 8858 9022 9186 9350

10007 10171 10335 10499 10663 10827 10991

1 2 3 4 5 6 7

3 7 10 13 16 20 23

36 39 43 46 49 52 56

69 72 75 79 82 85 89

102 105 108 112 115 118 121

135 138 141 144 148 151 154

CONVERSION-feet (ft) to metres (M) Fig. 5

400 450

1312 1476

2953 3117

4593 4757

6234 6398

7874 8038

9514 9678

11155 11319

8 9

26 30

59 62

92 95

125 128

157 161

1-3

Page 5 Aug 1/88

1-3

Page 6

Aug 1/88

~A~

JETSTREANI SeRiEs }200


ALTITUOE AMBIENTTEMPERATURE (DEG.C) (FT)

-35 -30

-25 -20 -15 -10

-5 o 5 o -so.o

-45.0 -40.0 -35.0

-30.0 -25.0

-20.0 -15.0 -10.0 1000

-48.0 -43.0 -38.0

-33.0 -28.0

-23.0 -18.0 -13.0

-8.0 2000 -46.0 -41.0 -36.0

-31.0 -26.0

-21.0 -16.0 -11.0

-6.0 3000 -44.1 -39.1 -34.1

-29.1 24.1 -19.1

-14.1 -9.1

-4.1 4000 -42.1 -37.1

-32.1 -27.1 -22.1 -17.1

-12.1 -7.1

-2.1 5000 -40.1 -35.1

-30.1 -25.1 -20.1

-15.1 -10.1

-5.1 -0.1

6000 -38.1 -33.1

-28.1 -23.1 -18.1

-13.1 -8.1 -3.1 1.9 7000 -36.1

-31.1 -26.1 -21.1

-16.1 -11.1

-6.1 -1.1 3.9 8000 -34.2

-29.2 -24.2 -19.2

-14.2 -9.2

-4.2 0.8 5.8 9000 -32.2 -27.2

-22.2 -17.2 -12.2

-7.2 -2.2 2.8 7.8 10000

-30.2 -25.2 -20.2

-15.2 -10.2 -5.2

-0.2 4.8 9.8 11000 -28.2

-23.2 -18.2

-13.2 -8.2 -3.2 1.8 6.8 11.8 12000 -26.2

-21.2 -16.2

-11.2 -6.2 -1.2 3.8 8.8 13.8 13000

-24.2 -19.2 -14.2

-9.2 -4.2 0.8 5.8 10.8 15.8 14000

-22.3 -17.3 -12.3

-7.3 -2.3 2.7 7.7 12.7 17.7 15000

-20.3 -15.3

-10.3 -5.3 -0.3 4.7 9.7 14.7 19.7

16000 -18.3

-13.3 -8.3 3.3 1.7 6.7 11.7 16.7 21.7 17000 -16.3

-11.3 -6.3

-1.3 3.7 8.7 13.7 18.7 23.7 18000 -14.3

-9.3 -4.3 0.7 5.7 10.7 15.7 20.7 25.7 19000 -12.4

-7.4 -2.4 2.6 7.6 12.6 17.6 22.6 27.6 20000 -10.4

-5.4 -0.4 4.6 9.6 14.6 19.6 24.6 29.6

21000 -8.4 -3.4 1.6 6.6 11.6 16.6 21.6 26.6 31.6 22000 -6.4 -1.4 3.6 8.6 13.6 18.6 23.6 28.6 33.6 23000

-4.4 0.6 5.6 10.6 15.6 20.6 25.6 30.6 35.6 24000 -2.5 2.5 7.5 12.5 17.5 22.5 27.5 32.S 37.5 25000 -0.5 4.5 9.5 14.5 19.5 24.5 29'.5 34.S 39.5

ALTITUOE AMBIENTTEMPERATURE (DEG.C) (FT)

10 15 20 25 30 35 40 45 so o -s.o o.o s.o 10.0 15.0 20.0 25.0 30.0 35.0 1000

-3.0 2.0 7.0 12.0 17.0 22.0 27.0 32.0 37.0 2000 -1.0 4.0 9.0 14.0 19.0 24.0 29.0 34.0 39.0 3000 0.9 5.9 10.9 15.9 20.9 25.9 30.9 35.9 40.9 4000 2.9 7.9 12.9 17.9 22.9 27.9 32.9 37.9 42.9 5000 4.9 9.9 14.9 19.9 24.9 29.9 34.9 39.9 44.9 6000 6.9 11.9 16.9 21.9 26.9 31.9 36.9 41.9 46.9 7000 8.9 13.9 18.9 23.9 28.9 33.9 38.9 43.9 48.9 8000 10.8 15.8 20.8 25.8 30.8 35.8 40.8 45.8 50.8 9000 12.8 17.8 22.8 27.8 32.8 37.8 42.8 47.8 52.8 10000 14.8 19.8 24.8 29.8 34.8 39.8 44.8 49.8 54.8

11000 16.8 21.8 26.8 31.8 36.8 41.8 46.8 51.8 56.8 12000 18.8 23.8 28.8 33.8 38.8 43.8 48.8 53.8 58.8 13000 20.8 25.8 30.8 35.8 40.8 45.8 50.8 55.8 60.8 14000 22.7 27.7 32.7 37.7 42.7 47.7 52.7 57.7 62.7 15000 24.7 29.7 34.7 39.7 44.7 49.7 54.7 59.7 64.7 16000 26.7 31.7 36.7 41.7 46.7 51.7 56.7 61.7 6f>.7 17000 28.7 33.7 38.7 43.7 48.7 53.7 58.7 63.7 68.7 18000 30.7 35.7 40.7 45.7 50.7 55.7 60.7 65.7 70.7 19000 32.6 37.6 42.6 47.6 52.6 57.6 62.6 67.6 72.6 20000 34.6 39.6 44.6 49.6 54.6 59.6 64.6 69.6 74.6 21000 36.6 41.6 46.6 51.6 56.6 61.6 66.6 71.6 76.6 22000 38.6 43.6 48.6 53.6 58.6 63.6 68.6 73.6 78.6 23000 40.6 45.6 50.6 55.6 60.6 65.6 70.6 75.6 80.6 24000 42.5 47.5 52.S 57.5 62.5 67.5 72.5 77.5 82.5 25000 44.5 49.5 54.5 59.S 64.5 69.5 74.5 79.5 84.5

1

TEMP.Rel. to ISA (ISA)/Amb.Temp./Press.Alt. Fig. 6

,-~('~~~\ \: ;-. }

-o o -

-N U1

--o o -N

EFFECTIVE HEAO'MNJ COMPONENT - KNOTS

EFFECTIVE TAIL'MNl COMPONENT - KNOTS

INWTISH AEROSPACE

JETSTREAWI SERiES J200


~--+-~--A_,, !-~-t-~--~---. ___ _. ____ j... ____ , .. L.--- -

~~------~--

1so

Wind Component Fig. 7

H/0/110

1-3

Page 7

Aug 1/88

1-3

....

i :r z w a:: :r

~

Page 8

Aug 1/88

BIWTISH AE~E

JETSTREANI SeRiES }200


"CENTIGRAOE CONVERSION C - F

Fig. 8 HI0/113

-o o -

-

40

38

36

34

32

30

28

26

-24 o

o o ,.. 22 >< -= w 20 e ::::> 18 1-::: ..J et: 16

14

12

10

8

6

4

SRn'TSH~SF"ACIT

JETSTREAAll SERiES J200


-80 60 -40 -20 o 20 40 60 TRUE OUTSIDE AIR TEMPERATURE -e 3201 001 2

Determination of Temperature in Relationship to ISA Fig. 9

21006162

1-3

Page 9

Nov 15/98

"' ~ ,,,

-~

o w w a.. UJ

1-3

Page 10

Nov 15/98

Q co N

o 11:1' N

o N N

o o N

o CIO ....

o co ....

o 11:1' ....

o N ....

o o ....

BRl77SH AIROSFJll&Jll



3103_031 2

....

1 N

1 C") o::!' U) co

1 1 1 .... CIO

1 1 Q)

1 o ....

1

....

....

1

CORRECTION TO INDICATED OAT - C

N ....

1

C") ....

1

Indicated Outside Air Temperature Corrections Fig. 10

21006043

-o o -N

~AEROSPACE

JETSTREANI SERES J200


CHAPTER l. GENERAL

LIST OF CONTENTS


LIMIT~TIONS

General

Weights

Speeds

Kinds of Operation Equipment List

Operating Limitations Placard

Standby Compass Placard

1-1-1

1-1-3

1-1-4

1-1-7

1-1-9

1-1-10

CHAP.1 CONTENTS

Page 1/2

Oct 15/88

LIST OF CONTENTS LIST OF

:.: EFFECTIVE PAGES ::::> CI> 1-1 -E e:

"'O CI>

-~ tt'

BRIT7SH AEROSFMCE

JETSTREANI SERiEs 'J200


CHAPTER 1

GENERAL


1/2 Oct 15/88

1/2 May 15/91 1 May 15/90 2 May 15/91 3 Aug 1/88 4 Sep 15/89 5 May 15/91 6 Sep 15/88 7 May 15/90 8 Aug 1/88 9 Apr 15/89 10 Aug 1/88

CHAPTER 1 LIST OF EFFECTIVE PAGES

Page 1/2

May 15/91

, ..... ,

e

r-ri o o

N

LIMITATIONS

l. GENERAL

BRITrSH AEROSFMCE



CHAPTER l. GENERAL

1.1 Category and use of aeroplane

This aircraft is certificated in the Commuter Category.

1.2 Manoeuvres

Operation is limited to normal flying manoeuvres. Aerobatic manoeuvres are not permitted. The maximum positive normal accelerations (i.e. load factors) which the structure has been designed to withstand without permanent deformation are +3.02g with flaps up and +2.0g with flaps down. Intentional manoeuvres shall be confined to those with load factors below these values.

1.3 Minimum flight crew

The minimum crew is two pilots.

1.4 Maximum number of occupants

The total number of occupants carried, including crew, shall not exceed 21, nor the number fer which seating accommodation, which is approved fer take-off and landing, is provided.

Children under the age of two years who are carried in the arms of passengers are excluded from this count.

1.5 Maximum air temperature

Operation of this aeroplane is not permitted when the air temperature at take-off exceeds ISA +37C.

1.6 Maximum altitude

The maximum permissible altitude is 25,000 ft.

1-1-1

May 15/90

BR'TISH AEROSPMCE

JETSTREANI SERiEs '}200


1.7 Smoking

smoking in the toilet,if fitted, is prohibited. Placards summarising the above limitation shall be provided inside and outside the toilet and shall not be obscured.

1.8 Baggage Compartment Door

The baggage compartment door shoot-bolts must be in the locked position for take-off, in flight and landing. If a security lock is fitted, the baggage compartment door may be locked but take-off is prohibited if the spare key for the security lock is not in the correct flight deck stowage.

1.9 Toilet Door/Vestibule Curtain

The toilet door and/or vestibule curtain ,if fitted, must not obstruct the aisle during take-off and landing.

2. WEIGHTS

2.1 Maximum Taxying Weight

The maximum permissible taxying ramp weight is 16314 lb.

2.2 Maximum Take Off Weight

The maximum permissible take off weight is 16204 lb or as limited by the following:

2.2.1 The maximum take off weight appropriate to the altitude and ambient air temperature of the airfield as given by the take off WAT curve.

2.2.2 The weight at which the take off distance required is eqtial to the take off distance available.

2.2.3 The weight at which the accelerate-stop distance required is equal to the accelerate-stop distance available.

2.3 Maximum Landing Weight

1-1-2

The maximum permissible landing weight is 15609 lb or as limited by the following:

2.3.l The maximum landing weight appropriate to the altitude and ambient air temperature of the airfield as given by the landing WAT curve.

May 15/91

::.:: ::i

BRITISHA~E



2.3.2 ,The weight at which the calculated landing distance required is equal to the landing distance available.

2.4 Maximum zero fuel weight

The total loaded weight of the aeroplane less the weight of usable f uel in the wing tanks shall not exceed 14330 lb.

~ 3. SPEEDS .: ] a..

!'\')

B#NTISH AEROSPACE

JETSTREAWI SERiEs }200


3.3 V2 Take Off Safety Speed

FIELD PRESS TEMPERATURE DEGREES C ALT.

o < o 8 16 23 30 37 44 51 52 1000 < -2 5 12 19 26 33 40 47 50 2000 < -5 2 9 16 23 30 37 44 48 48 3000 < -7 - -1 6 13 20 27 33 40 46 4000 < -9 -3 4 10 17 23 30 37 5000 < -12 -5 1 7 14 20 27 6000 < -14 -8 -1 5 11 18 7000 < -16 -10 -4 2 8 8000 < -18 -12 -6 o 9000 < . -21 -16 -10

10000 < -24 -19

WT LB V2 - KNOTS

16204 116 116 116 116 116 116 116 116 116 116 1.16 116 16120 116 116 116 116 116 116 116 116 116 116 116 116 15840 115 115 115 115 115 115 115 115 115 115 115 115 15570 114 114 114 114 114 114 114 114 114 114 114 114 15300 114 113 113 113 113 113 113 11'3 113 113 113 113 15020 114 113 112 112 112 112 112 112 112 112 112 112

1 14760 114 113 112 111 111 111 111 111 111 111 111 111 14500 114 113 112 111 110 110 110 110 110 110 110 110 14230 114 113 112 111 110 110 109 109 109 109 109 109 13970 114 113 112 111 110 109 108 108 10~ 108 108 108 13720 114 113 112 111 110 109 108 107 107 107 107 107 13470 114 113 112 111 110 109 108 107 106 106 106 106 13220 114 113 112 111 110 109 108 107 106 105 105 105 12970 114 113 112 111 110 109 108 107 106 105 104 104 12720 114 113 112 111 110 109 108 107 106 105 104 103 11000 114 113 112 111 110 109 108 107 106 105 104 103

USA & CAN

VR = V2 MINUS 3 KNOTS

1-1-4

Sep 15/89

O'-"J ;) 0 .l

~~

,--i

BRITISH AEROSF'lllCE



4. KINDS OF OPERATION EQUIPMENT LIST This aeroplane may be operated in day or night VFR, day or night IFR and known or forecast icing conditions when the appropriate equipment is installed and operable.

The following equipment list identifies the systems and equipment upen which type certif ication f or each kind of operation was given. Unless the aeroplane is operated in accordance with a current Minimum Equipment List (MEL) issued by the FAA, the following systems and items of equipment must be installed and operable for the particular kind of operation indicated.

Note:- The zero's (O) used in the following list mean the equipment and/or system was not required for type certification for that kind of operation.

4.1 Electrical power (ATA 24) VFR IFR ICING

DAY NIGHT DAY NIGHT CONDITION Batteries 2 2 2 2 2 DC Generators 2 2 2 2 2 Gen fail warn lights 2 2 2 2 2 Gen output ammeters 2 2 2 2 2 Busbar voltmeter 1 1 1 1 1 Inverter 2 2 2 2 2 AC f ail warning light 1 1 1 1 1 Inv fail warning light o 1 1 1 1 DC Main bus f ail

warning lights 1 1 1 1 1 Batt contact open wrn lts 2 2 2 2 2

4.2 Equipment/furnishings (ATA 25) Illuminated EXIT signs 3 3 3 3 3 Seat belts Required f or ea ch seat Shoulder harness Required f or ea ch crew seat Fasten Seat Belts/No Smoking Signs 1 1 1 1 1

4.3 Fire Protection (ATA 26) Powerplant f ire detection 2 2 2 2 2 Powerplant f ire

extinguishing 2 2 2 2 2 Portable f ire

extinguisher 2 2 2 2 2 Smoke detection(aircraft) 1 1 1 1 1

(Baggage Pod) 1 1 1 1 1

1-1-5

May 15/91

BRITTSH AEROS#WCE JETSTREAIW SERiES }200

MANUFACTURERS OPERATING MANUAL PART 1 ,,.,,

4.4 Flight Controls (ATA 27) VFR IFR ICING

DAY NIGHT DAY NIGHT CONDITION Stall warn & protection 2 2 2 2 2 Wing flaps & position ind. 1 1 1 1 1 Elev trirn & trirn ind. 1 1 1 1 1 Aileron trirn & trirn ind. 1 1 1 1 1 Rudder trirn & trirn ind. 1 1 1 1 1

4.5 Fuel systern (ATA 28) ~

Fuel boost purnps 2 2 2 ::: 2 2 ' c. Fuel low pressure warn lights 2 2 2 2 2 :::

Fuel pressure ind. 2 2 2 2 2 ;. ('.) Fuel quantity ind. 2 2 2 2 2 e ;:

BRITISH AEROSPACE

JETSTREAIW SrniEs }200

MANUFACTURERS OPERATING MANUAL PART 1 r-' , :\ J~J -

4.9 Lights (ATA 33) VFR IFR ICING

DAY NIGHT DAY NIGHT CONDITION Flight deck and instrument (required illumination) o 1 o 1 o Anti-collision lights o 2 o 2 o Landing lights o 1 o 1 o Position lights o 3 o 3 o Ice observation light o o o 1 o Emergency lighting system o 1 o 1 o ~ ::> 4.10 Navigation (ATA 34) ., .:: ...

e

"O Altimeters 2 2 2 2 2 ! Airspeed ind. 2 2 2 2 2 a.. Magnetic direction ind. 1 1 1 1 1

Outside air temp ind. 1 1 1 1 1 Vertical speed ind. 1 1 2 2 2 Turn and slip ind. 1 1 2 2 2 Gyro horizon ind. 2 2 2 2 2 Clock o o 1 1 1 Alternate static source o o 1 1 1 Directional Gyro (HSI) 2 2 2 2 2

4.11 Doors (ATA 52) Door unlocked warn system 1 1 1 1 1

4.12 Propellers (ATA 61) Propeller reversing system 2 2 2 2 2 Reverse pitch warn lights 2 2 2 2 2 Beta range warn lights 2 2 2 2 2

"" 4.13 Engine fuel system (ATA 73)

i"")

""

Fu el flowmeter ind. 2 2 2 2 2 o o 4 .14 Engine anti-icing system (ATA 74) N Continuous ignition system o o 2 2 2

4.15 Engine anti-icing systern (ATA 75) Engine anti-icing system o o 2 2 2

1-1-7

May 15/90

4.16

4.17

4.18

Engine

BRITISH AEROSPl4CE

JETSTREAJW SrniES }200


controls (ATA 76) VFR IFR

DAY NIGHT DAY NIGHT Single red line computer 1 1 1 1 Neg. torque sensing system 2 2 2 2

Engine indicating systems (ATA 77) Torque ind. 2 2 2 2 RPM ind. 2 2 2 2 EGT ind. 2 2 2 2

Engine oil system (ATA 79) Oil temperature ind. 2 2 2 2 Oil pressure ind. 2 2 2 2 Low oil pressure warn

lights 2 2 2 2 Oil cooler flap control &

ind. 2 2 2 2 Metallic contamination

detection system 2 2 2 2

ICING CONDITION

1 2

2 2 2

2 2

2

2

2

Notes: l. The above system and equipment list is for a crew of two pilots.

1-1-8

Aug 1/88

2. Equipment and/or systems in addition to those listed above may be required by operating regulations. (FAR Part 135).

3. The above system and equipment list does not include all specif ic f light instruments and communications/ navigation equipment required by the FAR Parts 91 and 135 operating requirements.

t. ;--.. ~'.\

~ :; ... .. o. ::> ...

;r ..

e ;;

-N

B~ AEROSPACE

JETSTREAA# SERiEs }200


JETSTREAM SERIES 3200 OPERATING LIMITATIONS

THIS AIRPLANE MUST BE OPERATED AS A COMMUTER CATEGORY AIRPLANE IN COMPLIANCE WITH THE OPERATING LIMITATIONS STATED IN THE FORM OF PLACARDS MARKING ANO MANUALS. NO ACROBATIC MANEUVERS, INCLUDING SPINS APPROVED CABIN MUST NOT BE PRESSURIZED DURING TAKE OFF ORLANDING

APPROVED TYPES OF OPERATION

DAY/NIGHT, VFR/IFR ANO ICING CONDITIONS :-SEE AFM FOR REQUIRED EQUIPMENT LIST

AIRSPEED LIMITATIONS DESIGN MANEUVERING SPEED . . . . . . . . . . . 180KT IAS ROUGH AIR SPEED . . . . . . . . . . . . . . . . . . . . . . 185KT IAS MAXIMUM FLAP EXTENSION SPEEEDS --

-100 . . . .. ... . . . . . . . . . . 170KTIAS -20 . . . . . . . . . . . . . . . . . . 160KT IAS -35 . . . . . . . . . . . . . . . . . . 150KT IAS -70 . . . . . . . . . . . . . . . . . . 120KT IAS

MAXIMUM LANDING GEAR OPERATING ANO EXTENDED SPEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 160KT IAS

POWER PLANT LIMITATIONS MAXIMUM ROTATIONALSPEED

CONTINUOUS . . . . . . . . . . UP TO 100.0% UPT05MINUTES .... 100.0-101.5% UPT030SECONDS .. 101.5-105.5% UP TO 5 SECONDS . . . . 105.5 -106.0% NEVER EXCEED . . . . . . . . . . 106.0%

MAXIMUM TORQUE . . . . . . . . . . . . . . . . . 100.0% MAXIMUM EGT; TAKE OFF ANO CONTINUOUS . . 650C

' DURING STARTING . . . . . . . . . . 770C OIL TEMPERA TU RE; MINIMUM FOR STARTING -30C

MAXIMUM UP TO 88% TORQUE 127C (10 MINUTE LIMITOVER 110C) MAXIMM OVER 88% TORQUE 110C

OIL PRESSURE; MINIMUM-GROUND IDLE 40PSI -BELOW 23000FT . . . . 70PSI -ABOVE 23000FT . . . SOPSI

MAXIMUM . . . . . . . . . . . . . . . . . . . 120PSI FUEL PRESSURE; MINIMUM - GROUND IDLE . . . . . 15PSI

NORMAL . . . . . . . . . . . . . . . . . . . 20-80PSI MAXIMUM . . . . . . . . . . . . . . . . . . . . 90PSI

PT N 03710962L 17 ISS.2 KIT 3384A/2

H,1 573X

OPERATIONS LIMITATIONS PLACARD Fig.l.

1-1-9

Apr 15/89

1-1-10

Aug 1/88

J~~ AE.ROSPACE

-JETSTREA/111 SERiEs J200


CALIBRATION IS ONL Y VALID WHEN BOTH GENERATORS ANO WINDSCREEN HEATERS ARE SWITCH ED OFF

H/11223X

STANDBY COMPASS PLACARD Fig.2.

N -o o -

-

BRITISH AERO~E



CHAPTER 2. AIRFRAME. FLYING CONTROLS & STALL WARNING

LIST OF CONTENTS


LIMITATIONS & ESSENTIAL DATA . . . . . . . . . . . . . . . . 2-1-1

CONDITIONAL PROCEDURES

Flight with Missing Vortex Generators . . . . . . . . . 2-2-1

ABNORMAL PROCEDURES

C.A.P. lsTALLI caption on ............... 2-3-1

EMERGENCY PROCEDURES

Window Failure . . . .

C.A.P. loooRI caption

2-4-1

on . . . . . . . . . . . . . . . 2-4-3

CHAP. 2 CONTENTS

Page 1/2

May 15/91

N

BRrTISH AERO~E

JETSTREANI SERES }200


CHAPTER 2

AIRFRAME, FLYING CONTROLS & STALL WARNING

LIST OF CONTENTS 1/2 LIST OF EFFECTIVE PAGES 1/2 2-1 1/2 2-2 1/2 2-3 1/2 2-4 1

2 3 4


May

May Aug May May May May May May

15/91

15/91 15/90 15/91 15/91 15/91 15/91 15/91 15/91


Page 1/2

May 15/91

N

BRfTISH AEROSPMCE



CHAPTER 2

AIRFRAME, FLYING CONTROLS & STALL WARNING

l. LIMITATIONS

1.1 Manoeuvring speed

Manoeuvres likely to involve full application of the primary flight controls shall not be attempted at a speed greater than 180 kt IAS.

1.2 Stall protection

The serviceability of both stall protection systems must be conf irmed prior to the f irst flight of the day by carrying out the relevant checks.

1.3 Control locks

If the tailwind component exceeds 20 kt, the control locks shall be engaged whenever the aircraft is taxiing or parked.

1. 4 Lift Dump

The maximum permissible speed f or allowing the flaps to extend to the lift DUMP position is 120 kt IAS.

l. 5 DV Window

The maximum permissible speed with the DV window open is 140 kt IAS.

2. ESSENTIAL DATA

2.1 Stall Protection

If one wing reaches the stall warning angle, the audio warning and stick shaker will activate.

If one wing reaches the stall identification angle, the stall ident lights will come on. If both wings reach this condition the stick pusher will activate until clear of stall identification angle. Stick pusher may be over-ridden by an 80 lb. pull force.

2.2 Crosswind

The maximum demonstrated crosswind component f or take-of f and landing is 25 kts.

2-1-1/2

Aug 15/90

e:

BRITISH AEROSFWCE



CONDITIONAL PROCEDURE

FLIGHT WITH MISSING VORTEX GENERATORS

Flight with one or more vortex generators missing is permitted far up to eight flights or one day's flying, whichever is the least, under the following conditions:-

l. One vortex generator may be missing. from either one wing or both wings, or

Two vortex generators may be missing from either one wing or both wings provided that they are not adjacent. If a third vortex generator is missing from either wing it must be replaced befare flight.

2. Flight is not permitted if any vortex generator is missing from the wing root fillets.

3. Far flight with vortex generators missing, the wing surface and wing root fillet must be in good condition and free from damage.

4. The airplane must not be used far stall or single-engined training if any vortex generators are missing.

END//

2-2-1/2

May 15/91

~ :::i .,

-= e:

-o ~ = .t

EIRIT7SH AEROSPMCE



ABNORMAL PROCEDURE

C.A.P. 1 STALL 1 CAPTION ON

Indicates STALL WARNING inoperative due to any of the following:-

l. 2. 3. 4.

STALL PROTECTION switch at OFF or TEST Power relay failure ssu failure Signal to pusher solenoid has been cancelled by the isolate relay.

CHECK STALL PROTECTION ..................... ON

CIRCUIT BREAKERS . . . . . . . . . . . . . . . TRIP/RESET

Far RightJ STALL Jc.A.P. trip/reset C/B STALL PROT RIGHT (5) on the DC Main C/B Panel

Far Left 1 STALL lc.A.P. trip/reset C/B STALL PROT LEFT (5) on the DC Essential C/B Panel

If caption remains on avoid flight conditions approaching the stall.

Note: If either of the STALL ident lights has been pressed, the stick pusher will remain inoperative until reset on the ground.

END//

2-3-1/2

May 15/91

BRITISH AEROSPACE

JETSTREANI SERies J200


EMERGENCY PROCEDURE

WINDOW FAILURE

FLIGHT DECK OR CABIN

INNER OR OUTER PANEL CRACKED CRAZED OR FAILED

WARNING : IF PART OF A WINDOW BECOMES DETACHED IT MAY STRIKE A PROPELLER AND BE DEFLECTED THROUGH THE SIDE OF THE FUSELAGE. AS A PRECAUTION AGAINST INJURY MOVE PASSENGERS FROM SEATS IN LINE WITH THE PROPELLER IF PRACTICAL.

CABIN DIFF .............. REDUCE TO 2.5 psi THEN ZERO

Immediately reduce cabin differential pressure to 2.5 psi and as soon as practicable to zero.

SEAT HARNESS . . . . . FITTED

Verify both pilots seat harnesses are fitted.

CABIN SIGNS . . . . . . . . . . . . . . . . . . . . . . . . . . ON

OXYGEN AS REQUIRED As differential pressure is going to be reduced to zero consideration should be given to the use of oxygen by crew.

DESCEND . . TO SAFETY ALTITUDE

Descend to safety altitude for sector being flown.

( cont) / ...

2-4-1

May 15/91

FLIGHT DECK

lll#TWIA~W

JETSTREAIW SERES J200


EMERGENCY PROCEDURE

WINDOW FAILURE (cent)

INNER OR OUTER PANEL DELAMINATED

SLIGHT DELAMINATION OF INNER OR OUTER PANEL IS ACCEPTABLE WITHOUT RESTRICTION FOR THAT FLIGHT PROVIDING VISION IS NOT IMPAIRED.

CAUTION: SUBSTANTIAL DELAMINATION SHOULD BE TREATED AS A POTENTIAL FAILURE. FRACTURE OF A DELAMINATED INNER LAYER COULD CAUSE GLASS SPLINTERS TO BE RELEASED INTO THE FLIGHT DECK.

END//

2-4-2

May 15/91

' ...... .

e

-77SHA~ICE

JETSTREANI SERiEs l200


Tbis rev1s1on complies with Britisb Civil Cbapter A7-3.

Airwortbiness Requirements, Section A

Signed /~~ JETSTREAM AIRCRAP'T LIMITED PRESTWICK AIRPORT, Date ~~ 'J AYRSBIRE, ll9 2RW, SCOTLAHD CAA Approval No: DAI/9386/92

Publication Ref No.SA.4-3100/MOM/53,57,58,61,63,64,266,267, 269,270.

TEMPORARY REVISION 2 - 1

Location: Insert in Chapter 2 with the page overleaf facing Page 2-4-3.

Reason:

Action:

To revise C.A.P. loooRI CAPTION ON emergency procedure.

Replace ON GROUND procedure with the procedure overleaf.

The introduction of data by revLSLons or amendments or temporary revisions or amendments not certified in accordance with British Civil Airworthiness Requiremente, Chapter A7-3, will invalidate the initial certification en the title page of the manual relative to the part revised. Revisions or amendments or temporary revisione or amendments embodied in this manual and certif ied by an appropriate approved organisation, other than that applicable to the initial certification, must be recorded en separate record sheets.

Page 1 of 2

Jun 7/93

~A~tCE

JETSTREAIW ' SERiES J200

MANUFACTURERS OPERATIN~ MANUAL PART 1

EMERGENCY PROCEDURE

c.A.P. lnooRI CAPTioN oN

ON GROUND

DOOR ... OPEN FROM INSIDE

open the door and leave it open.

ENT DOOR WRN C/B . TRIP/RESET

Trip and reset the ENT DOOR WRN C/B on the DC ESS busbar.

WARNING: THE DOOR MUST REMAIN OPEN FOR A MINIMUM OF 15 SECS TO ALLOW TIME FOR THE TIME DELAY RELAX TO FUNCTION IF ANY OF THE MICROSWITCHES HAVE FAILED IN THE DOOR CLOSED POSITION.

Wait for 15 secs then:

DOOR

DOOR HANDLE

DOOR DRAWBOLT-LOCKED INDICATORS (5)

DOOR HANDLE-LOCKED INDICATOR . .

CLOSE ANO LOCK FROM INSIDE

FULLY OUTBOARD

. . CONFIRM ALIGNED

. . . CONFIRM ALIGNED

IF DOOR CAPTION REMAINS ON OR IF CAPTION NOT ON WHEN DOOR OPENED

DIFFERENTIAL PRESSURE MINIMUM FOR FLIGHT

Select the mnimum cabin dif f erential pressure acceptable f or the flight.

SEAT BELT SIGN . . . . ON FOR DURATION OF FLIGHT

Notes: l. A single flight or series of flights is permitted with

C.A.P. lnooRj on if all drawbolt-locked and handle-locked indicators show door locked and secure.

END//

2. The airplane must not depart an airfield where repairs or replacements can be made.

(cent)/ .... Page 2 of 2

Jun 7/93

' '\' .

e

L.() -:r

BRITISH AEROS#WCE



EMERGENCY PROCEDURE

C.A.P. DOOR CAPTION ON

ON GROUND

DOOR . . . OPEN

Open the door and leave it open.

ENT DOOR WRN C/B . ..... TRIP/RESET

Trip and reset the ENT DOOR WRN C/B on the DC ESS busbar.

WARNING: THE DOOR MUST REMAIN OPEN FOR 15 SECONDS TO ALLOW TIME FOR THE TIME DELAY RELAY TO FUNCTION IF ANY OF THE MICROSWITCHES HAVE FAILED IN THE DOOR CLOSED POSITION.

DOOR .. CLOSE

VISUAL DOOR INDICATORS . CHECK

IF DOOR LIGHT REMAINS ON OR IF CAPTION NOT ON WHEN DOOR OPENED

DIFFERENTIAL PRESSURE MINIMUM FOR FLIGHT

Select the minimum cabin differential pressure acceptable for the flight.

SEAT BELT SIGN . . . . . . . . . . ON

Note: l. A single flight or a series of flights is permitted with

C.A.P. 1 DOOR 1 caption on provided door visual

indicators show door is locked.

END//

2. The airplane must not depart an airfield where repairs or replacements can be made.

( cont) / .

2-4-3

May 15/91

IN FLIGHT

BRrTISH AEROSFMCE



EMERGENCY PROCEDURE

C.A.P. DOOR CAPTION ON (cont)

WARNING: DO NOT TOUCH THE DOOR OR HANDLE

SEAT BELT SIGN

DIFF PRESS . .

Reduce cabin differential pressure to rninirnurn consistent with flight altitude.

LAND AS SOON AS PRACTICABLE

END//

2-4-4

May 15/91

,'

. . ON

REDUCE

e::

co N '-O

o o

N

BRPTISHA~



CHAP.3 AIR CONDITIONING & PRESSURISATION

LIST OF CONTENTS


LIMITATIONS & ESSENTIAL DATA

ABNORMAL PROCEDURES

3-1-1

C.A.P.,AIR OFFI caption on ............... 3-2-1

C.A.P. caption on 3-2-2

C.A.P. lnucTI caption on ................ 3-2-3


Cabin Differential Pressure greater than 6 psi .

e. A. P. 1CABIN1 caption on . . . . . . . . . Emergency Descent

3-3-1

. . 3-3-3

3-3-4

CHAP . 3 CONTENTS

Page 1/2

Dec 1/88

LIST OF CONTENTS LIST OF

:. EFFECTIVE PAGES :;)

"' 3-1

-5 3-2 e: -o

"' . a.. 3-3

BRITISH AEROSl'WCE



CHAPTER 3

AIR CONDITIONING & PRESSURISATION


1/2 Dec 1/88

1/2 May 15/91 1/2 Aug 1/88 1 Aug 1/88 2 Aug 1/88 3/4 Dec 1/88 1 Aug 1/88 2 Aug 1/88 3 Feb 15/90 4 May 15/91


Page 1/2

May 15/91

~ 00 f'.... o o o -N

~AEROSPACE

JETSTREANI SERiEs .,200


CHAPTER 3

AIR CONDITIONING & PRESSURISATION

l. LIMITATIONS

2.

Maximum Dif ferential Pressure

Highest Normal Working Pressure

. 6.0 psi

. 5.5 psi

During take-off and landing the cabin shall not be pressurised and the air FLOW supply selectors shall be OFF.

ESSENTIAL DATA

Inward Relief Valve

Safety Relief Valve . . . .

0.3 psi

5.8 psi

Absolute Air Pressure Regulator limits Cabin Alt to 13,000 feet.

3-1-1/2 Aug 1/88

Ui CX) r-o o o -N

~,:_EROSPACE 3~STREANI SERiEs J200

MANUFACTUREBS OPERATING MANUAL PART 1

ABNORMAL PROCEDURE

C.A.P. IAIR OFF CAPTION ON

CAUTION: ONE ATTEMPT ONLY MAY BE MADE TO REGAIN THE AFFECTED SYSTEM AS FOLLOWS:-

FLOW SELECTOR . . . .

Rotate the associated FLOW selector to OFF.

OFF

EMER AIR OFF CONT C/B TRIP/RESET

Trip the associated EMER AIR OFF CONT circuit breaker on the DC Essential Bus C/B Panel. This releases the latch on the emergency air off valve and allows the valve to open when the circuit breaker is reset.

FLOW SELECTOR INCREASE SLOWLY

Rotate associated FLOW SELECTOR slowly open to an initial position less than that at which the shut off occurred. Do not open too quickly as a rapid increase to airf low may cause the valve to close.

IF THE C.A.P. AIR OFF lcAPTION COMES ON AGAIN: FLOW . . . . . . . . . . . . . . . . . . . . . . . . . . OFF

OPPOSITE FLOW SELECTOR . . . . . . . . . . . . . . . . . IN CREASE

If possible increase the opposite airf low in an attempt to maintain the environmental conditions.

END//

3-2-1 Aug 1/88

lllWTISH AEROSPACE



ABNORMAL PROCEDURE

C.A.P. 1 O/TEMP l CAPTION ON PAUSE FOR 5 SECONDS TO ALLOW SHUT OFF VALVE TO CLOSE THEN :-

ASSOCIATED TEMP AUTO/MAN SELECTOR

Set the associated TEMPERATURE AUTO/MANUAL selector to OFF in an attempt to let the temperature control system stabilise.

HAS C.A.P., O/TEMP CAPTION GONE OFF?

YES i--~ ASSOCIATED TEMP AUTO /MAN SELECTOR

OFF

AUTO

Set the associated TEMPERATURE AUTO/MANUAL

seletor to AUTO and monitor the,O/TEMPlcaption.

NO IF O/TEMP CAPTION REMAINS ON OR COMES ON AGAIN AFTER

PREVIOUS ACTION

TEMPERATURE . . . . . . . . . REDUCE MANUALLY

Adjust the temperature by INC or DEC selections of the associated AUTO/MAN selector.

IF O/TEMP 1 CAPTION REMAINS ON AND MANUAL CONTROL UNSUCCESSFUL:

FLOW SELECTOR . . . . . . . . . . . . . . . . . . . . OFF

Rotate the associated FLOW selector to OFF. This shuts off the air bleed to the failed system.

OTHER FLOW SELECTOR

Rotating the usable FLOW rotary selector to a higher setting to replace the flow from the f ailed system.

END//

3-2-2

Aug 1/88

ADJUST

('.e

N -o o -

o o

N

BRITl:!IN AEROSPACE

JETSTREANI SERiES }200


ABNORMAL PROCEDURE

c.A.P. jnucTI CAPTION oN

ON THE GROUND

ASSOCIATED STOP BUTTON . . PRESS

Stop the engine and investigate cause of failure.

IN FLIGHT

ASSOCIATED FLOW SELECTOR . . . . . . . . . .

Rapidly rotate the associated FLOW selector to OFF. Check for reduction in f low by observing movement of Cabin Rate of Climb and by feel from the vents. Start stop-watch. Observe the reduction in flow; this confirms that the valve has closed.

PPOSITE FLOW SELECTOR . . . . .

. OFF

IN CREASE

Increase opposite airflow to maintain cabin pressurisation

AFTER 3 MINUTES ON STOPWATCH, IS C.A.P. DUCT STILL ON ?

TAKE NO FURTHER ACTION. REPORT DEFECT ON LANDING

DID FLOW REDUCE ?

YES TAKE NO FURTHER ACTION. REPORT DEFECT ON LANDING

Note: If C.A.P. remains on 5 minutes after engine shut down it can be assumed to be a false warning and the engine may be relit for a normal two engined landing

END// 3-2-3/4

Dec 1/88

' ""-

o o -N

B/INTISH AEROSPACE

JETSTREANI SERiEs 1200


EMERGENCY PROCEDURE

CABIN DIFFERENTIAL PRESSURE GREATER THAN 6 PSI

CABIN DIFFERENTIAL

Confirm by reference to cabin/altitude table that differential pressure exceeds 6 psi.

IS DIFFERENTIAL PRESSURE CONFIRMED?

t--~ LOG FAULTY GAUGE.

YES 1--_.. AIRFLOWS

Slowly reduce FLIGHT DECK and CABIN air f lows until a cabin rate of climb achieved and cabin differential reduces.

WHEN RATE OF CLIMB ACHIEVED

CONFIRM

.. REDUCE

FLOW SELECTORS ADJUST TO CONTROL CABIN

Slowly operate FLIGHT DECK and CABIN f low selectors to maintain cabin altitude required with differential of 5.2 psi or less.

IF FLOW CONTROLS WILL NOT REDUCE CABIN PRESSURE

Rotate MANUAL pressure CONTROL valve towards DUMP so as to reduce pressure differential below 6 psi.

IF OVERPRESSURISATION PERSISTS

Set electrical PRESSURE DUMP switch to DUMP. Don oxygen masks and descend below 10,000 ft.

(cent)/ ....

3-3-1 Aug 1/88

-TISH AEROSPACE



EMERGENCY PROCEDURE . .

CABIN DIFFERENTIAL PRESSURE GREATER THAN 6 PSI

-

Cabin Alt

Aircraft Alt.

END//

3-3-2

Aug 1/88

ALTITUD E (ft) 1000

o 2000 3000 4000 5000 6000 7000 8000 9000

10000 11000 12000 13000 14000 15000 16000 17000 18000 19000 20000 21000 22000 23000 24000 25000

PRESSURE (psi) 15.23 14.69 13.66

r 13.17 12.69 12.22 11.77 11.33 DIFF PRESS 10.91 4.68 psi 10.50 l 10.10 9.72 9.34 8.98

8.63 . 8.29 7.96 Exa.mple 7.64 7.33 cabin 2000 = 13.66 7.04 aircraft 13000 = 8.98 6.75 dif f erential= 4.68 6.47 6.20 5.94 5.69 5.45

psi J2Si psi

-o o o ........,

' o

e

N

BRITISH AEROSFYCE



EMERGENCY PROCEDURE

C.A.P. lcABINI CAPTION ON

INDICATIONS AND CONTROLS .... CONFIRM

Confirm that Cabin Altitude is greater than 10,000 ft Conf irm CABIN ALT control is correctly set Conf irm both FLOW selectors are turned fully clockwise

OXYGEN MASKS . . .

Remove headset and don oxygen masks, confirm oxygen flow

ON

CREW COMMUNICATIONS ESTABLISH

Set MIC C/O switch to MASK and replace headset with boom mike stowed. Establish communication between crew with masks on.

CABIN SIGNS ON

PASSENGER OXYGEN CONFIRM

Conf irm passenger oxygen masks deployed and luminescent star indicates pressure in system. If the masks have not deployed rotate the passenger oxygen control to OVERRIDE. Observe luminescent star indicates pressure in system.

PRESSURE SWITCH NORMAL

Verify PRESSURE switch selected to NORMAL.

MANUAL CONTROL

Verify pressurisation MANUAL CONTROL rotated fully clockwise in the direction of PRESS

IF CABIN ALTITUDE CANNOT BE CONTROLLED

APPLY PROCEDURE: EMERGENCY DESCENT

END//

PRE SS

3-3-3

Feb 15/90

POWER LEVERS

-TJSH A.nl\IMI llCl9'



EMERGENCY PROCEDURE

EMERGENCY DESCENT

FLIGHT IDLE

Retard POWER levers to FLIGHT IDLE and warn cabin crew/ passengers an emergency descent is being initiated.

RPM LEVERS . . . . FULLY ADVANCED

ATC TRANSPONDER A7700

Set emergency code A7700 on transponder to advise ATC of action.

SAFETY ALTITUDE . . . CHECK

DESCENT SPEED . . . . . . . VMO

Descend at VMO to obtain best rate of descent.

OXYGEN (IF REQUIRED) . . . . DON CREW COMMUNICATIONS . ESTABLISH

Establish safety altitude for sector being flown.

CABIN SIGNS . . . . . . ON

IF OXYGEN HAS BEEN USED

WHEN CABIN AT SAFE ALTITUDE

CREW OXYGEN . . AS REQUIRED Set crew oxygen control to position required.

PAX OXYGEN AS REQUIRED Passengers oxygen should return to low delivery pressure automatically but if OVERRIDE has been selected rotate passenger oxygen control to FIRST AID POSITION.

END//

3-3-4

May 15/91

~ 5' K 5'

i e:

~

e:

BRIT/SH AEROSPACE



CHAPTER 4. EMERGENCY EQUIPMENT AND OXYGEN

LIST OF CONTENTS


LIMITATIONS AND ESSENTIAL DATA . . . . . . . . . . . . . . 4-1-1


Crew Oxygen . . .

Ventilated Smoke goggles .

Dispatch with partial oxygen contents .

4-2-1

4-2-2

4-2-3/4

ABNORMAL PROCEDURE

C.A.P.1 EMER LTS caption on . . . . . . . . . . . . 4-3-1

EMERGENCY PROCEDURE

Aircraft Evacuation

Ditching

4-4-1

4-4-4

CHAP.4 CONTENTS

Page 1/2

Jul 15/89

:, ::i

"' -5 e:

-o !'.l .!: it

co 00 00 L.() o o

N

LIST OF CONTENTS EFFECTIVE PAGES 4-1

4-2

4-3 4-4

BR'l77SH AEROSFMCE


MANUFACTURERS OPERATING MANUAL PART 1 CHAPTER 4

EMERGENCY EOUIPMENT ANO OXYGEN


1/2 Jul 15/89 1/2 Jan 15/97 1 Jan 15/97 2 Jan 15/97 1 Sep 15/88 2 Sep 15/88 3 Jan 15/97 4 Jan 15/97 5/6 May 15/91 1/2 Aug 1/88 1 Aug 1/88 2 May 1/88 3 Aug 1/88 4 Aug 1/88 5 Aug 1/88 6 Aug 1/88


Page 1/2

Jan 15/97

"\ , ' '-, r~

~ r-oo L.[) o o -N

BRITISH AEROS#WCE



CHAPTER 4

EMERGENCY EQUIPMENT AND OXYGEN

l. LIMITATIONS

None applicable.

2. ESSENTIAL DATA

2.1 STANDARD EMERGENCY EQUIPMENT CARRIED Fixed oxygen installation . . . . . . Crew plus

passengers as required

Crew portable oxygen bottles . . . . . Mounted in crew seat plinths

Crew oxygen masks

Crew smoke goggles

Ahead and outboard of crew members

Ahead and outboard of crew members

Emergency lights . . . . . . Automatic or manual operation

Flight deck hand f ire extinguisher Outboard of crew

Cabin hand f ire extinguisher

First aid kit

Cabin emergency exits

. . . . . Stowage RH rear of cabin

Stowage RH rear of cabin

Overwings and main Door

Flight deck emergency exit .... Flight deck O.V. window

2.2 OPTIONAL EMERGENCY EQUIPMENT CARRIED As specified by operator.

4-1-1

Jan_15/97

-TISH AEROSl'WCE



2.3 FIXED OXYGEN SYSTEM

Supply indicator BLACK indicates no pressure in system.

Supply indicator showing PARTIAL STAR, indicates therapeutic pressure of 27.6 psi in system.

supply indicator showing FULL STAR, indicates mask deployment pressure of 72.5 psi.

Note: Passenger masks will be automatically deployed at a cabin altitude of 11,500 feet if the mode selector is at NORMAL or FIRST AID. Oxygen will not flow to the individual passenger until the mask is pulled down withdrawing the operating pin.

2.4 OXYGEN DURATION

The oxygen system when fully charged will provide not less than :-

2.4.1 A two hour supply for each pilot

ANO

2.4.2 A thirty minute supply f or eac~ passenger

Note: The two pilots must both be connected to their individual portable oxygen bottles.

These durations assume cabin decompression above 14,000 ft followed by an emergency descent and flight continuing at or below 14,000 ft.

2.5 VENTILATED SMOKE GOGGLES

4-1-2

The portable oxygen bottles, when fully charged, will provide not less 15 minutes supply to each pilot using his oxygen mask with ventilated smoke goggles.

Before the portable oxygen bottles are completely discharged each pilot in turn should transfer his supply connection from his portable bottle to the aircraft main supply. This will ensure a continued supply.

Jan 15/97

o o lJl (X) '-....1 lJl

,,

'(

-llRIT1SN AERO~E




CREW OXYGEN

Wh~n crew oxygen is required, one pilot should control the aircraf t whilst the other dons his oxygen mask and establishes communication. The process is then reversed.

HEADSET . . . REMO VE

TO USE OXYGEN MASKS:-

l. Press the red toggles together to release the mask from its housing.

2. Keep the toggles pressed to inflate the straps.

3. Place the straps over the head with mask covering nose and mouth.

4.. Release red toggles. Straps will grip head.

5. Check oxygen puffing.

HEADSET REPLACE ON HEAD WITH BOOM MIKE STOWED

MIC C/O SWITCH

Set the BOOM-MASK control switch on the side console to MASK.

MASK

e:> Notes: l. The N-100% SWITCH on the mask will provide diluted or C:> 100% oxygen as indicated. N

END//

2. The EMERGENCY rotary control on the mask by-passes the regulator and supplies 100% oxygen at a small positive pressure. Pressing this control acts as a test function and allows a flow of oxygen to the mask.

4-2-1

Sep 15/88

-TISN AEROS-CE JETSTREA.1111 SERiEs J200



VENTILATED SMOKE GOGGLES

When it is necessary to fit the ventilated smoke goggles, one pilot should control the aircraft whilst the other one dons his oxygen mask and goggles. Once communication has been established the role of the two pilots should be reversed so that the second pilot can fit his mask and goggles.

HEADSET . . .

TO USE VENTILATED SMOKE GOGGLES WITH OXYGEN MASK :-

l. Press the red toggles to release the oxygen mask from its housing

2. Keep the toggles pressed to inflate the straps

3. Place the straps over the head with the mask covering nose and mouth

4. Release red toggles. Straps will grip head

5. Set N - 100% switch to 100%

6. Turn the EMERGENCY rotary control to EMERGENCY. Check that oxygen is flowing

7. Fit smoke goggles over the eyes and overlapping the nose of the oxygen mask. Adjust strap around back of head

8. Push the slide valve down on the nose of the mask. This opens an orif ice allowing a steady stream of oxygen into the goggles

HEADSET REPLACE ON HEAD WITH BOOM MIKE STOWED

MIC C/O SWITCH . . . . . ~ . . . . .

...

Set the BOOM - MASK control switch on the side console to MASK

END//

4-2-2

Sep 15/88

. .MASK

-o o -

'-..[) r-oo l..) o o -N

BRITISH AEROSFMCE




DISPATCH WITH PARTIAL OXYGEN CONTENTS

THESE PROCEDURES ENABLE THE AIRCRAFT TO BE DISPATCHED WITH PARTIAL OXYGEN CONTENTS PROVIDED THAT THE NUMBER OF PASSENGERS IS RESTRICTED IN ACCORDANCE WITH THE FOLLOWING TABLES.

Note: The two pilots must be connected to their individual portable oxygen bottles which must indicate FULL.

Table 1

PORTABLE OXYGEN BOTTLE FULL INDICATION

INDICATED PRESSURE 1710 1730 1750 1780 1810 PSI

BOTTLE TEMPERATURE -30 -20 -10 o +10 C

1850

>+20

FOR FLIGHT BETWEEN 14,000 ANO 25,000 FEET, THE MINIMUM PERMITTED INDICATED PRESSURES ARE INDICATED BELOW.

Table 2

AMBIENT TEMPERATURE C PAX -20 -10 o 10 20 30 40

19 1560 1600 1650 1690 1740 1800 1850 17 1420 1560 1500 1540 1590 1640 1690 15 1270 1310 1340 1380 1420 1460 1510 13 1120 1150 1180 1220 1250 1290 1330 11 990 1020 1050 1080 1110 1150 1190

9 840 870 890 920 940 970 1000 7 710 730 750 770 800 820 850 5 570 580 600 620 630 650 670

Note: For OXYGEN TEMPERATURE use ground level ambient temperature except when the aircraft has been subject to cold soak (eg after a long, high-altitude flight followed by a short turnround) the minimum permitted indicated oxygen pressure is obtained by taking the reading for the temperature lOC below ambient.

( cont) / ....

4-2-3

Jan-15/97

BRITISH AEROS#WCE

JETSTREAllll SERiEs J200



DISPATCH WITH PARTIAL OXYGEN CONTENTS (cont) FOR FLIGHT BETWEEN 10,000 AND 14,000 FEET THE MINIMUM PRESSURES ARE INDICATED BELOW:

Table 3

49 CUBIC FOOT OXYGEN BOTTLE DURATION IN MINUTES

OXYGEN GAUGE UP TO 10 11 OR MORE PRESSURE PASSENGERS PASSENGERS

(At 21C or above) 223 or less 30 30 400 95 60 460 -120- 75 600 135 100 700 145 -120-800 155

... 130

1000 175 145 1200 195 160 1400 220 180 1600 240 195 1850 265 215

Note: The above durations include the consumption of two flight crew when flight time between 10,000 and 14,000 ft AMSL exceeds two hours.

If the f light time in the above altitude range is less than two hours, the flight crew are supplied solely from their portable oxygen cylinders.

cont) / ....

4-2-4

Jan 15/97

'~ :~ ~-~;~ f

N

o o U1 00 -.......i -.......i

.:

...

o n 1} "") o o

,-'-.j

B#NTISH AER05'WCE

JETSTREANI SERiEs l200



DISPATCH WITH PARTIAL OXYGEN CONTENTS (cent)

3. For temperatures below +2lC the following conversion table should be used. For higher temperatures, use the figure for +2lC.

Table 4

BOTTLE TEMPERATURE C

+21 -30 -20 -10 o +10

223 195 197 201 206 215 400 340 348 360 373 385 460 390 402 412 426 440

EQUIVALENT 600 515 530 545 560 580 PRESSURE 700 600 620 640 660 680 AT + 2lC 800 692 710 730 750 775 (PSI) 1000 870 890 910 945 970

1200 1040 1070 1100 1133 1166 1400 1220 1250 1285 1320 1360 1600 1385 1430 1460 1510 1555 1850 1710 1730 1750 1780 1810

INDICATED BOTTLE PRESSURE (PSI)

END//

4-2-5/6

May 15/91

-N

llRITISH AEROIYWCE



ABNORMAL PROCEDURE

C.A.P.

EMERGENCY LIGHTING SWITCH

REAR DOOR LIGHT SWITCH

IF C.A.P. REMAINS ON:

ON GROUND

TAKE-OFF IS PROHIBITED.

IN FLIGHT

NO FURTHER ACTION. LO.G DEFECT.

END//

EMER LTS CAPTION ON

CHECK ARMED

CHECK OFF

4-3-1/2 Aug 1/88

'

~ Al!IRDSPACE

JETSTREAAI SeRies J200


EMERGENCY PROCEDURE

AIRCRAFT EVACUATION

WARNING: IF THERE IS A FIRE OR SIGNS THAT FIRE MAY ERUPT, ONLY THE DOORS AND ESCAPE HATCHES AWAY FROM THE FIRE SHOULD BE USED.

BASIC PROCEDURE

The crew should supervise the rapid evacuation of all on board. Evacuate away from fire and ensure that everyone is kept suff iciently far from the wings to minimise injury should the fuel tanks explode. 'No smoking' should be stressed.

Crew and able-bodied persons should assist in the evacuation of children, disabled, aged and infirm passengers.

The f irst essential is for passengers followed by crew to evacuate the aircraft in the shortest possible time. This process should not be impeded by people collecting coats, briefcases, fire extinguishers or first aid kits. These items can be collected by the crew later when it is safe to do so.

' Ensure that all passengers and crew are out of the aircraft. f'.., o O EMERGENCY EXITS o -N All escape hatches and the door should be used to evacuate the passengers. The location and operation of the over-wing

escape hatches is shown in the accompanying diagram. The main door cannot be jettisoned. The D.V. windows provide additional escape routes for the pilot and co-pilot. Operation is shown in the accompanying diagram.

4-4-1 Aug 1/88

PULL OOWN ANO INWAROS

4-4-2

May 1/88

-TISH AEROSPACE

JETSTREANI SERiES }200


0

PASS OOOR THROUGH EXIT TO CLEAR PASSAGEWAY

ESCAPE ROUTES

ESCAPE HATCH Fig. 1

\ V/ , LOWE R THE OOOR OUTWAR OS~ __ lj\ EVACUATE THE AIRCRAFT ' < ~

,/i,\\.~i, l .

,.

t.

N -

o o ro o o o -N

8'NTISH AEROSPACE

JETSTREA~ SERiES 'J200


TO OPEN DV. WINDOW 1.PULL STRIPED HANDLE DOWN ANO REARWARDS 2.PULL WINDOW INWARD USING BOTH HANDLES 3.MOVE WINDOW REARWARDS IN TRACK UNTIL

CATCH ENGAGES

i CAUTION;DO NOT PULL ON

DESICCATOR

l~~~~l\

FOR LEFT PILOT

D V WINDOW ESCAPE ROUTE Fig. 2

4-4-3 Aug 1/88

BRITISH AEROSPACE



EMERGENCY PROCEDURE

DITCHING

ATC TRANSPONDER . A7700

Set emergency code A7700 on transponder to advise ATC of action.

DISTRESS MESSAGE . TRANSMIT

Transmit MAYDAY and advise position, disposition of crew and passengers, intentions on landing, description of any dangerous cargo and quantity of fuel.

ELT . . . . ON

CABIN CREW/PASSENGERS

Instruct cabin.crew and passengers to prepare for ditching and evacuation. Crew and passengers to don life jackets, uninflated at earliest ppportunity.

BRIEF

EXCESS FUEL . . . . .. BURN-OFF

Burn off excess fuel that is not required to make a saf e touchdown.

AIRFLOWS . . . e . OFF

LANDING GEAR . . . . . . . . .

Do not extend landing gear for ditching.

GEAR WARN C/B (WHITE COLLAR) . Trip GEAR WARN C/B on DC Essential Busbar Panel to prevent warning by gear horn with gear up on landing, circuit breaker.

(cont)/ ....

4-4-4

Aug 1/88

LEAVE UP

TRIP

trip

N

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(\J a co a a o -('\J

l!IRl77SH AEROSPACE

JETSTREAA# SERiES l200


EMERGENCY PROCEDURE

DITCHING (cent)

RIGHT STALL PROTECTION SWITCH . . . . OFF

Set RIGHT STALL PROTECTION SWITCH to OFF to prevent stick-pusher action during approach and touch down.

FLAPS . . 35 o

Set Flaps to 35.

APPROACH CHECKLIST

DITCHING BRIEFING . UPDATE

The captain will brief on his intentions and requirements for approach, ditching and after ditching.

PASTEN SEAT BELTS SIGNS . ON

Set PASTEN SEAT BELTS sign to ON.

EMERGENCY LIGHTS . . ARM

Verify EMERGENCY LIGHTS selector to ARM.

ALTIMETERS SET/CHECK

Set altimeter for landing and compare.

LANDING CHECK

GEAR . . . . . .

Confirm gear still UP for ditching.

FLAPS . . .

Confirm flaps set at 35.

(cont)/ ....

. . . . . . UP

. . . . . . . . . . . . 3 5 o

4-4-5 Aug 1/88

B#WTISH AEROSPACE

JETSTREANI SeRies }200


EMERGENCY PROCEDURE

DITCHING (cont)

AT 1000 FEET CALL ON PA "TAKE UP DITCHING POSITIONS"

AT 200 FEET CALL ON PA . . . . . "BRACE BRACE"

AT 100 FEET REDUCE RATE OF DESCENT TO MINIMUM.

MAINTAIN AIRSPEED Vref (VAT). TOUCHDOWN IN A FLAT ATTITUDE.

ON TOUCHDOWN

FEATHER LEVERS . . . . . . . . . ; PULL

WHEN AIRCRAFT AT REST

PASSENGERS EVACUATION . . . . . . . . . . . . . INITIATE

CAUTION: THE MAIN DOOR SHOULD NOT BE USED AS THE SILL WILL BE BELOW THE SURFACE OF THE WATER.

The captain will direct cabin crew and passengers to start evacuation, using the over wing emergency exists.

A passenger seat cushion should be carried out by each passenger to use as a flotation aid. The cushion should be held to the chest with the straps over the arms before entering the water.

END//

4-4-6

Aug 1/88

,

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N -o o o co o (...

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. 5 j

BIWT7SHA~E JETSTREAA# SERiES J200


CHAPTER 5. ELECTRICS

LIST OF CONTENTS


LIMITATIONS AND ESSENTIAL DATA . .

CIRCUIT BREAKER AND FUSE LOCATIONS

5-1-1

5-2-1

e: ;::: ~ ABNORMAL PROCEDURES

"1"' o 00 o o o -N

C.A.P.

C.A.P.

C.A.P.

GEN caption on . .

BUS TIE OPEN caption on

AC ESS caption on . . .

. 5-3-1

. 5-3-4

5-3-5

C.A.P. AC MAIN caption on . . . . . 5-3-6

C.A.P.

C.A.P. BAT

C.A.P. SERIES

caption on

caption on

caption on

5-3-7

5-3-8

5-3-9


C.A.P. BUS FAIL

C.A.P. INV red

Battery 150 light

caption on . . . . . . . . 5~4-1

caption on . . . . . . . . . . . 5-4-5

on (NiCad batteries only) . . . . 5-4-6

CHAPTER 5. CONTENTS

Page 1/2

Aug 1/88

e . ~!-. ;-.;

" ,,

LIST OF CONTENTS LIST OF EFFECTIVE PAGES 5-1

::..:: ::::i ' 5-2 -5 .: " s .: e':

5-2 GRE 5-2

5-3

r-'.".l ...n V') o o 5-4 N

BRIT/SH AEROSPACE

JETSTREANI SERES 7200


LIST

1/2 Aug

1/2 Feb 1 Nov 2 Nov 1 Apr 2 May 3 Nov 4 May 5 May 6 May 7 May 8 May 9 May 10 May 11 May 12 May 13 May 14 May 15 May 16 May 17 May 18 Aug 19 Apr 19 Sep 20 Apr 1 Aug 2 Apr 3 Apr 4 Aug 5 Aug 6 Aug 7 Feb 8 Aug 9/10 Aug 1 Aug 2 Aug 3 Sep 4 Apr 5

AOM JS32

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