LUFTFAHRT-BUNDESAMT GERATEKENNBLATT · PDF fileLUFTFAHRT-BUNDESAMT GERATEKENNBLATT (§ 4...

L U F T F A H R T - B U N D E S A M T

G E R A T E K E N N B L A T T

(§ 4 LuftVZO)

T I T E L B L A T T

Flugzeug - Kennblatt Nr.: 2823

Muster: BOEING 737

Baureihe: BOEINGBOEINGBOEINGBOEINGBOEINGBOEINGBOEINGBOEINGBOEING

737-100737-200737-300737-400737-500737-600737-700737-800737-900

Flugzeug - Kennblatt Mr: 2823

Muster: BOEING 737

Ausgabe DatumNr.

Baureihe:

Verkaufsbezeichnunq:

Baureihe:


Baureihe:


Baureihe:


Baureihe:


Baureihen:

BOEING 737-100

BOEING 737-130

BOEING 737-200

BOEING 737-230BOEING 737-230CBOEING 737-2K5

BOEING 737-300

10 15.12.1992

BOEINGBOEINGBOEINGBOEINGBOEINGBOEINGBOEINGBOEINGBOEING

737-31S737-330737-35B737-360737-375737-3K9737-3L9737-3M8737-3S3

BOEING 737-400

BOEING 737-430BOEING 737-46BBOEING 737-46JBOEING 737-4K5BOEING 737-4YO

BOEING 737-500

BOEING 737-505BOEING 737-530BOEING 737-5K5

BOEING 737-600BOEING 737-700BOEING 737-800BOEING 737-900

101010

5112311822

11586

262

7777

15.12.199215.12.199215.12.1992

08.09.199804.01.199515.05.199125.08.199919.12.199630.09.199429.11.199625.09.199611.04.1995

03.06.199205.04.200118.04.199729.03.199501.05.1996

03.12.199010.03.199501.12.1990

14.05.200114.05.200114.05.200114.05.2001

Boeing 737 JAA Data SheetJAA/25/97-018

JointAviationAuthorities

JAA DATA SHEET

Boeing 737 Series

Manufacturer:

Boeing Commercial Airplane GroupP.O. Box 3707SeattleWA 98124-2207United States of America

JAA/25/97-018

For Model B737-700For Model B737-800For Model B737-600For Model B737-900

Issue 7 introduces data applicable for the Boeing 737-900.

List of effective Pages:

PageIssue

17

27

36

47

56

66

76

86

96

106

117

126

136

146

157

Page6

166

176

186

197

207

217

227

237

247

257

267

Page 1Issue 7

17th March 2001


CONTENT

Section A. Data Applicable to all models

I. GeneralII. Certification BasisIII. Technical characteristics and operational LimitationsIV. Operating and service Instructions

Section B. B737-700 Series


Section C. B737-800 Series


Section D. B737-600 Series


Section E. B737-900 Series


Page 2Issue 7

17th March 2001


SECTION A: Data Applicable To All Models

(A)I. GENERAL

1. Airworthiness Category:

2. Authority: (Address)

3.

Large Transport Airplane, JAR 25

Federal Aviation Authority (USA)Seattle Aircraft Certification Office,1601 Lind Avenue SW,Renton WA-98055-4056United States of America

Manufacturer (Type Certification Holder): Boeing Commercial Airplane Group(Address): P.O. Box 3707

SeattleWA 98124-2207United States of America

(A)II. CERTIFICATION BASIS

See Individual aircraft model Certification Bases

(A)III. TECHNICAL CHARACTERISTICS AND OPERATIONAL LIMITATIONS

1. Production Basis: Production under Type Certificate

2.

3.

Description: Low wing jet transport with a conventional tail unitconfiguration, powered by two high bypass turbo fan enginesmounted on pylons beneath the wings.

Auxiliary Power Unit (APU): Allied Signal AS 131-9 [B]

3.1 APU Limits:

MAXRPM

53875

MAX EGT Start

1375 °F

MAX EGT Steady State(Limited to 5 minutes)

1275 °F

MAX EGTRunning(normal)

1275 °F

4. Propellers: N/A

Page 3Issue 6

5th September 2000


Fuel:

5.1 Eligible Fuels: ASTM Specification D-165 5 Jet A, JAR A1MIL-T-5624G; JP-5MIL-T-83133;JP-8Refer to Airplane Flight Manual for other approved fuels.

5.2 Fuel Capacity: 26024 litres (6875 US Gall), consisting of two wing tanks,each of 4875 litres (1288 US Gall) capacity, and one centre tank, capacity16274 litres (4299 US Gall).

6. Oil:

6.1 Eligible Oils: See CFM 56-7B Service Bulletin 79-001 as revised.6.2 Oil Capacity: 10.3 litres useable

7. Minimum Flight Crew: Two (Pilot and Co-pilot) for all types of flight

8. Required Equipment: See individual aircraft models

(A)IV OPERATING AND SERVICE INSTRUCTIONS

1. Operation Information: (See individual models)

2. Service Information: (See individual models)

Page 4Issue 7

17th March 2001


SECTION B: BOEING B737-700

(B)I. GENERAL

1. Performance Category: A

2. JAA Validation Application Date: 4th August 1993

3. JAA Validation Date (JAA recommendation): 18th February 1998

(B)II. CERTIFICATION BASIS

1. Reference Application Date for FAA Certification: 4th February 1993

2. Certification Date: Boeing B737-700 7th November 1997

Type Certificate Data Sheet No. A16WE

3. Certification Basis: FAR 25 Amendment 25-77 except where modified by FAAIssue paper G-l.

4. JAA Certification Basis:

4.1 Applicable JAR Requirements at the Reference Date:

JAR 25 Change 13, effective 5 October 1989Orange Paper 90/1, effective 11 May 1990Orange Paper 91/1, effective 12 April 1991JAR AWO Change 1, effective 29 November 1985Orange Paper AWO/91/1, effective 28 November 1991(Note also see AWO Change 2)

JAA IL-23 RVSM, effect. April 1994 (Boeing letter B-T111-96-1357 dated 12December 1996).

The following NPAs have been applied:

NPA 25 B, D, G-244 Accelerate Stop Distances and Related PerformancesNPA 25C-213 Discrete source damage due to rotor burstNPA 25B215 Stall and Stall Warning Speeds and Manoeuvre CapabilityNPA25B-217 Reduced ThrustNPA AWO 2 All Weather OperationsNPA AWO 5 All Weather OperationsNPA 25B, C, D-236 Flutter, Deformation and Fail Safe CriteriaNPA 25J-246 APU InstrumentsNPA 25C-260 Design Dive Speed (JAR 25.335(b)(2) plus ACJ at Ch. 14)NPA 25C-260 Nose Wheel Steering (JAR 25.499(e))NPA 25B-261 Harmonisation of JAR/FAR 25 Flight Requirements

Page 5Issue 7

17th March 2001


In addition, the following requirements have been applied:

• JAR AWO Change 2: All Weather Operations• Special Condition JAA/737-700/SC/C-07: (JAR 25.427(b)(3)FAA/JAA

Harmonised version) in place of JAR 25.427(b)(3)• Static Ground Load Conditions (Jacking): JAR 25.X519(b) in accordance with

JAR 25 Amendment 25/96/1• Stalling Speeds for Structural Design (defined in CRI C-12)• Type III Emergency Exit Operating Handle Illumination JAR 25.81 l(e) at JAR

25 Change 14

4.2 Reversions:

The following reversions from the defined certification basis have been applied:-

CRI A. 11 -02 Pressurised Cabin LoadsJAR 25.365 Reversion to FAR 25.365 Amendment 0.

CRI A. 11 -04 Emergency Landing Dynamic LoadsJAR 25.562 Reversion to JAR 25 Change 12 which excludes paragraph .562

CRI A. 11-05 Fatigue and Damage ToleranceJAR 25.571 Partial Reversion to FAR 25.571 Amendment 0

CRI A. 11-06 FastenersJAR 25.607(a) Reversion to FAR 25.607(a) Amendment 0

CRI A. 11 -08 Lift and Drag Device IndicatorJAR 25.699(a) Reversion to FAR 25.699 Amendment 0

CRI A. 11-11 DoorsJAR 25.783(f) Reversion to FAR 25.783 Amendment 15

CRI A. 11 -12 Seat, Berths, Safety Belts and HarnessJAR 25.785(a) Reversion to JAR 25.785(a) Change 12

CRI A. 11-16 Equipment, systems and InstallationsJAR 25.1309 Reversion to FAR 25.1309 Amendment 0

CRI A. 11 -23 Windshields and WindowsJAR 25.775(d) Reversion to FAR 25.775(d) Amendment 0

CRI J-04 APU Fuel Shut Off Valve IndicationJAR 25Al 141(f)(2) Reversion to FAR 25.1141 Amendment 11

Page 6Issue 7

17th March 2001


4.3 JAA Special Conditions:

The following special conditions have been applied defined in their respective CRL-

JAA/737-700/SC/B-10CRI B-10 Stall Warning Thrust Bias

Affected Requirement JAR 25.207(c) as amended by NPA 25B-215

JAA/737-700/SC/C-01CRI C-01 Pressurised Cabin Loads

INT/POL/25/7 Affected requirement JAR 25.365

JAA/737-700/SC/C-11CRI C-11 Interaction of Systems and Structure

Affected requirement JAR 25.302 & 25.310(b)

JAA/737-700/SC/D-01CRI D-01 Brakes Requirements Qualification and Testing


JAA/737-700/SC/D-04CRI D-04 Landing Gear Warning

INT/POL/25/1: Affected requirement JAR 25.729(e)(2) to (4)

JAA/737-700/SC/D-14CRI D-14 Exit Configuration

Affected Requirement: JAR25.807

JAA/737-700/SC/F-01CRI F-01 High Intensity Radiated Field (HIRF)

INT/POL/25/2:Affected requirement JAR 25.1431(a)

JAA/737-700/SC/F-02CRI F-02 Protection from Effects of Lightning Strike; Direct Effects

INT/POL/25/3: Affected requirement JAR 25X899 and ACJ 25X899

JAA/737-700/SC/F-03CRI F-03 Protection from Effects of Lightning Strike; Indirect Effects

INT/POL/25/4: Affected requirement JAR 25.581, 25.899, 25.954,25.1309

4.4 JAA Exemptions:

The following Partial Exemption has been applied:

JAA/737-700/PE/D-02CRI D-02 Hydraulic System Proof Pressure Testing

Partial Exemption Against JAR 25 1435(b)(l)

Page 7Issue 7

17th March 2001


4.5 JAA Equivalent Safety Findings:

JAA/737-700/ES/D-06CRI D-06 Towbarless Towing

Equivalent Safety with JAR25X745(d)

JAA/737-700/ES/D-08CRI D-08 Forward and Aft Door Escape Slide Low Sill Height

Equivalent Safety with JAR 25.809(f)(l)(ii)

JAA/737-700/ES/D-10CRI D-10 Overwing Hatch Emergency Exit Signs

Equivalent Safety with JAR 25.812(b)(l)(i)

JAA/737-700/ES/D-16CRI D-16 Automatic Overwing Exit

Equivalent Safety with JAR 25.783(f)

JAA/737-700/ES/D-17CRI D-17 Oversized Type I Exits, Maximum Number of Passengers

JAA/737-700/ES/D-18CRI D-18 Slide/Raft Inflation Gas Cylinders

Equivalent Safety with JAR 25X1436

JAA/737-700/ES/E-09CRI E-09 Automatic Fuel Shut Off

Equivalent Safety with JAR 25.979(b)(l)

JAA/737-700/ES/F-15CRI F-15 Wing tip Position Lights

Equivalent Safety with JAR 25.1389(b)(3)

4.6 JAA Environmental Standards:

Noise: ICAO Annex 16 Volume I (Third Edition)Fuel Venting & Emissions: ICAO Annex 16 Volume II (Second Edition).

5. Additional National Design Requirements:

Additional National Design Requirements for the Type Certification are defined in CRIA-02.

PageSIssue 7

17th March 2001


(B)IH. TECHNICAL CHARACTERISTICS AND OPERATIONAL LIMITATIONS

Design Standard:

(737-700 IGW)

Dimensions:

Denned by Boeing Top Drawing No. 001AOOO1-700 Rev. AG,dated January 12, 1998, and later approved changes andProduction Revision Record (PRR) No. 38280.

Boeing Top Drawing No. 001AOOO1-2703 Rev. CA, datedOctober 13, 1998, and later approved changes and ProductionRevision Record (PRR) No. 38280

SpanLengthHeightWing Area

34.32 m32.18m12.57m124.65 m2

112 ft 7 ins105 ft 7 ins41 ft 3 ins

1341 ft2

3. Engines: Two CFM 56-7B Turbofan Engines(DGAC Type Certificates M21 and M IM 45 refer)

OperatingConditions

Take OffMaximum Continuous

SLS Thrust (LB)CFM 56-

7B207B20/2 (1)

20,60019,400

7B22

22,70022,300

7B247B24/2 (1)

24,20022,800

7B26 (2)

7B26/B1 (4)

26,30025,900

7B27/B3 (3)

3.1

(1) Reference Boeing PLOD; B-H340-00-0380 (Revision C)(2) Reference Boeing PLOD; B-T111-98-2097 (Revision F: 737-700 IGW only)(3> Reference Boeing PLOD; B-H340-99-7649 (Revision B: 737-700 IGW only)(4) Reference FAA Letter 98-140S-421, Nov 19, 1998 (737-700 IGW only)

Engine Limits: For other limitations, see DGAC France Engine Type CertificateData Sheet M21or M IM 45 as applicable).

Operating Conditions

Take OffMaximum ContinuousGroundStarting

Rotor Speed (%)Nl104104N/AN/A

Rotor Speed (%)N2105105N/AN/A

TemperatureLimits (°C) EGT

950°C (5 minutes)925°C (no limit)

N/A725°C (no limit)

4. Air Speeds: Refer to Approved Airplane Flight Manual (See Section IV)

5. Maximum Operating Altitude: 12,497 m (41,000 ft) pressure altitude

Page 9

17Issue 7

th March 2001

8.

9.

10.

11.

12.

13.


6. All-weather Capability:

7. Maximum Weights:

Cat 3 (with 50 ft. decision height)

PhaseTaxi and RampTake-offLandingZero Fuel

737-700*1 55,000 Ibs.154,500 Ibs.129,200 Ibs.121,700 Ibs.

70,295 kg,70,068 kg.58,594 kg.55,193kg.

737-700 IGW**17 1,500 Ibs.17 1,000 Ibs.134,000 Ibs.126,000 Ibs.

77,791 kg.77,564 kg.60,781 kg.57,153kg.

* Specified weights for -700 are Increased Design Weights approved post-initialType Validation

** Reference Boeing PLOD reference B-Tl 11-98-209 (737-700 IGW Revision F)

Centre of Gravity Range: Refer to Approved Flight Manual

Datum: Weight & Balance Manual

Mean Aerodynamic Cord (MAC): 3.96m(155.81in)

Levelling Means: Weight & Balance Manual

Maximum Passenger Seating Capacity: 149 (with JAA/737-700/SC/D-14 applicable)or otherwise: 145

Note: A JAA Approved Interior is required.

Exits: Boeing B737-700:

1 MainFwdLH2 Main Aft LH3 Service (Fwd, RH, Aft, RH)4 Overwing/Emergency left5 Overwing/Emergency right

Number11

1+111

TypeType IType IType IType IIIType III

Size mm (inches)864Wxl829H (34x72),762Wxl829H (30x72),762Wxl651H (30 x 65 - both)508Wx914H (20x36)508Wx914H (20x36)

Additionally, for crew emergency evacuation purposes, the following exits areavailable on both sides:

Cockpit side window (2) Flight Crew Emergency Exit 483x508 (19x20)

Page 10Issue 7

17th March 2001


14. Baggage/Cargo Compartments:

15.

16.

17.

LocationFront FwdMiddleRear AftUnderfloor

ClassDN/ADN/A

Volume m3 (ft3)

11.37 (406)N/A16.7 (596)N/A

Wheels and Tyres:

Nose Assy (Qty 2) Tyre: 27 x 7.75 - 15 or 27 x 7.75 - R15Wheel: 27 x 7.75 - 15

Main Assy (Qty 4) Tyre: H43.5 x 16.0 - 21 or H44.5 x 16.5 - 21Wheel: HR44.5 x 16.5 - 21

Speed Rating: 225 MPH

Required Equipment: The approved equipment is listed in: (737-700) CRI A-10

ETOPS Operation

The Type Design of this aircraft has been approved for ETOPS Operation up to 180Minutes diversion time provided the Configuration, Maintenance and Proceduresrequirements of Boeing Document D044A007 Issue C dated 15 September 1999 (orlater issue) are complied with.

(B)IV OPERATING AND SERVICE INSTRUCTIONS

1. Operation Information:

1.1 Airplane Flight Manual, Document No. D631 AGO 1 JO 1

2. Service Information:

2.1 Maintenance Manual, Document No. D633A1012.2 Maintenance Review Board Report Revision 1; 19th November 1997 or

subsequent JAA approved revision2.3 Airworthiness Limitations and Certification Maintenance Requirements:

737-600/700/800 Maintenance Planning Document (MPD) Document Section 9Ref.: D626A001, Revision Dated September 1997, and later revisions thereof

2.4 Service Letters and Service Bulletins

Page 11Issue 7

17th March 2001


SECTION C: BOEING B737-800

(C)I. GENERAL

A1. Performance Category:

2. JAA Validation Application Data: 4th August 1993

3. JAA Validation Dates (JAA recommendation): 9th April 1998

(C)II. CERTIFICATION BASIS


Certification Date: Boeing B737-800 13th March 1998


Certification Basis: As for Boeing 737-700 [See Section (B)II ]

JAA Airworthiness Requirements: As for Boeing 737-700 [See Section (B)II ]

Additional National Design Requirements:


(C)III. TECHNICAL CHARACTERISTICS AND OPERATIONAL LIMITATIONS

2.

3.

4.

5.

Design Standard:

Dimensions:

Defined by Boeing Top Drawing No. 001A0001-800 Rev. AK,dated February 27th, 1998, and later approved changesProduction Revision Record (PRR) No. 38280.


34.32m39.5m12.57m124.65 m2


1341 ft2

Page 12Issue 6

5th September 2000


3. Engines: Two CFM 56-7B Turbo fan Engines(DGAC Type Certificates M21 and M IM 45 refer)



SLS Thrust (LB) CFM56-7B24

24,20022,800

7B267B26/2 (2)

26,30025,900

7B27

27,30025,900

7B27/B1 (1)

27,30025,900

3.1

(1)Reference Boeing PLOD Rev.B reference B-T113-99-3067; March 17, 1999(2)Reference Boeing PLOD Rev.C reference B-T113-99-0380; January 20, 2000

Engine Limits: For other limitations, see DGAC France Engine Type CertificateData Sheet M21 or M IM 45 as applicable).

OperatingConditions


Rotor Speed (%)Ml104104N/AN/A

Rotor Speed (%)N2105105N/AN/A

Temperature Limits (°C)EGT



4.

5.

6.

7.

Air Speeds: Refer to Approved Airplane Flight Manual (See Section IV)

Maximum Operating Altitude: 12,497 m (41,000 ft) pressure altitude

All-weather Capability: Cat 3 (with 50 ft. decision height)

* Maximum Weights:


174,700 Ibs.1 74,200 Ibs.146,300 Ibs.138,300 Ibs.

79,229 kg.79,002 kg.66,349 kg.62,721 kg.

* Specified Weights are Increased Design Weights approved post initial Type Validation.

8. Centre of Gravity Range: See Approved Airplane Flight Manual

9. Datum: Weight & Balance Manual

10. Mean Aerodynamic Cord (MAC): 3.96 m (155.81 in)

11. Levelling Means: Weight & Balance Manual

Page 13Issue 6

5th September 2000


12. Maximum Passenger Seating Capacity: 1 89 (with JAA/737-700/SC/D- 14 applicable)or otherwise: 180


13. Exits: Boeing B737-800:


Number11

1+122



15.

16.


Cockpit side window (2) Flight Crew Emergency Exit 483 x 508 (19 x 20)



ClassDN/ADN/A

Volume m3 (ft3)

19.6 (692)N/A25.46 (899)N/A

Wheels and Tyres:

Nose Assy (Qty 2) Tyre: 27 x 7.75 - 15 or 27 x7.75 - R15Wheel: 27 x 7.75 - 15

Main Assy (Qty 4) Tyre: H43.5 x 16.0 - 21 or H44.5 x 16.5 - 21Wheel: HR.44.5x 16.5-21


Required Equipment: The approved equipment is listed in: (737-700) CRI A-10

Page 14Issue 6

5th September 2000


17. ETOPS Operation


(C)IV OPERATING AND SERVICE INSTRUCTIONS


1.1 Airplane Flight Manual, Document No. D631A001.J02

2. Service Information:

2.1 Maintenance Manual, Document No. D633A1012.2 Maintenance Review Board Report Revision 1; 19th November 1997 or


737-600/700/800 Maintenance Planning Document (MPD) Document Section 9Ref: D626A001, Revision Dated September 1997, and later revisions thereof


Page 15Issue 7

17th March 2001


SECTION D: BOEING B737-600

(D)I. GENERAL

1. Performance Category:

2. JAA Validation Application Data:

3. JAA Validation Dates (JAA recommendation):

A

4th August 1993

9th September 1998

(D)II. CERTIFICATION BASIS


2. Certification Date: Boeing B737-600 12th August 1998


3. Certification Basis: As for Boeing 737-700 [See Section (B)II ]

4. JAA Airworthiness Requirements: As for Boeing 737-700 [See Section (B)II ]

5. Additional National Design Requirements:


(D)III. TECHNICAL CHARACTERISTICS AND OPERATIONAL LIMITATIONS

Design Standard:

Dimensions:

Defined by Boeing Top Drawing No. 001AOOO1-600 Rev. AW,dated June 8th 1998, and later approved changes.Production Revision Record (PRR) No. 38280.


34.32m31.2m12.57m124.65 m2

112 ft 7 ins102 ft 6 in41 ft 3 ins

1341 ft2

Page 16Issue 6

5th September 2000


3. Engines: Two CFM 56-7B Turbo fan Engines(DGAC Type Certificates M21 and M IM 45 refer)



SLS Thrust (LB)CFM56-7B20

CFM56-7B20/220,60019,400

CFM56-7B22CFM56-7B22/2

22,70022,300

3.1 Engine Limits: For other limitations, see DGAC France Engine Type CertificateData Sheet M21 or M IM 45 as applicable).

OperatingConditions


Rotor Speed (%)Nl104104

N/AN/A

Rotor Speed (%)N2105105

N/AN/A




4.

5.

6.

7.

9.

10.

11.

12.

Air Speeds: Refer to Approved Airplane Flight Manual (See Section IV)

Maximum Operating Altitude: 12,497 m (41,000 ft) pressure altitude

All-weather Capability: Cat 3 (with 50 ft. decision height)

Maximum Weights:


144,000 Ibs.143,500 Ibs.120,500 Ibs.113,500 Ibs.

65,317kg.65,090 kg.54,657 kg.51,482kg.

Centre of Gravity Range:

Datum:

See Approved Airplane Flight Manual

Weight & Balance Manual

Mean Aerodynamic Cord (MAC): 3.96 m (155.81 in)




Page 17Issue 6

5th September 2000


13. Exits: Boeing B737-600:


Number11

1+111


Size mm (inches)864Wxl829H (34x72),762Wxl829H (30x72),762Wxl651H (30x65 -both)508Wx914H (20x36)508Wx914H (20x36)

15.

16.

17.


Cockpit side window (2) Flight Crew Emergency Exit 483x508 (19x20)



ClassDN/ADN/A

Volume m3 (ft3)

7.59 (268)N/A13.8 (488)N/A

Wheels and Tyres:

Nose Assy (Qty 2) Tyre: 27 x7.75 - 15 or 27 x 7.75 - R15Wheel: 27 x 7.75 - 15

Main Assy (Qty 4) Tyre: H43.5 x 16.0 - 21 or H44.5 x 16.5 - 21Wheel: HR44.5 x 16.5 -21


Required Equipment: The approved equipment are listed in: (737-700) CRI A-10

ETOPS Operation


Page 18Issue 6

5th September 2000


(D)IV OPERATING AND SERVICE INSTRUCTIONS



2. Service Information:2.1 Maintenance Manual, Document No. D633A1012.2 Maintenance Review Board Report Revision 1; 19th November 1997 or


737-600/700/800 Maintenance Planning Document (MPD) Document Section 9Ref.: D626A001, Revision Dated September 1997, and later revisions thereof


Page 19Issue 7

17th March 2001


SECTION E : BOEING B737-900

(E)I. GENERAL

1. Performance Category:

2. JAA Validation Application Data:

3. JAA Validation Dates (JAA recommendation):

A

14th October 1997

19thApril2001

(E)IL CERTIFICATION BASIS

1. Reference Application Date for FAA Certification: 14th October 1997

Certification Date: Boeing B737-900 17th April 2001


2.

3. Certification Basis: FAR 25 Amendment 25-91 except where modified by FAAIssue paper G-l.

4. JAA Airworthiness requirements (Reference CRI 9/A-01)

JAR 25 Change 14, effective 27 May 1994Orange Paper 96/1, effective 19 April 1996JAR AWO Change 2, effective 1st August 1996JAAIL-23 RVSM, effective April 1994

The following NPAs have been applied:

NPA 25 B, D, G-244NPA25C-213NPA25B215NPA25B-217NPA AWO 2NPA AWO 5NPA 25B, C, D-236NPA 25J-246NPA 25C-260NPA 25C-260NPA 25C-260NPA25B-261NPA 25C-282

Accelerate Stop Distances and Related PerformancesDiscrete source damage due to rotor burstStall and Stall Warning Speeds and Manoeuvre CapabilityReduced ThrustAll Weather OperationsAll Weather OperationsFlutter, Deformation and Fail Safe CriteriaAPU InstrumentsDesign Dive Speed (JAR 25.335(b)(2) plus ACJ at Ch.14)Nose Wheel Steering (JAR 25.499(e))Reference JAR 25.415 and JAR 25.519Harmonisation of JAR/FAR 25 Flight RequirementsHarmonisation of Structures Requirements (see CRI C-05)

Page 20

17Issue 7

th March 2001


In addition, the following requirements have been applied:

• JAR AWO Change 2: All Weather Operations• Special Condition JAA/737-700/SC/C-07: (JAR 25.427(b)(3)FAA/JAA

Harmonised version) in place of JAR 25.427(b)(3)• Static Ground Load Conditions (Jacking): JAR 25.X519(b) in accordance with

JAR 25 Amendment 25/96/1• Stalling Speeds for Structural Design (defined in CR1 C-12)• Type III Emergency Exit Operating Handle Illumination JAR 25.81 l(e) at JAR

25 Change 14• ETOPS Approval (180 Minutes): JAA Information Leaflet Number 20

(1st July 1995 Revised)

The following Reversions from the defined certification Basis have been applied:

CRI A. 11-04 Emergency Landing Dynamic LoadsJAR 25.562 Reversion to JAR 25 Change 12 excluding paragraph .562

Note: Special condition JAA/737-700/SC/D-14 which is applicable to the model -900requires compliance to 25.562 at change 13 (same as change 14) except for25.562(c)(5) and (c)(6).

CRI A. 11-06 FastenersJAR 25.607(a) Reversion to FAR 25.607(a) Amendment 0

CRI A. 11 -08 Lift and Drag Device IndicatorJAR 25.699(a) Reversion to FAR 25.699 Amendment 0

CRI A. 11-11 DoorsJAR 25.783(f) Reversion to FAR 25.783 Amendment 15

CRI A. 11 -12 Seat, Berths, Safety Belts and HarnessJAR 25.785(a) Reversion to JAR 25.785(a) Change 12

CRI A. 11 -16 Equipment, systems and InstallationsJAR 25.1309 Reversion to FAR 25.1309 Amendment 0

CRI A. 11 -23 Windshields and WindowsJAR 25.775(d) Reversion to FAR 25.775(d) Amendment 0

CRI J-04 APU Fuel Shut Off Valve IndicationJAR 25A1141(f)(2) Reversion to FAR 25.1141 Amendment 11

CRI 9/A. 11-01 Pressurised Cabin LoadsJAR 25.365 Reversion to FAR 25.365 Amendment 0

CRI 9/A. 11 -02 Fuel Tank Access Covers

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JAR 25.963(g)(l) Reversion to FAR 25 963 (e)(l) Amendment 69

CRI 9/A11-03 Automatic Pilot SystemJAR 25.1329 Reversion to JAR 25.1329 Change 13 and associated ACJ

CRI 9/A11 -04 Electronic Display SystemsAMJ 25-11 Reversion to JAR 25 Change 13 and associated ACJ

5. JAA Special Conditions

The following Special Conditions have been applied as defined by the respective CRI:

JAA/737-700/SC/B-10CRI B-10 Stall Warning Thrust Bias

Affected Requirement JAR 25.207(c) as amendedbyNPA25B-215

JAA/737-700/SC/C-01CRI C-01 Pressurised Cabin Loads


JAA/737-700/SC/C-11CRI C-l 1 Interaction of Systems and Structure

Affected requirement JAR 25.302

JAA/737-700/SC/D-01CRI D-01 Brakes Requirements Qualification and Testing

INT/POL/25/6: Affected requirement JAR 25.735

JAA/737-700/SC/D-04CRI D-04 Landing Gear Warning

INT/POL/25/1: Affected requirement JAR 25.729(e)(2) to (4)

JAA/737-700/SC/D-14CRI D-14 Exit Configuration

Affected Requirement: JAR25.807

JAA/737-700/SC/F-01CRI F-01 High Intensity Radiated Field (HIRF)

INT/POL/25/2: Affected requirement JAR25.1431(a)

JAA/737-700/SC/F-02CRI F-02 Protection from Effects of Lightning Strike; Direct Effects

INT/POL/25/3: Affected requirement JAR 25X899 and ACJ 25X899

JAA/737-700/SC/F-03

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CRI F-03 Protection from Effects of Lightning Strike; Indirect EffectsINT/POL/25/4Affected requirements: JAR 25.581, 25.899, 25.954,25.1309

6. Exemptions

The following partial exemption has been applied:

JAA/737-700/PE/D-02CRI D-02 Hydraulic System Proof Pressure Testing

Partial exemption against JAR 25 1435 (b)(l)

7. JAA Equivalent Safety Findings

JAA/737-700/ES/D-08CRI D-08 Forward and Aft Door Escape Slide Low Sill Height

Equivalent Safety with JAR 25.809(f)(l)(ii)

JAA/737-700/ES/D-16GRID-16 Automatic Overwing Exit

Equivalent Safety with JAR 25.783(f)

JAA/737-700/ES/D-17CRI D-17 Oversized Type I Exits, Maximum Number of Passengers

JAA/737-700/ES/D-18CRI D-18 Slide/Raft Inflation Gas Cylinders

Equivalent Safety with JAR 25X1436

JAA/737-700/ES/E-09CRI E-09 Automatic Fuel Shut Off

Equivalent Safety with JAR 25.979(b)(l)

JAA/737-700/ES/F-15CRI F-15 Wing tip Position Lights

Equivalent Safety with JAR 25.1389(b)(3)

JAA/737-900/ES/9/C-01CRI 9/C-01 Material Strength Properties and Design Values

Equivalent Safety with JAR 25.613

JAA/737-900/ES/9/C-04CRI 9/C-04 Control Systems

Equivalent Safety with JAR 25.395(a)

JAA/737-900/ES/9/D-02CRI 9/D-02 Environmental Control Systems (Packs Off take-off)

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17th March 2001


Equivalent Safety with JAR 25.831 (a)

8. JAA Environmental Standards:

Noise: ICAO Annex 16 Volume I (Third Edition)Fuel Venting & Emissions: ICAO Annex 16 Volume II (Second Edition).

(E)III. TECHNICAL CHARACTERISTICS AND OPERATIONAL LIMITATIONS

Design Standard:

Dimensions:

Denned by Boeing Top Drawing No. 001AOOO1-900 Rev. HK,dated 6th March 2001 and later approved changes, andProduction Revision Record (PRR) No.38906


34.32m42.1m12.57m124.65 m2


1341 ft2

3. Engines: Two CFM 56-7B Turbo fan Engines



SLS Thrust (LB)CFM56-7B24

24,20022,800

CFM56-7B2626,30025,900

CFM56-7B2727,30025,900

CFM56-7B27/B127,30025,900

3.1 Engine Limits: For other limitations, see DGAC France Engine TypeCertificate Data Sheet.

OperatingConditions


Rotor Speed (%)Nl104104N/AN/A

Rotor Speed (%)N2105105

N/AN/A




4. Air Speeds: Refer to Approved Airplane Flight Manual (See Section IV)

5. Maximum Operating Altitude: 12,497 m (41,000 ft) pressure altitude

6. All-weather Capability: Cat 3 (with 50 ft. decision height)

7. *Maximum Weights:

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9.

10.

11.

12.

13.


174,700 Ibs.1 74,200 Ibs.146,300 Ibs.140,300 Ibs.

79,229 kg.79,002 kg.66,349 kg.63,628 kg.

Centre of Gravity Range:

Datum:

See Approved Airplane Flight Manual

Weight & Balance Manual

Mean Aerodynamic Cord (MAC): 3.96 m (155.81 in)




Exits: Boeing B737-900:

1 Main Fwd LH2 Main Aft LH3 Service (Fwd, RH, Aft, RH)4 Overwing/Emergency left5 Overwing/Emergency right

Number11

1+122




Cockpit side window (2) | Flight Crew Emergency Exit 483 x 508 (19 x 20)

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15.

16.

17.


ClassCN/ACN/A

Volume m3 (ft3)

N/A

N/A

Wheels and Tyres:

Nose Assy (Qty 2) Tyre: 27 x 7.75 - 15 or 27 x7.75 - R15Wheel: 27 x 7.75 - 15

Main Assy (Qty 4) Tyre: H43.5 x 16.0 - 21 or H44.5 x 16.5 - 21Wheel: HR44.5 x 16.5 -21


Required Equipment: The approved equipment is listed in: CRJ 9/A-10

ETOPS Operation

The Type Design of this aircraft has been approved for ETOPS Operation up to 180Minutes diversion time provided the Configuration, Maintenance and Proceduresrequirements of Boeing Document D044A007 Issue C (or later issue) are compliedwith.

(C)IV OPERATING AND SERVICE INSTRUCTIONS



2. Service Information:2.1 Maintenance Manual, Document No. D633A101

2.2 Maintenance Review Board Report Revision 3 together with MRBR Supplementfor 737-700C and 737-900 as JAA Approved 12th January 2000; subsequent JAAapproved revision

2.3 Airworthiness Limitations and Certification Maintenance Requirements:737-600/700/800 Maintenance Planning Document (MPD) Document Section 9Ref: D626A001, Revision Dated March 2001, and later revisions thereof

2.4 Service Letters and Service Bulletins.

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Anhang 1 zum LBA-Geratekennblatt Nr. 2823Boeing 737-600 / -700 / -800, -900

Ausgabe: 7Datum: 14. Mai 2001 Seite 1 von 1

Erqanzunqen und Beschrankunqen des LBA-Geratekennblattes 2823:

1. Dieses LBA-Geratekennblatt besteht aus einem Deckblatt, dem Boeing 737-600 / -700 / -8007 -900 JAA Data Sheet Nr. JAA/25/97-018 issue 7 und demAnhang 1 ,,Erganzungen und Beschrankungen des LBA-Geratekennblattes2823" (Ausgabe 7 vom 14. Mai 2001).

2. Alle vorgeschriebenen Schilder und Beschriftungen, die Anweisungen furPassagiere enthalten, mussen an den vorgesehenen Stellen in deutscherSprache angebracht sein (mit Ausnahme des Wortes ,,Exit").

—ENDE—

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