BAE SYSTEMS 

PUBLICATIONS TRANSMITTAL 

THE INFORMATION CONTAINED IN THIS TRANSMITTAL COMPUES WITH THE BRITISH CIVIL 

AIRWORTHINESS REQUIREMENTS, SECTION A, CHAPTER A5·3. THE TECHNICAL ACCURACY OF 

:::e~NFO:z;;;;;EN V::::IED AND IS~~:;~;~ :~r~:~C:pproval No. EASA 21 J.04 7 

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J~l Aircraft Maintenance Manual 

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INSTRUCTIONS FOR INCORPORATION 

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BAE SYSTEMS 

Jetstream Series 4100 

Aircraft Maintenance Manual 

STATEMENT OF INITIAL CERTIFICATION 

s.:~ec.Ukis document Is approved under the authOIIty of oo::roval No. EASA.21J.047. 

EASA Pan 21 Approval No. EASA.21J.047 

NOTE: 

I he ab0\1> certrllcaUon dOO$ noo apply to revt•lons made aner the data of Initial certrllcaUon by olher Appr<Mld Organo .. uon• 

Revisions mAde by other Af)proved Organisauons must each be separately oerttficd, and recordOO on scparato rceotd shoots. 

The copyright in tnis dOCument, v.tuch r.onta1ns lnfonnouon of a proprietary o.ature, is ves.tecJ m BAE SYSTEMS The contents of 

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wholly or in part. In any way what&oover, nor may 1t be used by, or Its: contents dwulgnd to. ony person whatsoever Without lhe 

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BAE SYSTEMS and its sub&~dlafY, atf.,late and associt~ted companies: d1&e1.8im all hablhty 't'.'llelher m oontracl or m tort mclud~ttg 

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© BAE SYSTEMS 2013. All ~Is rese.ved 

BAE SYSTEMS (Opcrotions) UmrOO<J, Ref!lonal Aircraft 

PrestW!Ck International Airport. Prostvock, Ayn;hloe, KA9 2RW, Unrted l<ing<fom 
CH/SE/SU till. 

INTRO-CONTENTS I 

SB ll ST I 

INTRO I 

INTRO 2 

INTRO 3 

INTRO 4 

INTRO 5 

I NTRO 6 

INTRO 7 

INTRO 8 

INTRO 9 

INTRO 10 

INTRO II 

INTRO 12 

INTRO 13 

INTRO 14 

INTRO 15 

FLEET CODES 1 

403 

I 

BRITISH AEROSPJIIC6 

J41 Aircrafl ~ainlenance Kanual 

INTRODUCTION 

LIST OF EFFECTIVE PAGES 

!!ill. CH/SE/SU PAGE DATE 

DEC 01/97 

DEC 01/97 

JUL 15/00 

DEC 01/97 

DEC 01/97 

DEC 01/97 

DEC Dl/97 

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JUL 15/00 

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INTRO-LOEP 

Page I 

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Subject 

INTRO 

SERV ICE BULLETIN LIST 

I NTROO UCTI ON 

BRITISH AEROSI'?ACE 

J41 Aircraf t Maintenance Manua l 

INTRODUCT ION 

TABLE Of CONTENTS 

FLEET CODE CROSS REFERENCE TABLE 

403 INTRO-CONTENTS 

Page I 

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SERV ICE BULLET IN LIST 

Service Rev Embod iment Title/Description Bu I I e t i n No No Oa te 

SB LIST 

Page 1 

DEC 01/97 
I 

BRITISH AEROSPJJIC6 

J41 Aircraft ~intenance Kanual 

** FOR AIRCRAfT All** 

INTRODUCTION 

I. The Authority for this Kanual 

A. Airworthiness Au thorities 

This Aircraft Ma in tenance Kanual (AIIK) is part of the set of manuals 

suppl led with the approval of these authorities: 

- tivi I Aviation Authority (CAA), UK 

- Federal Aviation Administration (FAA), USA 

-Joint Aviation Authorities (JAA) , Europe. 

B. Certification 

Certification of the a ircraft Is to: 

- Federal Aviation Regulations (FAR) Part 25 - Airworthiness Standards - Transport Category Airplanes 

- Joint Aviation Regulations (JAR) 25 - large Aeroplanes. 

C. Related Manuals 

The manuals included In the set are: 

- Aircraft Maintenance Kanual (AKM) 

-Aircraft Illustrated Parts Catalog (AI PC) 

- Aircraft Recovery Manual (ARK) 

- Component Ma intenance Manual (C~ 

- Engine ~ i ntenance llanua 1 (EM) 

-Engine Illustrated Parts Catalog (EIPC) 

- Engineers lla intenance and Troubleshooting Guide (EKTG) 

- Illustrated Tool and Equipment Kanual (ITEII) 

-Non-Destructive Testing llanual (NOT) - Quick Engine Change (QEC) llanual 

-Structurally Significant Items (SSI) Inspection llanual - Structural Repair Manual (SRI'\) 

- Troub I eshoot i ng 1\anua I (TSK) - Wiring Kanu al (WK) 

- Weight and Balance Manual (WBI'I). 

NOTE: The engine manufacturer supplies the EM and the EIPC. Write to the 

engine manufacturer If you have a problem with the EM or the EIPC. 

If you have a problem with one of the other manuals, write to BAE 

SYSTEIIS (OPERAT IONS) Ltd. on a publications query form (copies of the 

form are supplied with the set of manuals), and send It to: 

- BAE SYSTEKS (Operations) ltd. - Prestwick International Airport 

- Ayrsh ire 

- KA9 2RW - Scotland. 

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J41 Aircraft ~aintenance ~anual 

You can get more copies of tho Publications Query form if you write 

to this address. 

2. The Specification of this ~anual 

This manual is written to the 4ir Transport 4ssociation of 4mer ica 

Specification No. 100 (ATAIOO) at Revision 29. The maintenance tasks are 

written in the 4ircraft ~aintenance Task Oriented Support System (A~TOSS). 

The writing rules and vocabulary are in accordance with the AEC~A Simplified 

English Document No. PSC-85-16598 Revision 5. All spelling is in Amer ican 

Eng! ish. 

J. The ~anual Content 

A. Preliminary Pages 

(I) The A~ contains a set of Preliminary Pages and a set of Chapters. The 

preliminary pages include: 

-The Title Page - An Aircraft Effectivity Page 

-A List of Effective Pages (LEP) which lists the Record pages and the 

pages of this Introduction 

- Record of Revisions Pages - Record of Temporary Revisions Pages 

-Record of Service Bulletins Pages 

- These Introduction Pages - A List of Chapters. 

8. The Chapter Number System 

(I) The A~ has these groups of characters: 

(a) Aircraft General 

-Chapter 05 Time Limits/~aintenance Checks - Chapter 06 Dimensions and Areas 

- Chapter 07 Lifting and Shoring -Chapter 08 Leveling and Weighing 

-Chapter 09 Towing and Ta~iing 

- Chapter 10 Park ing, ~ooring, Storage and Return to Service 

-Chapter II Placards and ~arkings 

- Chapter 12 Servicing. 

(b) Airframe Systems 

- Chapter 20 Standard Practices - Airframe 

- Chapter 21 Ai r Conditioning - Chapter 22 Auto fl ight-

- Chapter 23 Communications 

- Chapter 24 Electrical Power - Chapter 25 Equipment/Furnishings 

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BRITISH AEROSRIICI/E 

J4l Aircraft "aintenance "anual 

- Chapter 26 Fire Protection 

- Chapter 27 Flight Controls - Chapter 28 Fuel - Chapter 29 Hydraulic Power 

- Chapter 30 lee and Rain Protection 

- Chapter 31 Indi cation/Recording Systems - Chapter 32 Landing Gear - Chapter 33 Ll ghts - Chapter 34 Navigation 

- Chapter 35 Oxygen 

- Chapter 38 Water/ Waste. 

(c) Structures 

- Chapter 51 Standard Practices and Structures General - Chapter 52 Doors - Chapter 53 Fuselage - Chapter 54 Nacel les 

- Chapter 55 Stabilizers - Chapter 56 WIndows - Chapter 57 Wings. 

(d) Propel I ers 

- Ch ap ter 61 Prope II ers. 

(e) Power Plant 

- Chapter 70 Standard Practices - Engine - Chapter 71 Power Plant - Chapter 72 Engine 

- Chapter 73 Engine Fuel and Control - Chapter 74 Ignition - Chapter 75 Air - Chapter 76 Engine Controls - Chapter 77 Engine Indicating 

- Chapter 78 Exhaust - Chapter 79 Oil - Chapter 80 Starling 

- Chapter 82 Water I nj cct I on. 

Tab Dividers 

At the front of each chapter there is a yellow tab card. The chapter number 

and title are shown on the tab. There are also yellow tab cards at the 

front of the Record of Revisions, and the Introduction. 

D. ldenti flcation Code (Ref. Fig. l) 

An identification code that has six numbers divides the chapter Into its 

related parts. This Identification code is divided into three clements. 

Each element contains two numbers. The code divides the data Into: 

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J41 Aircraft intenance Manual 

-Chapter/System (First element) 

- Section/Sub-system (Second element) 

- Subject/Unit (Third elemenl). 

Sec:ond E l eaent 

T~ 1 rd Element 

21-30-05 

L Subject/Unit (Pr~asure Con!roller) 

Hu•bers 01 thru 99 

are used 11 nec.e1sary 

Chapter /Sys tea -- (Air Conditioning) 

Soct1on/Subsyste• (Pres sur i :.at ion Contra l) 

Nuabers 1 thru 9 ar~ 

us ed in tht fourth part 

of the nuabe-r to fd ent f fy 

the sub·sub-systaa 

00002001/00 

First/Second/Third Element 

Figure 1 

E. The Page Number System (Ref. Fig. 2) 

(1) A system of page numbers divides each Chapter-Section-Subject (CH-SE-SU) into page blocks and topics, as follows: 

- Page Block - Page Block 

- Page Block 

- Page Block - Page Block 

- Page Block 

- Page Block 

- Page Block 

I -Description and Operation 201 - Maintenance Practices 

301 - Servicing 

401 -Removal/Installation 

50i - Adjustment/Test 

60i - Inspection/Check 

701 - Cleaning/Painting 80i - Repairs. 

00 oo- 2000t 

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(2) The page Identification code, which includes the CH-SE-SU code, is 

given at the bottom right side of each page. 

00002002/00 

21 -30-05 

Air Conditioning ______j J 

Pressurization Control 

Prassure Controller 

Page Identification 

F lgure 2 

F. The list of Effective Pages (LEP) 

Third page of 

Removel/lnstol l otion 

topic(Pege Block L01) 

L Page 403 

I ""' 1/92 

Oate of issue 

of Page 403 

(I) The lEP of each chapter gives a list, in number sequence, of pages 

contained in the chapter. The lEP Includes a list of the Contents and 

lEP pages and comes immediately before the Contents pages. 

(2) The data adjacent to each page number on the lEP shows the date for 

that page and, i r applicable the configuration (conf ig). The number of 

pages contained in a chapter and the data on each page must agree with 

the LEP data. 

(3) Each time a chapter has a revision, a new LEP is issued to give the new 

date of the changed pages. 

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G. The Table of Contents Pages 

The table of contents pages for each chapter give a list, in CH-SE-SU 

number sequence, of the subjects included in a chapter. The topics for each 

subject are listed in page block sequence. 

H. Task Index 

The task index pages, tor each chapter, give a list In AMTOSS task number order (para 6.8. (I)) of the tasks Included in the chapter. The task index 

also shows the task title and page number of the first page of each task. 

Tasks are not necessarily in task number order in the chapter. 

1. The Figure and Table Number System 

The figure and table number system in a page block Is the same as the page 

number system. For example, the second figure in a Maintenance Practices 

page block is Figure 202, the first table in a Servicing page block is 

Table 301. A Figure or table is put into the page block as near to the 

related text as possible. 

I J. Data in this Manual 

(I) The d~ta given in t his manual includes the: 

- Data necessary to do the tasks in the Maintenance Planning documents 

-Data that describes the aircraft, its structure and systems, and 

tells how the systems operate. Data is illustrated as necessary 

-Procedures and related safety precautions for 'on-aircraft' servicing and maintenance necessary for continued airworthiness. 

For data related to 'off-aircraft' maintenance and/or special maintenance, use the applicable manual. Refer to the list given in para 

I.C. of this introduct ion. 

I (2) Equivalent Tools, Fixtures and Test Equipment 

The tools, fixtures and test equipment which are necessary to a given 

maintenance task are referenced In the applicable AMM procedure. These 

i terns are recommended by BAE SYSTEMS (Operations) Lld to accomplish the given AMM procedure. The aircraft operator can use equivalent tools, 

fixtures or test equipment as alternatives to those referenced in the 

AKM if those items agree with the conditions that follow: 

-Functionally interchangeable with those referenced in the AKM 

-Applicable to the given maintenance procedure 

- Equally safe for the equipment and for the person or persons who are 

accomplishing the Procedure 

- BAE SYSTEIIS (Operations) Ltd. assumes no responsibi II ty for the use 

of the a lternat ive tools, fixtures and test equipment. 

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J41 Aircraft Halntenance Hanual 

In some cases, the recommended tools and fixtures given in the 

applicable maintenance procedure are given to make the removal or 

installation of a component easier. While the maintenance procedure may 

specify these tools and fixtures to aid the person or persons who 

accompl ish the maintenance, the maintenance procedure may be 

accompl ished If the tools or fixtures are not available (un less 

spec ified differently) with t he cond i tions that follow: 

-The intent of t he maintenance procedu re is not significantly altered 

and the revised maintenance procedure Is approved by the operator's engineer ing authority. BAE SYSTEHS (Operations) Ltd . assumes no 

responsibility for the precision of the revised maintenance 

procedure. 

-The maintenance procedure remains equally safe for the equipment and 

for the person or persons who do the maintenance. 

4. Page Block and Topic Contents 

[" 

A. Page Block 1 - Description and Operation 

(1) This topic gives sufficient data to train maintenance persons to know 

the function, the configuration, the ope ration and the control or the 

system, structure or component. 

B. Page Block 201 - Halntenance Practices 

(1) This topic includes all maintenance procedures, applicable to a 

CH-SE-SU, easily contained in one page block. Page Block 201 is also 

for those maintenance procedures which are not related to the topics of 

other page blocks. 

C. Page Block )01 - Servicing 

(1) This page block contains the applicable data for scheduled and 

unscheduled servicing. 

0. Page Block 401 - Removal/Instal latlon 

(I) This topic gives the necessary data for the removal and Installation of 

a unit/assembly. 

E. Page Block 501 - Adjustment/Test 

(1) This topic gives the data necessary to adjust and/or do a test of a 

system, sub-system, assembly or unit. There are three types of test: 

(a) The Operational Test is the procedure to make sure that a system, 

sub-system. assembly or unit operates. Special equipment is not 

necessary for this test. 

(b) The Functional Test is the procedure to make sure that a system, 

sub-system, assembly or unl t, is correctly adjusted and functions fully 

EFFECTIVITY: ALL INTRO 

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J~l Aircraft "a intenance "anual 

to its specification. This test usually uses special equipment to 

measure the performance of the system, sub-system, assembly or unit. 

(c) The System Test has all the adjustment and functional test data for the 

complete system. 

F. Page Block 601 - Inspection/Check 

(1) This topic gives the data necessary to make sure that a system. sub-system, assembly, unit or part Is serviceable. 

G. Page Block 701 - Cleaning/Painting 

(1) This topic gives the data necessary to clean and/or paint parts or 

areas of the aircraft. 

H. Page Block 801 -Repa i rs 

(1) This topic gives repair procedures that are necessary during 

maintenance and not Included in the Structural Repair "anual. 

5. Effectivity (Ref. Fig . 3) 

A. The Effectivity Block 

When data is applicable to specified aircraft or groups of aircraft, the 

effectivity block gives the "anufacturers Serial Numbers ("SN) of the 

aircraft. The effectivity block is at the bottom left side of each page. 

B. The "anufacturers Serial Number 

The MSN Is a three part number used to show that the data on a page is 

applicable to specified aircraft. The MSN are listed In number sequence. A 

hyphen is used to separate a group of "SN that are in one number after the 

other sequence. A comma is used to separate all other "SN. When the data on 

a page is applicable to all aircraft, the effectivity block contains the 

word ALL. 

6. How to use this Manual 

A. Applicable Data 

Do these steps to find the data in this manual: 

(1) If necessary, refer to the list of chapters in the Preliminary Pages 

and find the number of the chapter. 

(2) Read the yellow tab cards to identify the chapter. 

(3) Open the manual at the start of the chapter and refer to the Table of 

Contents pages or the Task Index pages. 

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Effec t ivity: 001-008,010,015,017-020, 023,025- 030 

Exaapl e 1 

Effectivity: All 

Exomp le 2 

Effectivity 

figure 3 

Oo-cc-2JCOl 

(4) Identify the CH-SE-SU on the Table of Contents pages or the task number 

from the Task Index pages. 

(5) Identify the page block applicable to the necessary data (Refer to para 

J.E. of this Introduction for a list of the page block numbers and 

their t i tIcs) . 

(6) An example of 

as follows: 

(a) To find the 

l ldenti fy 

~ Refer to 

l Ident ify 

EFFECTIVITY: All 

the procedure given in para 6.A. of this introduction i $ 

data to remove and install 

that the i tern Is structural 

the list of Chapters In para 

the chapter (Ref. Chapter 57 

a wing tip 

and part of 

J.B.(I)(c) 

- Wings). 

cover, you must: 

the wing. 

Structures. 

INTRO 

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J41 Aircraft ~intenance "anual 

! Use the yellow tab cards in the manual to locate Chapter 57- Wings. 

2 Refer to the Contents at the start of Chapter 57 and identify the 

necessary data which is 57-30-05, Page Block 401 - Wing Tip Cover 

Removal/Installation. You can also refer to the Task Index and 

identify the removal and installation tasks which are Task 

57-30-05-000-810 and Task 57-30-05-400-815. 

~Open the manual at 57-30-05, Page Block 401 where you wil I find the 

necessary procedures to remove and install the wing tip . 

B. AMTOSS codes (Ref. Fig. 4) 

( I) For the function of Automated Data Retrieval (ADR) , A"TOSS codes are 

included in Page Blocks 201 thru 801. AMTOSS gives each of the 

maintenance procedures (tasks) and the primary steps or the procedures 

(sub tasks) a different number identification code. 

(2) The identification code numbers have a minimum of five elements and a 

maximum of seven clements. These elements are an extension of the three 

element ATAIOO CH-SE-SU numbers. 

(3) Apart from its use In this manual, the AMTOSS codes give the opera tor a 

Production Management Data Base (PMOB). The PMDB Is used to help the 

maintenance planner to plan the maintenance tasks as necessary. These 

same codes are used In the production or the Jetstrcam Automatic 

Workcard System (Ref. para 9.B.). 

]. Revisions and Service Bulletins 

A. Issue of Revisions 

(I) The manufacturer regularly issues revisions to the maintenance manual 

to keep it at the correct standard. The revisions add, delete and/or 

change data as necessary. All rev1s1ons are by replacement of pages. 

You must not use hand-written revisions. 

(2) A letter of Transmittal is sent with every revision. The transmittal 

letter: 

- Is the authority to put the revision In the manual 

- Gives instructions on how to put the revision into the manual 

- Includes a Highlight column that gives a short description of the 

change to the page. 

You are recommended to keep the transmittal letters, at the front of 

the manual, for reference. 

(3) Each reference has a specified number and date. Revisions start at No.I 

and have numbers in sequence after that. 

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Seventh Ele•enc - The code for taaks or sub-tasks which ere apechl to t ht operator . For exa•ple,taalc.s/sub-tatks written by the operator 

or- by 1 sub-eontrac.tor. 

S ix th Ele•ent- Identification of configuration differences 

C11od\ f 1 c. at 1 on a 1 tandards) and differences in procedures. For 

Figures and Tables this ele•tnt shows the different sheet numbers. 

fifth Elt!tllt- Task/sub-tolk ldtntification nu11ber. 

Thia nu11ber,together with the 'first four ele11ents h 

opp llcoble to this task/1ub·tuk onty.All other 

tasks/tub-tasks which have tht Slllt four elements 

wil l htve 1 different fifth e lttUrH number.Nu•bert 

801 thru 999 oro used for tnks, end 001 thru 800 

a,.e used for sub- tasks. 

rourtl\ Element- Function code Nu•ber 

<400 h Inatollatlon) 

Firat thry !bird Elements- Equipaent ldenttficotlon (CH·SE-SU) 

----------T--------=--1 ASK 25-10-15-400-805-XXX-XXX 

Sub-tou S 25-10-15-420-001-XXX-XXX 

J EqU 1P•tnt/furnish i ngs 

Flight Co•pertment 

Crtw Stl t& 

First prf•ary step o"- t he crev ttlt tnstal l :•..:.•..:.l..:.o.::n ________ _J procedure after any ne-ccessary job tet-up procedur es •rt done 

Configurea/Operator codes 11 neceasery ----------------.J 

0000200VOO 

r03 EFFECTIVITY: ALL 

~TOSS Code Identification 

Figure 4 

oc 00100!• 

INTRO 

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J~l Aircraft "aintenance ~nual 

(4) A Record of Revisions page Is given at the front of the manual. When 

you have put a revision Into the manual, you must write the revision 

number and its issue date on the Record of Revisions page. 

(5) The vertical black line at the left side of a page shows that the data 

adjacent to the line has changed. If a black l ine is aligned with the 

page number and date, this shows that the data has not changed, some of 

the data has moved to or from a different page. 

B. Temporary Revisions 

(1) When it is necessary to include data in the manual quickly, a Temporary 

Revision (TR) is issued. The first page of the TR gives the transmittal 

instructions. The data/Instructions in a TR replace the equivalent 

data/instructions In the manual. A TR can a lso be used to Include data 

In advance of the next revision. 

(2} Each TR Is printed on yellow paper. The TR numbers are in sequence and 

start at -1 in each chapter. The chapter number goes in front of the TR 

number to give every TR an identification code . For example 27-1, 27-2. 27-3 and so on, 32-1, 32-2, 32-3 and so on. 

(3) The data/instructions In a TR Is either included In a rev ision 

(usua ll y, the next revision to the manual) or a subsequent TR replaces 

it. When a revision includes the data/instructions of a TR , the 

transmittal letter includes an instruction to remove the applicable TR. 

When a subsequent TR replaces a TR, the subsequent TR includes an 

instruction to remove the applicable TR. You must not remove a TR from 

the manual unless you get an instruction to do so (In the Transmittal 

letter of a revision or on the first page of a subsequent TR) . 

(4) At the front of this manual, immediately after the Record of Revisions 

page, is a Record of Temporary Revisions page. When you put a TR into 

the manual, you must wr ite the TR number (and the date you put the TR 

into the manual} on the record of Temporary Revisions. When you remove 

a TR from the manual, you must write the authority (Revision number or 

later TR number} on the Record of Temporary Revisions page. 

C. Service Bulletins 

(I) At the front of this manual, immediately after the Record of Temporary 

Revisions is a Record of Service Bulletins page. The data given 

includes the Serv ice Bulletin (SB) No., its issue number, the date of 

issue, and the revision that included it. 

(2) When text is dependant on the embodiment of a service bulletin, 'PRE 

SB' and 'POST 58' Information is included in the manual. When BAE 

SYSTEMS (Operations) Ltd. receive confirmati on of the embodiment, the 

'PRE 58' Information is deleted at the next revision. 

EfFECTIVITY: ALL INTRO 

Page 12 

JUL 15/00 
BRITISH AEROSFJIICii' 

J~l Aircraft "aintenance "anual 

8. What to do When You Get this "anual 

A. Procedure 

(1) At initial issue, a "ANUAL REGISTRATION card and two CHANGE OF ADDRESS 

cards are included at the front of the manual. 

J (2) When you get this manual d irectly from BAE SYSTE"S (Operations) Ltd.: 

-Write the necessary details on the "ANUAl REGISTRATION card 

- Send the ca rd t o the address given on the card. 

You wl 11 then get a full revision service for the manual . 

(3) When you get the manua l from a different operator: 

-Write the necessary details on the CHANGE OF ADDRESS card (include 

the last revision number that is written in the Record of Revisions) 

- Send the card to the address given on the card. 

You will then gel the revisions necessary to make the manual the 

correct standard . You will also be registered to get the full revision 

service. 

(4) If the cards have been used write to: 

- BAE SYSTE"S (Operations) ltd. 

- Prestwick International Airport 

- Ayrshire 

- KA9 2RW 

- Scotland. 

9. Compact Discs 

[" 

A. Interactive Electronic Technica l " anua ls (lET") 

The A"" is also produced as an lET" on a compact disc (CD). The technical 

data used In the A"" is computerised and is held in a central data store. 

This technical data is then put on the CD and is, therefore, the same data 

as that shown in the A"". 

The CD lets you use the A"" in the same way as if it were a hard copy manual. However, because of the interactive links and search facilities, It 

is quicker and easier to use than the hard copy. There arc highlighted 

blocks of text at each level of the A"" , which are used to cross refer to 

other referenced data. The high l ighted areas for references are in blue but 

change to yellow when the cursor Is placed in the arco. The highlighted 

references for graphics are In black. A click of the mouse button then 

takes you to the applicable data. For a full description of how to use the 

CD RO", refer to the CD RO" User Guide which is supplied with the initial 

Issue of your CD . 

EffECTIVITY: ALL INTRO 

Page 13 

JUl 15/00 
I 

BRITISH AEROSRIICIE 

J~l Aircraft Maintenance Manua l 

There are, however, a number of differences between the CO and the AMM 

which are not described In the CO ROM User Guide. These are due to the 

r equirements of the CO and are shown below. 

(I) list of Chapters 

A List of chapters Is shown which gives direct links to the Table of 

Contents for each Chapter. 

(2) Table of Contents 

The table of contents g ives links only to chapter headings and AKTOSS 

task numbers. 

(3) list of Effective Pages 

The data is held on the CO in documents and is shown as a series of 

page blocks. Because of this there is no requirement for a page number 

system and, therefore, there is no LEP. 

(4) ldenti f !cation Code 

The Identification code used Is the same as In the AMM, however the 

chapter, section, subject and page block number are shown at the top of 

the screen. This Is because there is no page number system. 

(5) Effectivity 

When data is appl icable to specified aircraft or groups of aircraft, 

the effectivity Is shown Immediately before the data to which it 

app l ies. The effectivity block of the AMM is not used on the CO. 

(6) Revisions 

Revisions to the CO are issued each time the AMM Is revised. A 

replacement CO is sent which includes all the revised data. 

A Transmittal is included on each revised CO wh ich shows the revised 

page blocks and a reason for change. The Transmittal also includes the 

revision number which Is the same as the revision number shown on the 

hard copy Transmittal. There is no record of revisions page. 

The signs @R@,@@ are shown at the left side of the screen to identify 

the data that has changed. 

B. Jetstream Automa tic Workcard System 

All the scheduled maintenance tasks and inspection requirements, given In 

the Maintenance Planning Document, are avai I able on a CO in a work and 

planning card layout. Different layouts are available for the work and 

planning cards so that operators can comply with their own maintenance 

philosophy and the requirements of their regulatory authority. You must 

EFFECTIVITY: All INTRO 

Page I~ 

JUL 15/00 
I 

BRITISH AERDSF'JIICE J~l Aircraft ~alntenance ~anual 

write to BAE SYSTE~S (Operations) Ltd. at the address shown if you want 

changes to your workcard system (Ref. ~ara 8.A. (~)). 

The system is li nked to the operators maintenance programme and allows 

workcards and planning informat ion to be printed for each maintenance 

interval. Planning information for service intervals includes: 

-Access panels- gives all access panels which must be removed for each 

service interval 

-Too ls and equipment- gives all the necessary tools and equipment 

-Consumable materials- gives all the necessary lubricants 

- x~endable parts - gives the necessary catalog sequence number from the 

I PC. 

The workcard CD is revised regularly at the same time as the A~. A list of revised workcards is shown on the CO and each revised card shows the page 

date of the AMM and Is given a new Issue number. 

EFFECT IVITY: ALL INTRO 

Page 15 

JUL 15/00 
Constructor•s 

Number 

41012 

41013 

41015 

41017 

41019 

41020 

41021 

41022 

41023 

41025 

41026 

41027 

41028 

41029 

41031 

41033 

41041 

41042 

41043 

41045 

41055 

41058 

41059 

41063 

41064 

41080 

41083 

41097 

41098 

41099 

41100 

41101 

403 

I 

BRITISH AEROSPJIIC6 

J41 Aircraft Kaintenance Kanua1 

flEET CODE CROSS REFERENCE TABLE 

Atlantic Coast 

Set Number Tai I Number 

12 N301UE 

13 N302UE 

15 N303UE 

17 N324UE 

19 N305UE 

20 N306UE 

21 N307UE 

22 N309UE 

23 N)08UE 

25 N312UE 

26 N313UE 

27 N314UE 

28 N310UE 

29 N311UE 

31 N317UE 

33 N315U£ 

41 N318UE 

42 N319UE 

43 N320UE 

45 N321UE 

55 N316UE 

58 N322UE 

59 NJ23UE 

63 N325UE 

64 N326UE 

80 N327UE 

83 N828UE 

97 N329UE 

98 N))OUE 

99 N331UE 

100 N332UE 

101 N333UE 

Customer fleet 

Effectivity Code 

012 

013 

015 

017 

019 

020 

021 

022 

023 

025 

026 

027 

028 

029 

031 

033 

041 

042 

043 

045 

055 

058 

059 

063 

064 

080 

08) 

097 

098 

099 

100 

101 

FLEET CODES 

Page I 

JUL 15/00 

BRITISH AEROSPACE 

J41 Aircraft Maintenance Manual 

CHAPTER OS 

AIRWORTHINESS LIMITATIONS 

LIST OF EFFECTIVE PAGES 

CH/SE/SU PAGE Qill. CH/SE/SU ~ Qill. 

OS-CONTENTS I AUG 1S/II OS-10-10 43 FEB 1S/07 

OS-TASK INDEX 1 AUG IS/ 11 OS-10-10 44 FEB 15/07 

OS-TASK INDEX 2 AUG 15/11 05-10-10 45 AUG 15/11 

05-10-00 I JAN 15/13 05-10-10 46 AUG 15/11 

OS-10-10 I SEP 15/04 05-10-10 47 JAN 15/13 

05-10-10 2 JAN 15/13 05-10-20 1 DEC 01/97 

05-10-10 3 JAN 15/13 05-10-20 2 FEB 15/10 

05-10-10 4 JAN 15/13 05-10-20 3 SEP 15/04 

05-10-10 5 JAN 15/13 05-10-20 4 OCT 15/99 

05-10-10 6 JAN 15/13 05-10-20 5 DEC 01/97 

05-10-10 7 JAN 15/13 05-10-30 I FEB 15/08 

05-10-10 8 FEB 15/05 05-10-30 2 FEB 15/08 

05-10-10 9 FEB 15/05 05-50-00 1 DEC 01/97 

05-10-10 10 SEP 15/13 05-50-10 601 DEC 01/97 

05-10-10 11 FEB 15/07 05-50-10 602 DEC 01/97 

05-10-10 12 AUG 15/10 05-50-12 601 DEC 01/97 

05-10-10 13 FEB 15/07 05-50-12 602 DEC 01/97 

05-10-10 14 FEB 15/07 05-50-15 601 AUG 15/11 

05-10-10 IS FEB 15/07 OS-50-1S 602 AUG 15/ II 

05-10-10 16 FEB 15/09 OS-50-1S 603 AUG 15/ 11 

05-10-10 17 FEB 15/07 OS-50-1S 604 AUG 15/ 11 

05-10-10 18 AUG 15/11 05-50-1S 605 AUG 15/11 

05-10-10 19 AUG 15/11 05-so-15 606 AUG15/11 

05-10-10 20 AUG 15/11 05-S0-15 607 AUG 15/11 

05-10-10 21 AUG 15/11 05-50-15 608 AUG 15/11 

OS-10-10 22 AUG 15/11 05-50-15 609 AUG 15/11 

05-10-10 23 AUG 15/11 05-50-15 610 AUG15/11 

05- 10- 10 24 AUG 15/11 05-50-15 611 AUG 15/11 

05-10-10 25 AUG 15/11 05-50-15 701 AUG 15/11 

05-10-10 26 AUG 15/11 05-50-15 702 AUG 15/11 

05-10-10 27 AUG 15/11 05-50-15 703 AUG 15/11 

05-10-10 28 FEB 15/09 05-50-15 704 AUG 15/11 

05-10-10 29 FEB 15/09 05-50-20 601 DEC 01/97 

05-10-10 30 FEB 15/09 05-50-20 602 DEC 01/97 

OS-10-10 31 FEB 15/09 05-50-20 603 DEC 01/97 

05-10-10 32 FEB 15/09 05-50-30 601 JUL 15/00 

05-10-10 33 FEB 15/09 05-50-30 602 JUL 15/00 

05- 10-10 34 FEB 15/09 05-50-30 603 FEB 15/00 

05-10-10 35 FEB 15/09 05-50-30 604 JUL 15/00 

05-10-10 36 FEB 15/09 05-50-32 601 DEC 01/97 

05-10-10 37 FEB 15/09 05-50-32 602 DEC 01/97 

05-10-10 38 FEB 15/09 05-50-32 603 DEC 01/97 

05-10-10 39 FEB 15/09 05-50-32 604 DEC 01/97 

05-10-10 40 FEB 15/09 05-50-32 605 DEC 01/97 

05-10-10 41 FEB 15/07 05-50-34 601 DEC 0 1/97 

05-10-10 42 FEB 15/07 05-50-34 602 DEC 01/97 

403 05-LOEP 

Page I 

I SEP 15/13 
BRITISH AERDSI'MCE 

J41 Aircraft Maintenance Manual 

CH/SE/SU PAGE DATE CH/SE/SU fill. DATE 

OS-S0-34 603 DEC Ol/97 os-50-76 603 DEC 01/97 

05-50-34 604 DEC Ol/97 05-50-76 604 SEP 15/05 

05-50-36 601 DEC 01/97 05-50-76 605 SEP 15/05 

05-50-36 602 DEC 01/97 05-50

-

78 601 DEC 01/97 

05-50-36 603 DEC 01/97 05-50-78 602 DEC 01/97 

OS-50-40 601 DEC 01/97 05-50-78 603 DEC 01/97 

05-50-40 602 DEC 01/97 05-50-80 601 DEC 01/97 

05-50-40 603 DEC 01/97 05-so-8o 602 DEC 01/97 

os-50

- 50 601 DEC 01/97 05-50-80 603 DEC 01/97 

05-50-50 602 DEC 01/97 05-50-82 601 DEC D1/97 

05-50-50 603 DEC 01/97 05

- 50-82 602 DEC 01/97 

05-50-50 604 DEC 01/97 05-50-82 603 DEC 01/97 

05-50-50 605 DEC 01/97 05-50-84 601 DEC 01/97 

05-50-52 601 DEC 01/97 05-50-84 602 DEC 01/97 

05-50-52 602 DEC 01/97 05-50-84 603 DEC 01/97 

05-50-52 603 DEC 01/97 05-50-86 601 FEB 15/02 

05-50-60 601 DEC 01/97 05-50-86 602 FEB 15/02 

05-50-60 602 DEC 01/97 05-50-88 601 AUG 15/11 

05-50-60 603 DEC 01/97 05-50-88 602 AUG 15/11 

05-50-62 601 DEC 

0

1/97 05-50-88 603 AUG 15/11 

05-50-62 602 DEC 

0

1/97 05-50-88 604 AUG 15/11 

05-50-62 603 DEC 01/97 os-so-88 605 AUG 15/11 

OS-S0-62 604 DEC 

0

1/97 os-5o-88 606 AUG 15/11 

05-50-64 601 DEC 

0

1/97 

05-50-64 602 DEC 

0

1/97 

05-50-66 601 DEC 

0

1/97 

05-50-66 602 DEC 01/97 

05-50-66 603 DEC 01/97 

05-50-66 604 DEC 01/97 

05-50-66 605 DEC 01/97 

05-50-70 601 DEC 01/97 

05-50-70 602 DEC 01/97 

05-50-72 601 SEP 15/04 

05-50-72 602 SEP 15/04 

05-50-72 603 SEP 15/04 

05-50-]2 604 SEP 15/04 

05-50-]2 605 SEP 15/04 

05-50-72 606 SEP 15/04 

05-50-72 607 SEP 15/04 

05

- 50-72 608 SEP 15/04 

05-50-72 609 SEP 15/04 

05-50-72 610 SEP 15/04 

05-50-72 611 SEP 15/04 

05-50-72 612 SEP 15/04 

05-50-72 613 SEP 15/04 

05-50-]2 614 SEP 15/04 

05-50-74 601 DEC 01/97 

05-50

- 74 602 DEC 01/97 

05-50-74 603 DEC 01/97 

05-50-74 604 DEC 01/97 

05-50-76 601 FEB 15/06 

05-50-76 602 FEB 15/02 

403 05-LOEP 

I Page 2 

SEP 15/13 
I 

BRITISH AEROSRACE 

Subiect 

GE NERAL 

TASK INDEX 

KANOATORY LIFE LIKITATIONS 

TIKE LIKITS 

J~l Aircraft Kaintenance Kanual 

CHAPTER OS 

AIRWORTHINESS LIKITATIONS 

TABLE OF CONTENTS 

AIRWORTHINESS LIKITATIONS 

CERTIFICATION NTENANCE REQUIREKENTS 

CRITICAL DESIGN CONFIGURATION CONTROL LIKITATIONS (COCCL) - FUEL SYSTEK 

KAINTENANCE CHECKS - GENERAL 

ICE AND SNOW CONDITIONS 

FLIGHT IN VERY BAD OUST CONDITIONS 

CONTAKINATION BY OUST/SAND/VOLCANIC ASH 

EXPLOSIVE DECOKPRESSION 

LIGHTNING STRIKE AND STATIC DISCHARGE 

LEAKAGE OF KERCURY 

LEAKAGE OF ALKALINE ELECTROLYTE 

LEAKAGE OF ACID ELECTROLYTE 

FIRE IN THE ENGINE NACELLE 

SLAK DEFLECTION OF A CONTROL SURFACE 

FLAPS EXTENDED AT TOO HIGH A SPEED 

HIGH ENERGY STOP 

TIRES 

LANDING WITH HIGH DRAG OR SIDE LOADS 

LAND ING GEAR EXTENDED AT TOO HIGH A SPEED 

BIRO STRIKE 

HEAVY LANDING 

LANDING WHEN THE AIRCRAFT WAS TOO HEAVY 

FLIGHT IN HEAVY TURBULENCE OR EXTREKE HANOEUVRES OR BUFFETING 

FLIGHT THROUGH HAIL 

PROPELLER STRIKE/SUDDEN ENGINE DECELERATION 

BAD ENG INE VIBRATION OR PROPELLER VIBRATION 

ENGI NE/PROPELLER 

UNDAKPEO DOOR OPENING 

AIRFRAHE SYHHETRY CHECK 

Ch/Se/Su 

OS-10-00 

OS-10-10 

OS-10-20 

05-10-30 

os-so-oo 

05-50-10 

os-50-12 

05-50-15 

05-50-20 

05-50-30 

OS-S0-32 

05-50-34 

05-50-36 

05-50-40 

05-50-50 

05-50-52 

05-50-60 

05-50-62 

05-50-64 

05-50-66 

OS-S0-70 

OS-50-72 

05-S0-74 

05-50-76 

05-50-78 

05-50-80 

05-50-82 

o5-50-84 

05-50-86 

05-50-88 

403 OS-CONTENTS 

Page 1 

AUG 15/11 
I 

05-50-10-210-801 

05-50-12-210-801 

05-50-15-100-801 

05-50-15-100-802 

05-50-15-200-801 

05-50-15-200-802 

05-50-20-210-801 

05-50-30-2 10-80 1 

05-50-32-210-801 

05-50-34-210-801 

05-50-36-210-801 

05-50-40-210-801 

05-50-50- 210-801 

05-50-52-210-801 

403 

BRITISH AEROSMIICE 

J41 Aircraft Maintenance Manua l 

CHAPTER 05 

AIRWORTHINESS LIMITATIONS 

TASK INDEX 

Ch/Se/Su Page 

Oo an Inspection Before Flight in lee 05-50-10 

and Snow Conditions 

Do an Inspection Afte r a Flight in 05-50-12 

Very Bad Dust Conditions 

General 05-50-15 

Cleaning After Flight Through 05-50-15 

Oust/Sand Storm/Volcanic Ash/Oust or 

Severe Conditions on Ground. 

General 05-50-15 

Inspection After Flight Through 05-50-15 

Oust/Sand Storm/Volcanic Ash/Oust or 

Severe Conditions on Ground. 

Do an Inspect ion after an Explosive 05-50-20 

Decompression 

Do an Inspect ion of the Aircraft 05-50-30 

After a Report of a Lightn ing Strike 

Do an Inspection after a Leakage of 05-50-32 

Mercury 

Do an Inspection after a Leakage of 05-50-34 

Alka line Electrolyte 

Do an Inspection after a Leakage of 05-50-36 

Ac id Electrolyte 

Do an Inspection after a Fire in the 05-50-40 

Engine Nacelle 

Do an Inspection after a Slam 

Deflection of a Control Surface 

05-50-50 

601 

60 I 

701 

702 

601 

602 

601 

601 

60 I 

601 

601 

601 

601 

Do an Inspec tion After the Flaps were 05-50-52 601 

Extended at Too High a Speed 

05-TASK INDEX 

Page I 

AUG 15/11 
I 

05-50-60-21o-8o1 

05-50-62-210-801 

05-50-64-210-801 

05-50-66-21o-8o1 

05-50-70-210-801 

05-50-72-21 o-8o 1 

05-50-74-210-801 

05-50-76-210-801 

05-50-78-210-801 

o5-50-8o-21o-8o1 

05-50-82-210-801 

05-50-84-210-801 

o5-50-86-21o-8o1 

o5-50-88-21o-8o1 

o5-50-88-21o-8o2 

403 

BRITISH AEROSPACIE 

J~l Aircraft ~aintenance ~anual 

~ Ch/Se/Su Page 

Do an Inspection Following Emergency 05-50-60 601 

Stops Using ~aximum Braking From 

Speeds of 90 kts or Greater 

Do an Inspection after a Landing with 05-50-62 601 

Burst Tires or Tires with Flat Areas 

Do an Inspection after a Landing with 05-50-6~ 601 

High Drag or Side Loads 

Do an Inspec t ion After the Landing 05-50-66 601 

Gear was Extended at Too High a Speed 

Do an Inspection After the Aircraft 05-50-70 601 

Has Hit a Bird or Birds 

Do an Inspection of the Aircraft 05-50-72 601 

After a Heavy Landing 

Do an Inspection of the Aircraft 05-50-74 601 

After a Landing When the Aircraft was 

Too Heavy 

Do an Inspection After a Flight in 05-50-76 601 

Heavy Turbulence or Extreme 

~anoeuvres or Buffet ing 

Do an Inspection After Flight through 05-50-78 

Ha i I 

Do an Inspection after a Propeller 05-50-80 

Strike or Sudden Engine Deceleration 

Do an Inspection after Bad Engine 05-50-82 

Vibration or Propeller Vibration 

Do an 1 nspec t ion after an 05-50-84 

Engine/Propeller Overspeed 

Do an Inspection of the Passenger 05-50-86 

Door after an Undamped Opening 

Do a Symmetry Check of the Airframe 05-50-88 

Do a Rigging Check of the Airframe 05-50-88 

05-TASK 

601 

601 

601 

601 

601 

601 

602 

INDEX 

Page 2 

AUG 15/ll 
** FOR AIRCRAFT All** 

I. General 

BRITISH AEROSRIIC6 

J41 Aircraft Maintenance Manual 

TIME LI MITS 

DESCRIPTION AND OPERATION 

A. Mandatory Time Limits 

This section gives the instructions for continued airworthiness of the 

Jetstream 4100 aircraft. The section includes the mandatory time limits 

for the inspection of the aircraft structure, replacement of parts and the 

necessary maintenance of equipment. The instructions are divided into two 

sections: 

- Airworthiness Limitations (Ref . 05-10-10) 

- Certification Maintenance Requirements (Ref . 05- 10-20). 

B. Airworthiness limits 

The Airworthiness Limitations section is confined to structural items only . 

It gives the structural life limits of the primary parts of the aircraft. 

The section also gives mandatory replacement time, times between structural 

inspections and the related AMM procedure references as approved In Joint 

Aviation Requi rements (JAR) and Federa l Aviation Requirements (FAR) 25.571. 

C. Certification Maintenance Requirements 

The Certification Maintenance Requir ements (CMR's) are confined to the 

equipment, systems and installations. It gives the references to the 

maintenance inspections procedures and the maximum time between inspections 

as approved in JAR/FAR 25.1309. The CMR's are necessary to keep the same 

level of aircraft airworthiness as at certification. 

D. Inspection Requirements 

Where there is a conflict of Information for an inspection requirement 

defined against more than one airworthiness directive of EASA or the 

airworthiness authority of the state of design, the most severe Inspection 

requirement must be observed. 

E. Structural Repair Manual (SRM). (Ref. SA.4-4100/SRM/400) 

The SRM detai Is inspection tasks for pub I ished repairs to fatigue critical 

structure (Ref. AMM 05-10-10, paragraph 4). These Inspections are 

additional to the Inspections of the airframe detailed In AMM 05- 10-10, 

paragraph 3. The inspection tasks are only applicable if the repair is 

f itted to the a ircraft. 

EFFECTIVITY : ALL 05-10-00 

Page 1 

JAN 15/13 
I 

I 

** FOR AIRCRAFT ALL** 

I. General 

A. Approval 

BRITISH AEROSRIICE 

J4 1 Aircraft Maintenance Manual 

AIRWORTHINESS LIMITATIONS 

DESCRIPTION AND OPERATION 

(I) THIS AIRWORTHINESS LI MITATIONS SECTION IS APPROVED BY EASA AND 

VARIATIONS MUST ALSO BE AP PROVED BY EA SA (JAR-25 APPENDIX II PARAGRAPH 

H25 . 4) . 

(2) THE FAA SPEC IFIED MAINTENANCE REQUIRED UNDER PARAGRAPHS 43.16 AND 

91 . 403 Of THE FEDERAL AVIATION REGULATIONS, MUST BE IN ACCORDANCE WITH 

THE MANUFATURER'S PUBLISHED DATA, UNL ESS AN ALTERNATIVE PROGRAMME HAS 

BEEN FAA APPROVED. 

B. Description 

(1) This section is confined to structura l i terns only. It gives each 

mandatory replacement time, structural inspection interval, and related 

structural inspection procedure approved under JAR/FAR 25.571. 

(2) The Jetstream 4100 ai rcraft is bui It to damage-tolerant design 

standards with a design economic repair life of 60000 flights . 

(3) An analysis has been made of all the airplane structure as required 

under JAR/FAR 25.571. The only primary component with a structural 

life l imi t is the landing gear . The analysis has also given the 

initial and subsequent inspection ti mes for Structurally Significant 

I terns (S S I ) . 

(4) The Components/Parts wl t h a I ife I imi t 

this Section under their part number. 

given in number of landings. 

are listed in pa ragraph 2 of 

The mandatory life limit is 

(5) Retirement lives are calculated from the date of fi rst installation 

after original manufacture, and are not re-set to zero following any 

upgrade to a later modification standard. 

(6) The struc tural inspection times for t he SSis are listed in paragraph 3 

of this Section. The Tables in paragraph 3 are in ATA chapter/section 

sequence and list the SSis, the init i al and subsequent inspection times 

in flight cycles and the associated inspection procedure (AMM TASK 

REF) . Each SSt is identified as a seven digit sequence number, fo r 

examp le 52-10-001. The first four numbers ident ify the ATA 

chapter/section and the last three numbers are the SSt sequential 

number in t hat ATA section . 

C. Airplane Maintenance Program 

(I) The Airplane Maintenance Program must Include all listed SSis with 

initial and subsequent inspection times not exceed ing the listed times . 

Lo3 EFFECT IVITY: ALL 05-10-10 

Page 1 

SEP 15/04 
I 

EIRI77SH AEROSAIICE 

J41 Aircraft Maintenance Manual 

The listed times may not be increased without consultation with the 

airplane manufacturer and specific approval from the responsible 

JAA/FAA Aircraft Certification Office. 

(2) The Airplane Maintenance Program must also provide for the mandatory 

replacement of the life limited items at or before the expiry of the 

listed mandatory 1 ife limit for the Item. The 1 isted mandatory I lfe 

limit may not be exceeded wi thout consultat ion with the airplane 

manufacturer and specific approval from the responsible JAA/FAA 

Aircraft Certification Office. 

2. life Limited Component Parts 

A. Supplementary Retirement Criteria 

(1) Landing gear units overhauled after 12th July 2002 must have the lives 

of all life limited components, listed in Tables I and 3 and identified 

by an asterisk (*),established, and any components found to be in 

excess of the published lives must be removed from the landing gear 

uni L. 

(2) Any other installed landing gear units where the life of a component , 

listed in Tables 1 and 3 and Identified by an asterisk (*),cannot be 

established, or where the component has exceeded the published life 

limit, must be removed before 31st March 2008. 

B. Main landing Gear 

UNIT NUMBER PART NUMBER 

AIR84352 Drag *AIRi31374 

Stay 

AIR84352 Drag *AIR131372 

Stay 

AIR84352 Drag !tAIRI36146 

Stay 

AIR84352 Drag *AIRI23734 

Stay 

AIR84352 Drag *AIRI31468 

Stay 

AIR84352 Drag *AIR131444 

Stay 

r., EFFECTIVITY: All 

Table I 

DESCRIPTION 

Lower Link 

Upper Link 

Upper Link 

lock lever 

Pin, Retract 

Actuator 

Pin, Pivot 

MANDATORY ll FE 

LIMITS (LANDINGS) 

66500 

37400 

37400 

66500 

66500 

66500 

05-10-10 

Page 2 

JAN 15/13 
BRITISH AEROSPJAC6 

J~l Aircraft Kaintenance Kanua l 

Table continued ... 

UNIT NUKBER PART NUKBER DESCRIPTION MANDATORY LIFE 

LIKITS (LAND I NGS) 

AIR8~352 Drag *AIRI35160 Trunnion, 66500 

Stay Outboard 

R8~352 Drag *A IR135158 Trunnion, Inboard 66500 

Stay 

AIR83072 Shock *A IR131366 Cyl inder 66500 

strut 

A1R83090 Shock 

strut 

AIR83072 Shock *AIR131368 Piston 36000 

strut 

AIR83090 Shock 

strut 

AI R83072 Shock *AIR131370 Torque Arm, Lower 37~00 

strut 

41R83090 Shock 

strut 

AIR83072 Shock *A IR136210 Torque Arm, Lower 37~00 

strut 

AIR83090 Shock 

strut 

AIR83072 Shock *AIR131382 Torque Arm, Upper 37400 

strut 

AIR83090 Shock 

strut 

AIR83072 Shock *4IR136206 To rque Arm, Upper 37400 

strut 

AIR83090 Shock 

strut 

AIR83072 Shock *AIR 31~32 Apex Pin, Torque 66500 

strut 4rm 

AIR83090 Shock 

strut 

AIR83072 Shock *A 31~52 Pin, Torque Arm 66500 

strut 

AIR83090 Shock 

strut 

I" 

EFFECTIVITY : All 05-10-10 

Page 3 

JAN 15/13 
I 

UNIT NUMBER 

AIR83072 Shock 

strut 

AIR83090 Shock 

strut 

AIR83072 Shock 

strut 

AIR83090 Shock 

strut 

A I R83072 Shock 

strut 

AIR83090 Shock 

strut 

AIR83072 Shock 

strut 

AIR83090 Shock 

strut 

AIR83072 Shock 

strut 

AIR83090 Shock 

strut 

A I R83072 Shock 

strut 

AIR83090 Shock 

strut 

AIR86496 

AIR86496 

AIR85339 

BRITISH AEROSRIICE 

J4l Aircraft Maintenance Manual 

Table continued ... 

PART NUMBER 

*AIR I35154 

*AIRI41824 

DESCRIPTION 

Trunnion, Door 

Drive 

Trunnion, Door 

Drive 

MANDATORY LIFE 

lit\ ITS (LAND I NGS) 

36000 

36000 

*AIRI35156 Trunnion Threaded 66500 

*AIR141826 

*AIRI31444 

*AIRI31468 

AlR8&496/l 

AIR8&49&/2 

AIR8&49&/0 

ALL 

AIRI344 14 

AIR134415 

Trunnion Threaded 66500 

Attachment Pin , Drag Stay 

Pin, Retract 

Actuator 

Retract Actuator 

Retract Actuator 

Gear Uplock 

Left lever 

Right lever 

66500 

66500 

60000 

12200 

60000 

24000 

24000 

NOTE: 1: Note l is no longer required. 

NOTE: 2: If component records are found to be incomplete, do either of the 

following: Remove the component from service, or refer to SB 

J41-05-00l wh ich provides data for the calculation of an assumed life 

EFFECTIVITY : All 05-10-10 

Page 4 

JAN 15/13 
I'' 

BRITISH AEROS,qlfC6 

J~l Alrcrart ~aintenance ~anual 

for the component. Where the calculated life is greater than the life 

stated in this chapter, the component must be removed from service. 

NOTE: 3: Ret irement l ives ~recalculated from the date of first 

installation after original manufacture, and are not re-set to zero 

following any upgrade to a later modifi cation standard. 

PART NUMBER 

1~152055 401 

C. Nose landing Gear 

UNIT NUMBER 

AIRB358& Shock 

Strut 

AIR8358& Shock 

Strut 

AIR83586 Shock 

Strut 

AIR83586 Shock 

Strut 

AIRB358& Shock 

Strut 

A I R83586 Shock 

Strut 

AIR83586 Shock 

Strut 

AIR83586 Shock 

Strut 

AIR83586 Shock 

Strut 

AIR83586 Shock 

Strut 

EFFECT IVITY: All 

Table 2 

DESCRIPTION ~ANOATORY LIFE LI MITS 

(FLYING HOURS) 

Aft door hinge bracket 16600 

Table 3 

PART NUMBER DESCRIPTION 

*AIR131378 Piston, Main 

*AIR131376 Casing, Main 

*A RI~I68~ Casing, /lain 

IR 3171~ Pinion, Steering 

AIR136088 Pinion, Steering 

AI RI~I516 Pinion, Steering 

*AIR131672 Rack, Steering 

Actuator 

*AIR131880 Piston, Steering 

*A IRI31728 Housing, Steering 

*A IR131756 Capsule, 

Shortening 

MANDATORY l IFE 

LI MI TS (L ANDINGS) 

60000 

60000 

See Note ~ 

60000 

See Note 4 

19000 

12000 

See Note 5 

60000 

33000 

60000 

60000 

60000 

05-10-10 

Page 5 

JAN 15/13 
BRITISH AEROSFMC6 

J41 Aircraft ~aintenance ~anual 

Table 3 continued ... 

UNIT NU~BER PART NU~BER DESCRIPTION ~ANDATORY LIFE 

L1 ~ITS (LAND I NGS) 

AIR83586 Shock *AIRI31796 Shortening Arm, 60000 

Strut Upper 

AIR83586 Shock *AIRI31788 Shortening Arm, 60000 

Strut Lower 

AIR83586 Shock *AIRI31800 Shortening Arm, 60000 

Strut Drag 

AIR83586 Shock *AIR131778 Pin Shortening 60000 

Strut ~ech, Lower 

A I R83586 Shock *AIR131782 Pin Shortening 60000 

Strut Mech, Centre 

AIR83586 Shock *AIR131804 Pin Shortening 60000 

Strut Mech, Upper 

AIR83586 Shock *A IR131806 Pin Shortening 60000 

Strut Mech, Aft 

AIR83586 Shock *AIR131882 Pin, Downlock 60000 

Strut 

AIR83586 Shock *A I R 131912 Trunnion, Stbd 60000 

Strut 

A I R83586 Shock *AIRI32516 Trunnion. Port 60000 

Strut 

AIR83586 Shock *AIR131870 Torque Arm, Upper 60000 

Strut 

AIR83586 Shock *A1Ri3i380 Torque Arm, Lower 60000 

Strut 

AIR83586 Shock *AIR 13 I 770 Pin, Torque Arm 60000 

Strut Apex 

AIR83586 Shock *AIRI31918 Pin, Torque Arm 60000 

Strut 

AIR83586 Shock *A I R 131686 Axle 60000 

Strut 

AIR83586 Shock *AIRI35044 Towing Bracket 12000 

Strut See Note 6 

[" EFFECTIVITY: ALL 05-10-10 

Page 6 

I JAN 15/13 
I 

BRITISH AEROSFMCE 

J41 Aircraft ~aintenance ~anual 

Table 3 continued .•• 

UN IT U~B R PART NUIIBER DESCRIPTION AN TORY LIFE 

LI ~I TS (LAN DINGS) 

AI R85334 All Down lock 60000 

AI R85344 All Down lock 60000 

AIR85336 All Up lock 60000 

AIR86478 ALL Retract Actuator 60000 

NOTE: I : Note I is no longer required . 

NOTE: 2: If component records are found to be incomplete, do either of the 

following: Remove the component from service, or refer to SB 

J41 -05-001 which provides data for the calculation of an assumed life 

stated in this chapter, the component must be removed from service . 

NOTE : 3: Retirement l ives are calcu lated from the date of first 

insta l lation after original manufacture, and are not re-set to zero 

fo ll owing any upgrade to a later modification standard. 

NOTE: 4: Service Bulletin J4l-A32-079 has been introduced to inspect for, 

and rectify any cracks that may be found in the casing. 

~ 5: Service Bulletin J4l-32-076 provides information relating to the 

life limitations for this part. 

NOTE: 6: For ease of tracking, this part will be discarded and replaced at 

overhaul. Refer to Service Bulletin J41-32-070 for further 

information. 

D. Fuel System 

NOTE : If component records are found to be incomp lete , do either of the 

fol lowi ng: Remove the component fr om service , or refer to SB 

J4 1-05-001 which provides data for the calculation of an assumed l ife 

for the component . Where the calculated life is greater than the life 

stated in this chapter, the component must be removed from service . 

PART NU~BER 

14128007-401 

EFFECTIVITY: ALL 

Table 4 

DESCRIPTION 

Negative 'G' tank 

(Pre-repair 

2JA93090200IR) 

~ANDATORY LIFE LI~ITS 

(LAND I NGS) 

15000 

05-10-10 

Page 1 

JAN 15/13 
I 

I 

I" 

BRITISH AEROSFtiiCE 

J41 Aircraft Ma intenance Manual 

Table 4 continued ... 

PART NUMBER DESCRIPTI ON MANDATORY l l FE l iMI TS 

(lAND INGS) 

14128007-402 Negative IGI tank 15000 

(Pre-repa ir 

2JA9 3090200 I R) 

14128007-401 Negative IG I tank 15000 

(Post- repair 

2JA93090200 lR) 

14128007-402 Negative ' G' tank 15000 

(Post-repair 

2JA9 30902001R) 

14128042-401 Negative IG I tank 15000 

(Postmod 41279. Premed 

41492) 

14128042-402 Negative IG I tank 15000 

(Postmod 41279. Premed 

41492) 

14128042-409 Negative I Gl tank 60000 

(Postmod 41492) 

14128042-410 Negative I G I tank 60000 

(Postmod 41492) 

E. Flap and Spoi ler Control Systems 

NOTE: If component records are found to be incomplete, do either of t he 

foll owing: Remove the component from service, or refer to SB 

J41-05-001 which provides data for the ca lcu lation of an assumed li fe 

for the component. Where the calculated life is greater t han t he li fe 

stated in this chapter, the component must be removed from service. 

NOTE: Retirement lives are calcu la ted from t he date of first Installation 

after or igi nal manufacture, and are not re-set to zero following any 

upgrade to a later mod ification standard. 

Table 5 

PART NUMBER DESCR IPTION /lANDA TORY l l FE l iiiiTS 

(lANDINGS) 

TY1763-0lA Spoi ler Actuator 5000 See Note 

TY1763-01 B Spoi ler Actuator 5000 See No te 

EFFECTIVITY: ALL 

I 

05- 10-10 

Page 8 

FEB 15/05 
I 

I 

F. 

BRITISH AEROSRACE 

J41 Aircraft Maintenance Manua l 

Table 5 continued . .. 

PART NUMBER DESCRIPTION MANDATORY LIFE Ll MITS 

(LAND I NGS) 

TY 1763-01C Spoi I er Actuator 15000 See No te 

TY 1763-010 Spoiler Actuator 15000 See Note 

NOTE: Spoiler Actuator Part No. 's TY1763-0 1A, TY1763-0IB, TY1763-0IC and 

TY1763-0ID are eligible for increase in I lfe to 60000 land ings by 

upgrading to TY1763-02A standard by incorporation of Optional BAe SB 

J41-27-058. 

TY 1763-02A Spoiler Actuator 60000 

TY 1756-02A Flap Hydraulic Control 2000 

Un i t 

TY1756-03A Flap Hydraulic Control 5000 

Un it 

TY 1756-03B Flap Hydraulic Control 5000 

Unit 

TY1756-03C Flap Hydraulic Control 60000 

Unit 

TY1757-01A Flap Actuator 500 

TY1757-02A Flap Actuator 60000 

TYI757-02B Flap Actuator 60000 

Main Baggage Bay Door 

NOTE: If component records are found to be incomple te, do either of the 

--follow ing : Remove the component from service, or refer to SB 

J41 -05-001 which provides data for the calculation of an assumed life 

for the component. Where the calculated li fe is greater t han the l ife 

stated in this chapter, the component must be removed from service . 

PART NUMBER 

N4082 

Table 6 

DESCRIPTION 

Main Baggage-bay 

Counter Balance Motor 

Spring 

MANDATORY LIFE LIMITS 

(LAND I NGS) 

3600 Landings 

EfFECTIVITY : ALL 05-10-10 

Page 9 

FEB 15/05 
I 

PART NU~BER 

14152026- 407 

14152026-415 

BRITISH AEROSFJfiC6 

J41 Aircraft ~aintenance ~anual 

Table 6 conLinued ... 

DESCRIPTION 

Kain Baggage-bay 

Counter Balance ~tor 

Cable 

~ain Baggage-bay 

Counter Balance Motor 

Cable 

MANDATORY LIFE LIMITS 

(LAND I NGS) 

3600 Landings 

3600 Landings 

G. Passenger Door 

I" 

NOTE: If component records are found to be incomplete, do either of the 

fo l lowing: Remove the component from service, or refer to SB 

J41-05-00I which provides data for the calculation of an assumed life 

for the component. Where the calculated life is greaLer than the 

life sLaLed In this chapter, the component must be removed from 

service. 

Tab le 7 

PART NU~BER DESCRIPTION ~ANDATORY LIFE LIMITS 

(LAND I NGS) 

14153057-1 Passenger Door Roller 34000 Landings 

Guide 

14153057-2 Passenger Door Roller 34000 Landings 

Guide 

14153057-3 Passenger Door Roller 34000 Landings 

Guide 

14153057-4 Passenger Door Roller 340DO Landings 

Guide 

14153057-93 Passenger Door Roller 34000 Landings 

Guide 

14 153057-94 Passenger Door Roller 34000 Landings 

Guide 

14153057-95 Passenger Door Roller 34000 Landings 

Guide 

14153057-96 Passenger Door Roller 34000 Landings 

Guide 

EFFECTIVITY: ALL 05-10-10 

Page 10 

SEP 15/13 
I 

BRITISH AERDSFMCIF 

J~l Aircraft Maintenance Manual 

** FOR AIRCRAFT 012-013 015-015 017-017 019-023 025-029 031-031 033-033 

0~1-0~3** 

H. Rear Emergency Exit 

NOTE: 1: If component records are found to be incomplete, do either of the 

following: Remove the component from service, or refer to SB 

J~l-05-001 which provides data for t he ca lculation of an assumed life 

for the component . Where the calculated li fe is greater than the 

life stated In this chapter , the component must be removed from 

service . 

NOTE: 2: Rep lace life expired cleats by embodiment of modification JM41277A 

(SB J41-53-0 14) 

PART NUMBER 

14153083-26 

** FOR AIRCRAFT ALL** 

I. Forward Pressure Bulkhead 

Table 8 

DESCRIPTION 

Cleats 

MANDATORY LIFE LIMITS 

(LAND I NGS) 

7200 see note 2 

NOTE: If component records are found to be incomplete, do either of the 

following: Remove the component from service, or refer to SB 

J41 -05-001 which prov ides data for the calculation of an assumed life 

for the component. Where the calculated life is greater than the 

life stated in this chapter, the component must be removed from 

service. 

Tab le 9 

PART NUMBER DESCRIPTION 

NAS6305-29D Bolt (2 OFF) 

EFFECTIVITY: All 

MANDATORY LIFE liMITS 

(LAND I NCS) 

26000 

05-10-10 

Page 11 

FEB 15/07 
I 

BRITISH AERDSAIICE 

J41 Aircraft Maintenance Manual 

J. Power plant 

hble 10 

PART NUMBER DESCRIPTION MANDATORY LIFE LIMITS 

(FlYI NG HOURS) 

95054-01 Forward engine iso lator 6000 

elastomerlc components 

NOTE: Part No. 95054-01 life limitation may be extended for aircraft Post 

Mod. JM 41413, in accordance with SB J41-]l-024. 

95054-02 Rear engine isolator 3000 

elastomeric components 

(Post Mod. JM 41073. 

Pre Mod. JM 41413) 

95054-02 Rear engine isolator 400 

elastomeric components 

(Pre Mod. JM 41073. Pre 

Mod . JM 4 14 I 3) 

95054-05 Rear engine Isolator 6000 

elastomeric components 

(Pos l Mod. JM4 14 1 3) 

NOTE: Part No. 95054-05 life limitation may be extended in accordance with -- SB J41-71-024. 

3. Structurally Significant Items (SSis) 

A. Chapter 52 - Doors 

Passenger/Crew Door 

NOTE: Information on all SSI numbers preceeded by an asterisk (*)will be 

superseded by information given In service bulletin J41 - 51 -00 I. 

Table 11 

SSI NUMBER REFERENCED TASK AND ITEM 

DESCRIPTION 

52-10-001 TASK 52-10-05-210-870 Outer 

Skin 

52-10-001 TASK 52-10-05-2 10-829 

Airsta irs Hinges 

EFFECTIVITY: All 

INITIAL 

INSPECTION 

20000-26000 

Flights 

20000-26000 

Flights 

SUBSEQUENT 

INSPECTIONS 

3300 F I i ghts 

30000 Flights 

05-10-10 

Page 12 

AUG 15/10 
BRITISH AEROS,!=JIICE 

J41 Aircraft Maintenance Manual 

Table 11 continued ... 

SSI NUMBER REFERENCED TASK AND ITEM INITIAL SUBSEQUENT 

DESCRIPTION INSPECTION INSPECTIONS 

*52-10-008 TASK 52-10-05-210-828 20000-22500 3300 F I i ghts 

Roller Guide Assemblies Fl ights 

*52-10-008A TASK 52-10-05-250-801 20000-22500 30000 F I ights Roller Guide Assembly Flights 

F i tt i ng Bores 

** FOR AIRCRAFT 012-013 015-015 017-017 019-023 025-029 031-031 033-033 041-043 

045-045 055-055 058-059 063-064 080-080 083-083 097-099** 

52-10-009 TASK 52-10-05-210-831 Top 

Ro ller Guide Support 

Structure 

** FOR A I RCRAFT 100-101 ** 

52-10-009 TASK 52-10-05-210-831 Top 

Roller Guide Support 

Structure 

** FOR AIRCRAFT All** 

52-10-009A TASK 52-10-05-2 10-832 Side 

Pans 

52-10-009B TASK 52-10-05-2 10-833 Seal 

Carriers 

52-10-010 TASK 52- 10-05-210-844 Stop 

52- 10-011 TASK 52-10-05-210-849 Edge 

Member 

52-10-013 TASK 52-10-05-2 10-855 Door 

Frame at Splice Joint 

52-10-015 TASK 52-10-05-210-860 Cross 

Beam/Outer Sk in at 

Attachment to Skin 

52-10-016 TASK 52-10-05-210-834 

Formers and lntercostals 

EFFECTIVITY: All 

6000 F 1 i ghts 

30000-40000 

Fl ights 

37400 Flights 

30000 Flights 

26000-30000 

Flights 

30000-40000 

Flights 

30000-40000 

Flights 

30000-40000 

Flights 

29800 Flights 

1500 Fl ights 

I 2000 F I i gh ts 

36500 Flights 

30000 Flights 

30000 Fl ights 

14300 Flights 

30000 Flights 

30000 Flights 

16600 Flights 

05-10-10 

Page 13 

FEB 15/07 
I" 

I 

SSI NUMBER 

52- 10-017 

BRITISH AERDSFMCE 

J41 Aircraft Maintenance Manual 

Table 11 continued ... 

REFERENCED TASK AND ITEM 

DESCRIPTION 

TASK 52-10-05-210-865 Fore 

and Af t Intercostal 

Attachment to Door Frame 

INIT IAL 

INSPECTION 

30000-40000 

Flights 

SUBSEQUENT 

INSPECTIONS 

30000 Flights 

Overwing Emergency Exits 

SSI NUMBER 

*52-20-001 

52-20-002 

52-20-003 

52-20-005 

52-20-007 

52-20-008 

52-20-009 

52-20-011 

52-20-012 

52-20-013 

Table 12 

REFERENCED TASK AND ITEM 

DESCRIPTION 

TASK 52- 20-05-210-809 

Sur round Beam 

TASK 52-20-05-210-815 lower 

Vertical Beam 

TASK 52-20-05-210-819 

Bottom Abutment Fittings 

TASK 52-20-05-2i0-824 

Bottom Abutment fitting 

Surround Structure 

TASK 52-20-05-210-830 Side 

Abutment Stop Block 

Attachment 

TASK 52-20-05-210-835 Cross 

Beam at Side Abutment 

TASK 52-20-05-2i0-839 Top Abutment Retrac table 

Shootbolt Fitting 

TASK 52-20-05-210-844 Top 

Abutment Fitting Surround 

Structure 

TASK 52-20-05-210-860 Outer 

Skin 

TASK 52-20-05-210-849 

Window Structure 

EFFECTIVITY: All 

INITIAL SUBSEQUENT 

INSPECTION INSPECTIONS 

20000 Flights 5200 Flights 

30000-40000 

F 1 i ghts 

20000-26000 

Flights 

20000-26000 

Flights 

30000-40000 

Flights 

23000 Flights 

6600 Fl ights 

6500 F 1 i ghts 

30000 F 1 i ghts 

20000-26000 6100 Flights 

Flights 

26000-30000 13000 Flights 

Flights 

30000- 40000 30000 Flights 

Fli ghts 

30000 Flights 7300 Flights 

20000-26000 9200 Flights Flights 

05-10-10 

Page 14 

FEB 15/07 
I 

BRITISH AEROSPJIICB 

J41 Aircraft ~aintenance ~anua l 

Aft Emergency Exit 

Table 13 

SSI NU~BER REFERENCED TASK AND ITE~ INITIAL SUBSEQUENT 

DESCRIPTION INSPECTION INSPECTIONS 

52-20-015 TASK 52-20-10-210-805 Outer 20000-26000 3500 F 1 ights 

Skin f II ghts 

52-20-017 TASK 52-20-10-210-809 26000-30000 12000 flights 

Bottom Abutment fitting Flights 

52-20-019 TASK 52-20-10-210-814 30000-40000 30000 f 1i gh ts 

Bottom Abutment Fitting f li ghts 

Surround Structure 

52-20-021 TASK 52-20-10-210-819 Side 26000-30000 6000 Flights 

Abutment Fitting ~ounting flights 

52- 20-023 TASK 52-20- 10-210-824 Side 30000-40000 18500 Flights 

Abu tment fitting Surround flights 

Structure 

52-20-025 TASK 52-20-10-210-830 Top 26000-30000 30000 f 1 i ghts 

Abutment Retractable flights 

Shootbolt fitting 

52-20-027 TASK 52-20-10-210-835 Top 26000-30000 9400 F 1 ights 

Abutment fitting Surround Flights 

Structure 

52-20-029 TASK 52-20-10-210-840 Door 26000-30000 10300 flights 

Outer Frame Fli ghts 

52-20-031 TASK 52-20-10-210-845 20000-26000 4400 F 1 ights 

Fore-Aft Channel End flights 

Attachment 

52-20-033 TASK 52-20-10-210-860 20000-26000 6100 Fl ights 

Surround Pressing at Side flights 

Abutments 

Baggage Door 

NOTE: Information on all SSI numbers preceeded by an asterisk (*) will be 

superseded by informat ion given in service bulletin J41-5 1-001 . 

EFFECTIVITY : All 05-10-10 

Page 15 

FEB 15/07 
BRITISH AERDSRIICE 

J41 Aircraft Maintenance Manual 

Table 14 

SSI NUIIBER REFERENCED TASK AND ITE/1 INITIAL SUBSEQUENT 

DESCRIPTION INSPECTION INSPECTIONS 

52-30-001 TASK 52-30-05-210-819 Outer 30000- 40000 15000 Flights 

Skin/Stiffeners Flights 

52-30-003 TASK 52-30-05-210-841 Seal 30000 Flights 30000 Flights 

Carriers 

52-30-007 TASK 52-30-05-210-834 Side 26000-30000 30000 Flights 

Abutment Stop Fittings Flights 

*52-}0-009 TASK 52-30-05-210-822 Side 21000 Flights 10000 flights 

Abutment Stop fitting 

Surround Structure 

52-30-009A TASK 52-30-05-210-863 21000 F 11 ghts 10000 Flights 

Abutment fitting Bolts 

52-30-009B TASK 52-3D-05-210- 843 Skin 30000 - 40000 30000 Flights 

Under Abutment Flights 

52-30-011 TASK 52-30-05-210-844 Top 30000-40000 30000 Flights 

Abutment Stop Fitting F1 ights 

52-30-013 TASK 52-30-05-210-849 Top 30000-40000 30000 Flights 

Abutment Stop Fitting Flights 

Surround Structure 

52-30-015 TASK 52-30-05-210-823 lower 30000-40000 30000 Flights 

Abutment Stop Fittings flights 

52-30-017 TASK 52-30-05-210-859 Lower 30000-40000 30000fllghts Abutment Stop Fitting Flights 

Surround Structure 

*52-30-021 TASK 52-30-05-2 10-830 20000-26000 26000 Flights Korizontal Stiffeners and Flights Channels 

52-30-023 TASK 52-30-05-210-861 Side 26000-30000 19600 F I ights 

Beam flights 

52-30-024 TASK 52-30-05-210-842 Inner 31800 Flights 31800 F I ights 

Seal 

52-30-025 TASK 52-30-05-210-862 Hoop 30000-40000 30000 F I ights Beam Flights 

I" EFFECTIVITY : ALL 05-10-10 

Page 16 

I FEB 15/09 
BRITISH AEROSF!IICIE 

J41 Aircraft Haintenance Hanual 

B. Chapter 53 - Fuselage 

Ha in Structure 

NOTE: Information on a ll SSI numbers preceeded by an asterisk (*)will be 

superseded by information given In service bullet in J41-51-001. 

SSI NUHBER 

Table 15 

REFERENCED TASK AND ITEH 

DESCRIPTION 

INITIAL 

INSPECTION 

SUBSEQUENT 

INSPECTIONS 

** FOR AIRCRAFT 012-013 015-015 017-017 019-023 025-029 031-031 033-033 041-043 

045-045 055-055 058-058** 

53-10-001 TASK 53-10-00-210-839 Front 20000-21000 

Pressure Bulkhead Web Flights 

** FOR AIRCRAFT 059-059 0&3-064 080-080 083-083 097-101** 

53-10-001 TASK 53-10-00-210-839 Front 20000-26000 

Pressure Bulkhead Web Flights 

** FOR AIRCRAFT ALL** 

53-10-00lA TASK 53-10-00- 210-983 

Stiffeners on Rear face 

Only 

** FOR AIRCRAFT 097-098 PRE SB J4 1-53-23** 

53-10-002 TASK 53-10-02-210-959 

Station 4 to 8 Diaphragms 

** fOR AIRCRAFT 099-101** 

20000-26000 

Flights 

4500 flights 

3300 F I i ghts 

6000 F 1 ights 

6600 flights 

3000 F 1 ights 

** fOR AIRCRAFT 012-013 015-015 017-017 019-023 025-029 031-031 033-033 D41-043 

045-045 055-055 058-059 063-064 080-080 D83-083 097-098 POST SB J41-53-23** 

53-10-002 TASK 53-10-02-210-959 

Station 4 to 8 Diaphragms 

** fOR AIRCRAFT ALL** 

53-10-003 TASK 53-10-00-250-841 front 

Pressure Bulkhead - Ha in 

Vertical Beam at Pintle 

Bracket 

EFFECTIVITY : ALL 

36200 F I i gh ts 

20000-26000 

f l ights 

8100 flights 

21800 Flights 

05-10-10 

Page 17 

FEB 15/07 
I" 

I 

BRITISH AEROSRIICIE 

J41 Aircraft ~aintenance Manual 

Table 15 continued ... 

SSI NU~BER 

53-10-004 

REFERENCED TASK AND ITE~ 

DESCRIPTION 

TASK 53-10-04-280-801 Nose 

Fuselage Structure 

including the Avionics Bay 

Door Structure between 

Stn.4 and Stn.52. 

INITIAL SUBSEQUENT 

INSPECTION INSPECTIONS 

10000 Flights 6000 Fl ights 

~Compliance will continue to be maintained in accordance with service 

bulletin J4 1-53-047, until t he service bulleti n is cancelled. 

53-10-005 

*53-10-006 

53-10-007 

TASK 53-10-00-210-843 Front 

Pressure Bulkhead - ~ain 

Vertical Beam at Retraction 

Jack Bracket 

TASK 53-10-02-210-950 

Structure in Avionics Bay 

TASK 53-10-00-210-845 Front 

Pressure Bulkhead -

Attachment at Vertical Beam 

to Fuselage Top 

53-10-008 TASK 53-10-00-210-847 Front 

Pressure Bulkhead -

Attachment at Vertical Beam 

to Fuselage Bottom 

53-10-009 TASK 53-10-04-210-801 Front 

Pressure Bulkhead -

Secondary Beam at 

Retraction Jack Bracket 

53-10-011 TASK 53-10-00-210-851 Front 

Pressure Bulkhead - Angle 

Attaching Bulkhead to Skin 

53-10-01 lA TASK 53-10-00-210-990 Upper 

Doubler Angle Attaching 

Bulkhead to Skin 

53-10-013 TASK 53-10-00-210-853 Front 

Pressure Bulkhead Stringer 

Cleats 

*53-10-013A TASK 53-10-02-210-951 Nos e 

Spine At tachment Cleats 

EFFECTIVITY: All 

20000-26000 7400 Fl igh ts 

Flights 

23000 F I ights 10000 F 1 i ghts 

20000-26000 

Flights 

6300 Flights 

20000-26000 8300 Flights 

Flights 

26000-30000 30000 Flights 

Fl ights 

20000-26000 8800 Flights 

Flights 

20000-26000 10000 Flights 

F 1 i ghts 

20000-26000 6600 Flights 

Flights 

20000 Flights 6600 Flights 

05- 10-10 

Page 18 

AUG 15/11 
BRITISH AERDSPJIICE 

J41 Aircraft ~aintenance ~anual 

Table 15 continued ..• 

SSI NU~BER 

53-10-015 

REFERENCED TASK AN D ITE~ 

DESCRIPTION 

TASK 53-10-02-210-855 

Intercosta l Aft of Front 

Pressure Bulkhead 

*53-I0-015A TASK 53-10-02-210-952 

lntercostals Forward of 

Front Pressure Bulkhead 

53-10-017 TASK 53-10-05-210-803 

Center Keel Aft of Front 

53-10-019 

53-10-020 

*53-10-021 

53-10-022 

53-10-023 

53-10-024 

53-10-025 

53-10-027 

*53-10-028 

Pressure Bulkhead Behind 

Downlock Bracket 

TASK 53-10-05-210-801 Frame 

at Stn 71.75 Attachment to 

Windshie ld Frame 

TASK 53-10-04-210-802 

Windshield Frames Tension 

Joint 

TASK 53-10-02-210-863 Frame 

at Stn 71.75 

TASK 53-10-00-210-865 

Windshield frames A 

TASK 53-10-02-210-866 

Windshield Frame - Glazing Straps 

TASK 53-10-00-210-868 

Windshield Frames B 

TASK 53-10-00-210-871 

Canopy Structure Attachment 

Fittings 

TASK 53-10-00-210-873 Frame 

Stn 90 - Attachment to 

Windshield frame 

TASK 53-10-02-210-953 

lntercostals and Brackets 

at frames 90, 108 and 130 

EFFECTIVITY: ALL 

INITIAL 

INSPECTION 

20000-26000 

Flights 

SUBSEQUENT 

INSPECT IONS 

5400 F I i ghts 

20000 Flights 5400 Flights 

30000-40000 30000 Flights 

F I ights 

30000-40000 15800 Flights 

Flights 

26000-30000 21500 Flights 

Flights 

20000-22470 8200 Flights 

F I ights 

20000-26000 10000 Flights 

Flights 

20000-26000 11400 Flights 

Flights 

20000-22000 13800 Flights 

Flights 

20000-26000 18500 Flights 

Flights 

20000-20400 8200 Flights 

Flights 

19000 F 1 i ghts 8200 F 1 i ghts 

05-10-10 

Page 19 

AUG 15/11 
I 

SSI NUMBER 

53-10-029 

53-10-031 

53-10-033 

53- 10-035 

53-10-037 

53-10-039 

53-10-0~ I 

53-10-0~3 

53-10-045 

53-10-047 

53-I0-047A 

BRITISH AERDSFJIICE 

J~l Aircraft Maintenance Manual 

Table 15 continued ... 

REFERENCED TASK AND ITEM 

DESCRI PTION 

TASK 53-10-02-210-875 Frame 

Stn 90 

TASK 53-10-00-210-877 Frame 

Stn 108 - Attachment to 

Windshield Frame 

TASK 53-10-00-210-879 Frame 

Stn 108 

TASK 53-10-02-210-881 Frame 

Stn 130 - Windshield Straps 

at Upper and Lower Corners 

TASK 53-10-00-210-883 Frame 

Stn 130 

TASK 53-10-02-210-884 Frame 

Stn 150 - Door Aperture 

Corner 

TASK 53-10-02-2 10-886 Frame 

Stn ISO - Door Aperture 

Side 

TASK 53-10-02-210-888 Frame 

Stn 179 - Door Aperture 

Corner 

TASK 53-10-04-210-803 Frame 

Stn 179 - Door Aperture 

Side 

TASK 53-10-00-210-892 Upper 

Intercostal Between Frames 

150 and 179 - Fuselage Skin 

TASK 53-10-00-210-895 Upper 

Intercostal Between frames 

150 and 179 - Fuse lage 

Joint Strap 

TASK 53- 10-02-210-896 Lower 

Intercostal Between Frames 

150 and 179 - Fuselage Skin 

INITIAL SUBSEQUENT 

INSPECTION INSPECTIONS 

20000-21000 16900 Flights 

Flights 

20000-26000 15000 Flights 

Flights 

20000 Flights 9700 Flights 

20000-25100 15000 Flights 

Fl ights 

20000-25600 6000 Flights 

Fl ights 

20000-26000 7200 Flights 

F I ights 

20000-26000 11100 Fl ights 

F II ghts 

20000-26000 6200 Flights 

Flights 

26000-30000 18400 Flights 

Flights 

20000-26000 26400 Flights 

Flights 

20000-26000 

F II gh ts 

20000-26000 

Flights 

6100 Flights 

30000 F I i ghts 

EFFECTIVITY: All 05-10-10 

Page 20 

AUG 15/11 
I 

BRITISH AEROSRACE J~l Aircraft Maintenance Manual 

Tab le 15 continued ... 

SSI NUMBER REFERENCED TASK AND ITEM INI TIAL SUBSEQUENT 

DESCRIPTION INSPECTION INSPECTIONS 

53-10-0~9A TASK 53-10-02-210-899 Lower 20000-26000 8200 Flights 

53-10-051 

53-10-053 

53-10-053A 

53-10-055 

53-10-056 

53-10-057 

53-10-059 

53-l0-059A 

53-10-061 

53-10-061A 

53-10-063 

Intercostal Between Frames Flights 

150 and 179 - Fuselage 

Joint Strap 

TASK 53-10-00-250-901 Frame 20000-26000 30000 Fligh ts 

Stn 312- At Wing Flights 

Attachment (Vertical) 

TASK 53-10-00-250-907 Frame 

Stn 312- Outer Flange 

TASK 53-10-0~-210-80~ Frame 

Stn 312 - Inner Flange 

TASK 53-10-00-250-909 Frame 

Stn 312 - Wing Attachmen t 

(lateral) 

TASK 53-10-0~-210-805 

Stringer Cleats at Frames 

3~~. ~79 and 593 

TASK 53-10-05-270-801 Frame 

Stn 366 - Wing Attachment 

(Vertical) 

TASK 53-10-00-250-9 15 Frame 

Stn 366- Outer Flange 

TASK 53-10-0~-210-806 Frame 

Stn 366 - Inner Flange 

TASK 53-10-05-250-801 Frame 

Stn 366 - Wing At tachment 

(latera I) 

TASK 53-10-0~-210-807 Frame 

Stn 366 - Wing Attachment 

(lateral) Flange Root 

TASK 53-10-00-210-921 

Support Structure for Wing 

Drag Attachment Stn 347-389 

20000-26000 9500 Flights 

Flights 

26000-30000 8100 Flights 

F 1 i ghts 

20000-26000 7700 Flights 

Fl ights 

27000 Flights 27000 Flights 

30000-36000 7700 Flights 

F I i gh ts 

20000-26000 18300 Flights 

F I i ghts 

26000-30000 9700 Flights 

Fli ghts 

30000-36000 30000 Flights 

Flights 

26000-30000 30000 Flights 

Flights 

20000-26000 8700 Flights 

Flights 

EFFECTIV ITY: ALL 05-10-10 

Page 21 

AUG 1$/11 
I 

BRITISH AEROSl'MCE 

J41 Aircraft Maintenance Manual 

Table 15 continued ... 

SS I NUMBER 

*53-10 -064 

53-10-065 

53-10-067 

53-10-069 

REFERENCED TASK AND ITEM 

DESCRIPTION 

TASK 53-10-02-210-954 

Surround Pressings at the 

Corners 

TASK 53-10-00-210-923 Frame 

Stn 479- Level with Bottom 

Corner of Rear Emergency 

Ex it 

TASK 53-10-00-210-925 Frame 

Stn 479 - Side of Rear 

Emergency Exit 

TASK 53-10-00-210-927 Frame 

Stn 510 - Level with 

Corners of Rea r Emergency 

Exit 

INITIAL 

INSPECTION 

SUBSEQUENT 

INSPECTIONS 

23000 Flights 23000 Flights 

20000-26000 

Flights 

20000-26000 

F I i ghts 

20000-21500 

F 11 ghts 

6200 F 1 i ghts 

6400 F 1 i ghts 

]100 Flights 

** FOR AIRCRAFT 045-045 055-055 058-059 063-064 080-080 083-083 097-10 1** 

53-10-070 TASK 53-10-05-210-802 Rear 

Emergency Exit Surround 

Abutment Cleats 

** FOR AIRCRAFT ALL** 

53-10-071 TASK 53-10-05-210-805 Frame 

Stn 510 - Side of Rear 

Emergency Exit 

53-10-073 TASK 53-10-00-210-931 

Intercostal Between Frames 

479 and 510 Above Exit 

53-10-075 TASK 53-10-04-210-808 

Intercostal Between Frames 

479 and 510 Below Exit 

53-10-077 TASK 53-10-04-210-809 Frame 

Stn 537- Level With 

Corners of Baggage Bay Door 

Aperture 

*53-10-077A TASK 53-10-02-250-930 Frame 

Stn 537 - Level With Bottom 

Corner of Baggage Bay Door 

Aperture 

EFFECTIVITY : ALL 

43700 Flights 6000 Flights 

30000-40000 

Flights 

30000 F 1 ights 

20000 Flights 6000 Flights 

26000-30000 20200 Flights 

Flights 

26000-30000 16300 Flights 

F 1i ghts 

20000-26000 30000 Flights 

Flights 

05- 10-10 

Page 22 

AUG 15/11 
I'' 

I 

SSI NUMBER 

53-10-079 

53-10-081 

53-10-083 

53-10-085 

53-10-087 

53-I0-087A 

53- 10-089 

53- 10-091 

53-10-093 

53-10-095 

BRITISH AERDSRIICE 

J~l Aircraft Maintenance Manual 

Table 15 continued ... 

REFERENCED TASK AND ITEM 

DESCRIPT ION 

TASK 53-10-00-250-932 Frame 

Stn 537 - Side of Baggage 

Bay Door Aperture 

TASK 53 10-00-210-92~ Frame 

Stn 593- Level With 

Corners of Baggage Bay Door 

Aperture 

TASK 53-10-00-2 10-928 Frame 

Stn 593 - Side of Baggage 

Bay Door Aperture 

TASK 53- 10-02-210-904 

Intercostal Between Frames 

537 and 593 - Top of 

Baggage Bay Door Aperture 

TASK 53-10-04-210-810 

Intercostal, Doub ler and 

Skin Between Frames 537 and 

593 at Bottom of Baggage 

Bay Door Aperture 

TASK 53-10-02-250-938 

Doubler at Intercostal 

Between Frames 537 and 593 

at Bottom of Baggage Bay 

Door Aperture 

TASK 53-10-00-210-943 

Escape Hatch Aper ture- All 

Corners 

TASK 53-10-05- 210-804 

Escape Hatch Aper ture at 

Sides 

TASK 53-10-04-210-811 

Escape Hatch Support 

Structure 

TASK 53-10-00-210-949 

Escape Hatch Support 

Structure 

INITI AL 

INSPECTION 

20000-26000 

Flights 

20000- 26000 

Flights 

20000-26000 

Flights 

20000- 26000 

Flights 

26000-30000 

Flights 

26000-30000 

Fl ights 

20000-24000 

Flights 

30000-40000 

Flights 

26000-30000 

Flights 

20000-26000 

Fli ghts 

EFFECTIVITY : ALL 

SUBSEQU ENT 

INSPECTIONS 

12700 Fl ights 

10600 F 1 ights 

8900 F 1 ights 

16100 F I ights 

23600 fl ights 

23600 Fl ights 

4800 F 1 ights 

16600 Flights 

11700 Flights 

15100 Flights 

05-10- 10 

Page 23 

AUG 15/11 
I 

BRITISH AEROSPJIICE 

J41 Aircraft ~a lntenance ~nual 

Table 15 continued ••. 

SSI NU~BER 

53-10-097 

53-10-098 

REFERENCED TASK AND ITE~ 

DESCRIPTION 

TASK 53-10-00-210-951 Light 

Frame 

TASK 53-10-00-210-851 

lntercostals at Frame 613 

in the Rear Equipment Bay 

*53-10-099 TASK 53-10-00-210-954 Rear 

Pressure Bulkhead - Skin 

Panel 

*53-10-099A TASK 53-10-02-210-955 

Horizontal Stiffeners on 

Forward Face of the Rear 

Pressure Bulkhead 

*53-I0-099B TASK 53-10-02-210-956 Fin 

Post Attachment Angles on 

the Aft Face of t he Rear 

Pressure Bulkhead 

*53-10-099C TASK 53-10-02-210-957 

Diaphragms on the lower 

Central Aft Face of the 

Rear Pressure Bulkhead 

53-I0-099D TASK 53-10-00-210-828 Rear 

Pressure Bulkhead - Outflow 

Valve Cut-out at Stringer 

z91.6 Port 

53-10-101 TASK 53-10-00-210-955 Rear 

Pressure Bulkhead -

Vertical Membe r for Fin 

Attachment 

53- 10- 103 TASK 53-10-04-210-812 Rear 

Pressure Bulkhead -

Attachment to Fuselage Skin 

Above Floor Level 

53-10-l03A TASK 53-10-04-210-813 Rear 

Pressure Bulkhead -

At tachment to fuselage Skin 

Below Floor Level 

EFFECTIVITY: ALL 

INITIAL SUBSEQUENT 

INSPECTION INSPECTIONS 

20000-26000 10100 Flights 

Flights 

31800 Flights 31800 Fl lghts 

20000 flights 6600 f II ghts 

20000 flights 6600 Flights 

20000 F I i ghts 6600 F II ghts 

20000 flights 6600 Flights 

20000-26000 30000 flights 

Flights 

20000-26000 30000 Flights flights 

26000-30000 16600 flights flights 

26000-30000 16600 flights 

flights 

05-10-10 

Page 24 

AUG 15/11 
I 

BRITISH AERD.sFJIICii' 

J41 Aircraft Kaintenance Hanual 

Table 15 continued ... 

SSI NUKBER REFERENCED TASK AND ITEK INITIAL SUBSEQUENT 

DESCRIPTION INSPECTION INSPECTIONS 

*53-10- 104 TASK 53-10-02-210-958 Rear 19700 Flights 4700 F I ights Pressure Bulkhead 

Peripheral Cleats 

53-10-105 TASK 53-10-04-210-814 Frame 26000-30000 30000 Flights 

Stn 655- Attachment to Fin Flights 

Rear Spar 

53-10-107 TASK 53-10-05-210-806 Frame 30000-40000 30000 F I ights 

Stn 655 - General F I ights 

53-10-109 TASK 53-10-00-210-963 20000-26000 6300 Flights 

Typical Stringer Fatigue Flights 

53-10-111 TASK 53-10-05-210-807 30000-40000 30000 Flights 

Typical Keel Member Flights 

53-10-113 TASK 53- 10-05-210-808 Keel 30000-40000 30000 f l ights 

Member at Region of Light Flights 

Frames 

53-10-115 TASK 53-10-00-250-968 Keel 20000-26000 30000 Flights 

Member at Region of Heavy F I ights 

Frames 

Plates and Skin 

NOTE: Information on all SSI numbers preceeded by an asterisk (*)will be 

superseded by information given in service bulletin J41-51-001. 

SSI NUHBER 

53-30-001 

53-30-003 

53-30-005 

53-30-007 

Table 16 

REFERENCED TASK AND ITEM 

DESCRIPTION 

TASK 53-30-00-210-801 Skin 

at Kain Entry Door Corners 

TASK 53-30-00-210-805 Skin 

at Kain Entry Door Sides 

TASK 53-30-00-210-810 Skin 

at Escape Hatch Corners 

TASK 53-30-00-210-815 Skin 

at Escape Hatch Sides 

EFFECTIVITY : All 

INITIAL 

INSPECTION 

20000-20900 

Flights 

20000-26000 

Flights 

20000-21400 

flights 

20000-26000 

flights 

SUBSEQUENT 

INSPECT IONS 

30000 F I ights 

30000 F I ights 

4800 Flights 

16500 Flights 

05-10-10 

Page 25 

AUG 15/11 
BRITISH AEROSAIICE 

J41 Aircra ft "a lntenance "anual 

Table 16 continued •.. 

SSI NU"BER REFERENCED TASK AND ITE" INITI AL SUBSEQUENT 

DESCRIPTION INSPECTION INSPECTIONS 

53-30-008 TASK 53-30-00-2 10-804 Lower 20000-24200 12900 Flights 

Skin Lugs at Escape Hatch Flights 

Surround 

53-30-009 TASK 53-30-00-2 10-820 Skin 20000-22100 30000 F 1 i ghts 

at Emergency Exit Corners Flights 

53-30-011 TASK 53-30-00-210-825 Skin 26000-30000 30000 Fli ghts 

at Emergency Exit Sides Flights 

*53-30-013 TASK 53-30-00-260-801 Skin 20000-26000 16500 Fl ights 

at Baggage Door Corners Fli ghts 

*53-30-015 TASK 53-30-00-260-802 Skin 20000-22000 7400 Flights 

at Baggage Door Sides Flights 

53-30-017 TASK 53-30-00-2 10-840 Skin 20000-26000 9600 f II ghts 

at Windows Flights 

TASK 53-30-00-2 10-807 Skin 20000-25500 6300 Flights 

a t Windows - Pan Flights 

53-30-019 TASK 53-30-00-210-845 20000-26000 6000 fl ights 

Hori zontal Lap Joint Flights 

53-30-021 TASK 53-30-00-210-850 30000-40000 30000 F 1 ights Vertica l Butt Joints Flights 

53-30-023 TASK 53-30-00-210-872 Skin 26000- 30000 30000 f 11 ghts 

at Joint with Front Flights 

Pr essure Bu lkhead 

53-30-025 TASK 53-30-00-2 10-857 Skin 20000-26000 30000 Fl ights 

at Joint with Rear Pressure f 11 ghts 

Bulkhead 

*53-30-037 TASK 53-30-00-210-860 Plain 20000-25000 13600 Flights Area of Skin fli ghts 

53-30-041 TASK 53-30-00-210-869 Holes 30000-40000 30000 Fl ights 

to Accommodate Systems Flights 

Between Front and Rear 

Spars Stn 312 - 331 

Attachment Fitting 

I" 

EFFECTIVITY : AL L 05-10-10 

Page 26 

I AUG 15/1 1 
I 

SSI NU~BER 

BRITISH AEROSFMCE 

J41 Aircraft ~aintenance ~anua l 

Table 16 continued .•• 

REFERENCED TASK AND ITE~ 

DESCRIPTION 

INITIAL 

INSPECTION 

SUBSEQUENT 

INSPECTIONS 

NOTE: Information on all SS I numbers preceeded by an asterisk (*)will be 

superseded by information given i n service bul lotin J41-5l-00l . 

Table 17 

SSI NUKBER REFERENCED TASK AND ITE~ 

DESCRIPTION 

*53-40-001 TASK 53-40-00-250-802 Nose 

Undercarriage - Pintle 

Bracket Bearing Cap Grease 

Ni pple Holes 

*53-40-00IA TASK 53-40-00-210-819 

Pintle Bracket Club Foot 

Fi ttlngs 

53-40-00 IB TASK 53-40-00-250-807 

Pintle Bracket Bearing 

Block at Barrel Nut 

*53-40-00IC TASK 53-40-00-240-801 

Pintle Bracket Tension 

Bolts 

53-40-003 TASK 53-40-00-250-805 Nose 

Undercarriage - Retraction 

Jack Bracket 

*53-40-005 TASK 53-40-00-250-810 Nose 

Undercarriage - Oownlock 

Bracket Fitting lugs 

*53-40-005A TASK 53-40-00-210-820 

Downlock Bracket 

53-40-005B TASK 53-40-00-220-801 

Downlock Bracket Fitting 

Base Bolts 

53-40-007 TASK 53-40-01-210-801 

Attachment Bracket for Wing 

at Stn 312 - Vertical load 

53-40-007A TASK 53-40-01-250-801 

Vertical load Attachment 

Bracket Lugs 

EFFECTIVITY : All 

INITIAL 

INSPECTION 

20000-26000 

Flights 

20000-26000 

Flights 

20000-26000 

F I i ghts 

20000-26000 

Flights 

20000-23600 

Flights 

20000-26000 

F I i gh ts 

20000-26000 

Flights 

20000-26000 

Flights 

30000-40000 

Flights 

30000-40000 

Flights 

SUBSEQUENT 

INSPECTI ONS 

25800 F I ights 

25800 Flights 

25800 F 1 i ghts 

25800 F 1 ights 

15700 Flights 

30000 F 1 i ghts 

30000 Flights 

30000 F 1 i ghts 

30000 F 1 ights 

30000 Flights 

05-10-10 

Page 27 

AUG 15/ II 
BRITISH AEROSP.JIICii' 

J41 Aircraft "aintenance "anual 

Table 17 continued ... 

SSt NU"BER REFERENCED TASK AND ITE" INITIAL SUBSEQUENT 

DESCRIPTION INSPECTION INSPECTIONS 

I 53-40-009 TASK 53-40-01-210-802 30000-40000 30000 Flights 

Attachment Bracket for Wing Flights 

at Stn 312 - lateral load 

I 53-40-011 TASK 53-40-01-210-803 30000-40000 30000 Flights 

Attachment Bracket for Wing Flights 

Drag Load 

I 53-40-013 TASK 53-40-01-210-804 30000-40000 30000 Fl ights 

Attachment Bracket for Wing Flights 

at Stn 366 - Vert ical Load 

I 53-40-015 TASK 53-40-01-210-805 30000-40000 30000 F 1 i ghts 

Attachment Bracket for Wing Flights 

at Stn 366 - lateral load 

I 53- 40-017 TASK 53-40-01-210-806 Links 30000-40000 30000 F 11 g h t s 

at Wing Attachment Stn 312 Flights 

Vertical 

I 53-40-019 TASK 53-40-01-210-807 links 30000-40000 30000 F I i ghts 

at Wing Attachment S tn 312 Flights - latera I 

I 53-40-021 TASK 53-40-0l-210-808 Drag 30000-40000 30000 Flights 

links Flights 

I 53-40-023 TASK 53-40-01-210-809 links 30000-40000 30000 Flights 

at Wing Attachment Stn 366 Flights 

- Vertical 

I 53-40-025 TASK 53-40-01-210-810 Links 30000-40000 30000 F II ghts 

at Wing Attachment Stn 366 Flights 

- lateral 

53-40-027 TASK 53-40-00-250-825 Fin 20000-26000 30000 Flights 

Attachment Brackets at Stn flights 

613 

53-40-029 TASK 53-40-00-250-830 Fin 20000-26000 11200 Flights 

Attachment Bracket Stn 655 F I ights 

53-40-035 TASK 53-40-00-210-835 Pod 26000-30000 21200 Fl ights 

Attachment Brackets Stn flights 

411, 456 and 510 

r·· 

EFFECTIVITY : ALL 05-10-10 

Page 28 

FEB 15/09 
I 

SSI NU"BER 

53-40-037 

BRITISH AEROSAIIC6 

J41 Aircraft "aintenance "anual 

Table 17 continued ... 

REFERENCED TASK AND ITE" 

DESCRIPTION 

TASK 53-40-00-210-836 Pod 

Attachment Support Brackets 

Stn 411, 456 and 510 

IN I Tl Al 

INSPECTION 

26000-30000 

Flights 

C. Chapter 54- Nacelles/Pylons 

Nacelle 

SUBSEQUENT 

INSPECTIONS 

21200 Flights 

NOTE: Information on all SSt numbers preceeded by an asterisk (*) wilt be 

superseded by information given in service bulletin J41-51-00I . 

SSI NU"BER 

54-10-001 

*54-10-003 

54-10-005 

*54-10-007 

54-10-009 

54-10-011 

54-10-013 

54-10-015 

Table 18 

REFERENCED TASK AND ITEM 

DESCRIPTION 

INITIAL 

INSPECTION 

TASK 54-10-01-250-801 Horse 30000-40000 

Collar Flights 

TASK 54-10-00-210-875 

Forward Side Support Rods 

TASK 54-10-00-210-806 

Forward Top Support Rods 

TASK 54-10-00-210-808 

Forward Side Support Rod 

Ends 

20000-24000 

Flights 

20000-26000 

F I ights 

20000-24000 

Flights 

TASK 54-10-00-210-812 20000-26000 

Forward Top Support Rod Flights 

Ends 

TASK 54-10-00-210-814 Horse 20000-26000 

Collar-Eyebolt for Right Flights 

Upper Support Rod 

TASK 54-10-00-210-816 Horse 20000-26000 

Collar-Eyebolt for Upper F 1 ights 

Diagonal Support Rod 

TASK 54-10-00-210-818 Horse 20000-26000 

Collar-Eyebolt For left Flights Upper Support Rod 

EFFECTIVITY: ALL 

SUBSEQUENT 

INSPECTIONS 

30000 f I ights 

I 1000 Flights 

I 1700 Ft ights 

11000 Flights 

11700 F 1 ights 

11700 F I ights 

11700 Flights 

11700 F I ights 

05-10-10 

Page 29 

FEB 15/09 
BRITISH AERDSFMCE 

J41 Aircraft Maintenance Manual 

Tab le 18 continued ... 

SSI NUMBER REFERENCED TASK AND ITEM INITIAl 

DESCRIPTION INSPECTION 

54- 10-017 TASK 54-10-00- 210-822 Horse 20000-26000 

Col tar- lower Fi t ting F I i ghts 

54-10-019 TASK 54-10-00-210-824 26000- 30000 

Fitting on Horse Collar For F I i ghts 

Upper Engine Attachment 

54-10-021 TASK 54-10-00-2 10-826 26000-30000 

Fitt ing on Horse Collar For Flights 

Lower Engine Attachment 

54- 10-025 TASK 54-10-00-210-823 Upper 26000-30000 

Aft Mounting Strut-Ends Flights 

54-10-027 TASK 54-10-00-210-830 Upper 26000-30000 

Aft Mounting Strut Flights 

54-10-029 TASK 54-10-00-210-829 lower 2 6000-30000 

Aft Mounting Strut Flights 

54-10-031 TASK 54-10-00-210-832 lower 2 6000- 30000 

Aft Mounting Strut- Ends Flights 

54-10-033 TASK 54-10-00-210-876 20000-26000 

Firewall Flights 

I 54-I0-033A TASK 54- 10-01-250-802 30000-36000 

Firewall Attachment Fi t ting Fi ights 

Bolt-holes 

54-10-035 TASK 54- 10-00- 210-838 Upper 20000-26000 

Fitti ng on Firewa ll for Fl ights 

Forward and Aft Support 

Rods 

54-10-037 TASK 54-10 -00- 210-877 26000- 30000 

Forward Mid Side Fi tting on F 1i ghts 

F i rewa II 

54-10-039 TASK 54-10-00-210-842 20000-26000 

Firewa ll Fi tting for lower Fl igh ts 

Forward Suppor t Rods 

54-i0-04 1 TASK 54-i0-00-210-844 lug 26000-30000 

on Rear Mounting F I i ghts 

EF FECTIVITY: ALL 

SUBSEQUENT 

INSPECTIONS 

14100 Fl ights 

30000 F I i ghts 

30000 F I i ghts 

21600 Fl ights 

21600 Fl ights 

20700 F I i ghts 

20700 Fli ghts 

30000 F 1 I ghts 

30000 Flights 

5700 F I i ghts 

21600 Fl ights 

14100 Fi ights 

20700 Fl i ghts 

05-10-10 

Page 30 

FEB 15/ 09 
BRITISH AERDS#MCE 

J41 Aircraft Maintenance Manua l 

Table 18 continued ... 

SSI NUMBER REFERENCED TASK AND ITEM INITIAL 

DESCRIPTION INSPECTION 

54-10-043 TASK 54-10-00-210-846 Aft 20000-26000 

Upper Support Rods Flights 

54-10-045 TASK 54-10-00-210-848 Aft 26000-30000 

Cross Support Rods Flights 

54-10-M7 TASK 54-10-00-210-852 Aft 20000-26000 

lower Support Struts Flights 

54-10-049 TASK 54-10-00-210-854 Inner 26000-30000 

and Outer Diaphragms Flights 

54-10-051 TASK 54-10-00-210-873 Aft 20000-26000 

Upper Support Rod-Ends Flights 

54-10-053 TASK 54-10-00-210-858 Aft 26000-30000 

Cross Support Rod-Ends f I igl'lts 

54-10-055 TASK 54-10-00-210-862 Aft 20000-26000 

lower Support Strut-Ends Flights 

54-10-056 TASK 54-10-00-210-864 26000-30000 

Fittings for Forward Ends Flights 

of Cross Support Rods 

54-10-057 TASK 54-10-00-210-827 20000-26000 

Diapl'lragm Top lug Flights 

54-10-059 TASK 54-10-00-210-868 20000-26000 

Diaphragm Center lug flights 

54-I0-061 TASK 54-10-00-210-871 20000-26000 

Diaphragm Aft Lug F I igl'lts 

54-I0-063 TASK 54-10-00-210-872 Joint 26000-30000 

Between Diaphragm and Flights 

F i rewa II 

54-I0-067 TASK 54-10-00-250-866 30000-36000 

Overwheel Shear Panel Flights 

I 54-10-069 TASK 54-10-01-250-804 30000-36000 

Diaphragm to Overwheel Flights 

Shear Panel Joint 

I" EffECTIVITY : All 

SUBSEQUENT 

INSPECTIONS 

3400 Flights 

5600 F II gh ts 

6600 Flights 

30000 F I i ghts 

3400 F I i gl'lts 

5600 Flights 

6600 F I igl'lts 

5600 F I i gh ts 

6600 f I i ghts 

12300 Flights 

7500 f I i gl'lts 

30000 F I i gl'lts 

30000 Flights 

30000 Flights 

05-10-10 

Page 31 

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BRITISH AEROSFMCIE 

J41 Aircraft Maintenance Manual 

D. Chapter 55- Stabilizers 

Horizontal Stabilizers 

SSI NUMBER 

55-10-001 

55-10-003 

55-10-005 

55-10-007 

55-10-009 

55- 10-011 

55-10-013 

55-10-015 

Table 19 

REFERENCED TASK AND ITEM 

DESCRIPTION 

TASK 55-10-01-290-801 Skin 

Joint at Stn 35.5 

TASK 55-10-00-290-812 Skin 

Between Stn 3 and Stn 35.5 

TASK 55-10-00-290-814 Skin 

Between Stn 35-5 and Stn 

103 -5 

TASK 55-10-00-290-818 Skin 

Between Stn 103.5 and 

Tai I plane Tip 

TASK 55-10-01-290-802 Rib 

at Stn 3 (Attachment to 

Fin) 

TASK 55-10-01-290-803 Rib 

at Stn 3 (Attachment to 

Elevator Hinge Bracket) 

TASK 55-10-01-290-804 Rib 

at Stn 67.5 (Attachment to 

Elevator Hinge Bracket) 

TASK 55-10-01-290-805 Rib 

at Stn 122 (Attachment to 

Elevator Hinge Bracket) 

INITIAL 

INSPECTION 

30000-40000 

Flights 

26000- 30000 

Flights 

26000-30000 

F I i ghts 

26000-30000 

Flights 

30000-40000 

Flights 

30000-40000 

flights 

30000-40000 

Flights 

30000-40000 

f l ights 

SUBSEQUENT 

INSPECTIONS 

22900 Flights 

22900 F II ghts 

22900 F I i ghts 

22900 F r r ghts 

30000 Flights 

30000 Fl ights 

30000 Fl ights 

30000 F 11 gh ts 

NOTE: If fatigue damage is found when carrying out SSI's 55-10-0 15 or 

55-50-029 then the following inspection has to be carried out at the 

same maintenance check/input SSI 55-50-031 . 

55-10-017 

55-10-019 

TASK 55-10-01-210-801 Front 

Spar at Stn 3 (Attachment 

to fin) 

TASK 55- 10-01-210-802 Rear 

Spar at Stn 3 {Attachment 

to fin and Elevator Hinge) 

EFFECTIVITY: ALL 

30000-40000 

Flights 

30000-40000 

Flights 

30000 fl ights 

30000 f I ights 

05-10-10 

Page 32 

FEB 15/09 
BRITISH AERDS..JWCJJT J~l Aircraft ~aintenance ~anual 

Table 19 continued ... 

SSI NU~BER REFERENCED TASK AND ITE~ INITIAL SUBSEQUENT 

DESCRIPTION INSPECTION INSPECTIONS 

55-10-021 TASK 55-10-00-250-83~ Front 20000-26000 1200D F I i gh ts 

Spar at Stn 67.5 (Boom f I i ghts 

Joint) 

I 55-10-023 TASK 55-10-01-290-806 Rear 30000-~0000 12000 F I ights 

Spar at Stn 67.5 (Boom flights 

Joint) 

I 55-10-025 TASK 55-10-01-290-807 Rear 30000-~0000 30000 F I i ghts Spar at Stn 67.5 (Elevator F I ights 

Hinge Attachment) 

55-10-027 TASK 55-10-00-290-8~~ Front 26000-30000 12000 F 1 ights 

Spar Between Stn 0 and 67.5 Flights 

55-10-029 TASK 55-10-01-290-808 Rear 30000-~0000 12000 F 1 i ghts 

Spar Between Stn 0 and 67 . 5 Flights 

55-10-031 TASK 55-10-00-210-908 Cut 26000-30000 12000 F If ghts 

Out in Skin at Stn 67.5 F I i ghts 

Elevator 

Table 20 

SSI NU~BER REFERENCED TASK AND ITE~ 1 NIT I Al SUBSEQUENT 

DESCRIPTION INSPECTION INSPECTIONS 

55-20-001 TASK 55-20-00-290-805 30000-~0000 15200 F 1 i ghts Attachment to Hinge Between Flights 

Stn 5.7 and Stn 15.45 

55-20-003 TASK 55-20-00-290-806 30000-40000 30000 F 1 i ghts Structure Between Stn 25 Flights 

and Stn 30 

55-20-00~ TASK 55-20-00-290-807 Inner 30000-~0000 30000 Flights 

Cut Out Flights 

55-20-005 TASK 55-20-00-290-808 Hinge 30000-40000 30000 fl ights 

at Stn 67.5 Flights 

55-20-007 TASK 55-20-00-290-809 30000-40000 30000 F 1i ghts 

Structure Between Stn 67 Flights 

and Stn 74 

r, 

EFFECT IVITY : ALL 05-10-10 

Page 33 

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SSI NU~BER 

55-20-009 

55-20-011 

55-20-012 

BRITISH AEROSFMCir 

J~l Aircraft ~aintenance ~anual 

Table 20 continued ... 

REFERENCED TASK AND IT£~ 

DESCRIPTION 

INITIAL 

INSPECTION 

TASK 55-20-00-290-819 Hinge 30000-40000 

at Stn 122 Flights 

TASK 55-20-00-290-811 

Structure Between Stn 122 

and Stn 123 

TASK 55-20-00-290-8 12 

Structure Other Than Hinge 

Attachments 

30000-40000 

Flights 

30000-40000 

Flights 

Vert ical Stabili zer 

SS I NU~BER 

55-30-001 

55-30-003 

55-30-005 

55-30-007 

55-30-011 

55-30-013 

55-30-015 

Table 21 

REFERENCED TASK AND ITEM 

OESCR I PTI ON 

TASK 55-30-01-290-811 Skin 

Panel Between Stn 29 and 

Stn 50.25 

TASK 55-30-01-290-812 Skin 

Panel Between Stn 62.5 and 

Tip 

TASK 55-30-01-210-809 Skin 

Attachment to Forward 

Attachment Brackets 

TASK 55-30-01-210-810 Skin 

Attachment to Aft 

Attachment Brackets 

TASK 55-30-01-290-813 

Bottom Rib 

TASK 55-30-01-210-8 11 Rib 

at Stn 50.25 (Tal I plane 

Attachment) 

TASK 55-30-01-210-812 Rib 

at Stn 62.5 (Rudder Hinge) 

TASK 55-30-01-210-8 13 Rib 

at Stn 113.5 (Rudder Hinge) 

EFFECTIVITY: ALL 

INITIAL 

INSPECTION 

30000-40000 

F 1 i gh ts 

30000-40000 

Flights 

30000-40000 

Flights 

30000-40000 

F I ights 

30000-40000 

Flights 

30000-40000 

F I I ghts 

30000-~0000 

Flights 

30000-~0000 

F I i ghts 

SUBSEQUENT 

INSPECTIONS 

30000 F I i ghts 

30000 F II ghts 

30000 F 11 ghts 

SUBSEQUENT 

INSPECT IONS 

30000 Flights 

30000 F I i ghts 

30000 flights 

30000 F 1 i ghts 

30000 flights 

30000 f II ghts 

30000 f I ights 

30000 f I i ghts 

05-10-10 

Page 34 

FEB 15/09 
BRITISH AERDSAIICii' 

J41 Aircraft Maintenance Manual 

Table 21 continued ... 

SSI NUMBER REFERENCED TASK AND ITEM INITIAL SUBSEQUENT 

DESCRIPTION INSPECTION INSPECT IONS 

55-30-0 17 TASK 55-30-00-210-810 front 26000-30000 15000 Flights 

Spar at AtLachment to fin Flights 

Attachment Bracket at Stn 

33-5 

I 55-30-018 TASK 55-30-01-290-814 Front 30000-40000 30000 Flights 

Spar at Stn 37 Flights 

55-30-019 TASK 55-30-01-290-815 Rear 30000-40000 30000 Flights 

Spar at Attachment to Fin F I i ghts 

Attachment Brackets at Stn 

26 

I 55-30-02 1 TASK 55-30-01-290-816 Front 30000-40000 30000 F I i ghts 

Spar at Stn 50.25 Flights 

I 55-30-023 TASK 55-30-01-290-817 Rear 30000-40000 30000 Flights 

Spar at Stn 50.25 Flights 

I 55-30-025 TASK 55-30-01-290-818 Front 30000-40000 30000 F I ights 

Spar at Stn 62.5 Flights 

I 55-30-027 TASK 55-30-01-290-819 Rear 30000-40000 30000 Flights 

Spar at Stn 62.5 Flights 

I 55-30-029 TASK 55-30-01-290-820 Rear 30000-40000 30000 Flights 

Spar at Top Rudder Hinge Flights 

I 55-30-031 TASK 55-30-01-290-821 Front 30000-40000 30000 Flights 

Sub Spar at Tailplane Flights 

Attachment 

55-30-033 TASK 55-30-00-290-838 Rea r 26000-30000 30000 F I i ghts 

Sub Spar at Tal I plane Flights 

Attachment 

I 55-30-035 TASK 55-30-01-210-814 30000-40000 30000 Flights 

Attachment Rudder Bottom Flights 

Hinge Fitting 

I 55-30-037 TASK 55-30-0 1-290-822 30000-40000 30000 F I i ghts 

Access Holes in Fin Skin Fli ghts 

(Aft Fin Tailplane 

Attachment) 

Rudder 

I" EFFECTIVITY : All 05-10-10 

Page 35 

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BRI77SH AEROSAIICii' 

J~l Aircraft "a lntenance "anua l 

SSI NU"BER 

55-~0-001 

55-40-003 

55-40-005 

55-~0-00] 

55-~0-009 

Table 22 

REFERENCED TASK AND ITE" 

DESCRIPT ION 

TASK 55-40-00-210-818 

Rudder Structure Attachment 

to Bottom Hinge Fitting 

TASK 55-40-00-210-822 

Attachment Bracket Rudder 

Center Hinge Fitting 

TASK 55-40-00-210-821 

Structure at Center Hinge 

FItting 

TASK 55-40-00-210-819 

Support Bracket Rudder Top 

Hinge Fitting 

TASK 55-40-00-210-820 

Structure at Top Hinge 

Fl ttl ng 

Attachment Fittings 

INI TI AL 

INSPECTION 

30000-40000 

Flights 

30000-33500 

F 1i ghts 

30000-40000 

Flights 

30000-40000 

Flights 

30000-40000 

Flights 

SUBSEQUENT 

INSPECTIONS 

30000 F I i ghts 

30000 F 1 I ghts 

30000 F 1 i ghts 

30000 Flights 

30000 F 1 i ghts 

NOTE: Information on all SSI numbers preceeded by an aster isk (*)will be 

superseded by Information given in service bulletin J41-51-001. 

SS I NU"BER 

55-50-001 

55-50-002 

55-50-003 

55-50-005 

Table 23 

REFERENCED TASK AND ITE" 

DESCRIPTION 

TASK 55-10-01 -2 10-803 

Tallplane/Fin Forward 

Attachments on the 

Ta i 1 plane 

TASK 55-10-01-220-801 

Tallplane Pick-Up Bolts 

TASK 55-10-01-210-804 

Tallplane/Fin Aft 

Attachments on the 

Tall plane 

TASK 55-10-01 - 210-805 

Tal I plane/Fin Forward 

Attachment on the Fin 

EFFECTIVITY: ALL 

IN ITI AL 

INSPECT ION 

SUBSEQUENT 

INSPECTIONS 

30000-40000 30000 Flights Flights 

41900 Flights 13400 Flights 

30000-40000 30000 Flights 

F I I gh ts 

30000-40000 30000 Flights Flights 

05-10-10 

Page 3E'> 

FEB 15/09 
BRITISH AEROS-.CJ!ICE 

J41 Aircraft Maintenance Manual 

Table 23 continued ... 

SSI NUIIBER REFERENCED TASK AND ITEM INITIAL SUBSEQUENT DESCRI PTION INSPECTION INSPECT IONS 

I 55-50-007 TASK 55-10-01-210-806 30000-40000 30000 f I i gh t s 

Tal lplane/fln Aft f I i gh ts 

Attachment on the fin 

55-50-009 TASK 55-30-00-210-815 20000-26000 30000 flights Rudder Torque Tube flights 

55-50-011 TASK 55-30-00-210-816 20000-26000 30000 f I i ghts 

Bottom Rudder Hinge fitting flights 

on Fin 

55-50-013 TASK 55-30-00-210-817 20000-26000 30000 flights 

Center Hinge Fitting on flights 

Rudder 

55-50-014 TASK 55-30-00-210-820 20000-26000 16000 Flights Center Hinge link flights 

55-50-015 TASK 55-30-00-210-812 20000-26000 30000 Flights 

Center Rudder Hinge Fitting Flights 

on fin 

55-50-017 TASK 55-30-00-210-814 Top 20000-26000 30000 f I ights 

Hinge Fitting on Rudder Flights 

55-50-018 TASK 55-30-00-210-808 20000-26000 16000 Flights 

fin/Rudder Top Hinge link Flights 

55-50-019 TASK 55-30-00-210-809 Top 20000-26000 30000 Flights 

Rudder Hinge Fitting on Fin Flights 

55-50-021 TASK 55-10-00-2 10-859 20000-26000 30000 F I ights 

Inboard Hinge Fitting on Fl ights 

Elevator 

55-50-023 TASK 55-10-00-210-861 20000-26000 30000 F I ights 

Inboard Elevator Hinge F I ights 

Fitting on Ta i lplane 

55-50-025 TASK 55-10-00-210-862 20000-26000 30000 Flights 

Center Hinge Fi tting on Fl ights 

El evator 

55-50-027 TASK 55-10-00-210-874 20000-26000 30000 f I i ghts Center Elevator Hinge Flights 

Fitting on Ta l lplane 

I" EFFECTIV ITY: All 05-10-10 

Page 37 

FEB 15/09 
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SSl NU"BER 

55-50-029 

BRITISH AEROSF'JIICIIi' 

J41 Aircraft "alntenance "anual 

Table 23 continued ... 

REFERENCED TASK AND ITE" 

DESCRIPTION 

TASK 55-10-00-210-879 

Outboard Hinge Fitting on 

Elevator 

INITIAL 

INSPECTION 

20000- 26000 

flights 

SUBSEQUENT 

INSPECTIONS 

30000 F II ghts 

NOTE: If fatigue damage is found when carrying out SSI 's 55-10-015 or 

55-50-029 then the following inspection has to be carried out at the 

same maintenance check/input SSI 55-50-031. 

*55-50-031 TASK 55-10-00-210-884 

Outboard Elevator Hinge 

Fitting on Tailplane 

TASK 55-10-00-260-801 

Outboard Elevator Hinge fitting on Tailplane 

E. Chapter 57 - Wings 

Wing "a inframe 

On Condition On Condition 

On Condition On Condition 

NOTE: Information on all SSI numbers preceeded by an asterisk (*)will be 

superseded by informat ion given in service bulletin J41-51-00I. 

Table 24 

SSI NU"BER REFERENCED TASK AND ITE" 

OESCRI PTI ON 

57-10-001 TASK 57-10-00-210-810 

Center Wing Rib (Joint) 

57-10-003 TASK 57-10-05-210-839 

Center Wing Rib (Drag 

Attachment) 

57-10-005 TASK 57-10-00-210-815 Rib 3 

at Wing Attachment Fittings 

57-10-007 TASK 57-10-05-210-840 Rib 3 

at Flap Hinge fitting 

57-10-009 TASK 57-10-05-210-841 Rib 3 

as a Tank End Rib 

57-10-011 TASK 57-10-05-210-842 Rib 6 

at Flap Hinge Fitting 

I" EFFECTIVITY: ALL 

INITI AL 

INSPECTION 

26000-30000 

Flights 

30000-40000 

Fl ights 

20000-26000 

f I i ghts 

30000-40000 

Flights 

30000-40000 

Flights 

30000-40000 

Flights 

SUBSEQUENT 

INSPECTIONS 

30000 f I ights 

30000 F I i ghts 

30000 Flights 

21000 F I ights 

30000 F 1 i ghts 

21000 Flights 

05-10-10 

Page 38 

FEB 15/09 
BRITISH AEROSPJIICE 

J41 Aircraft ~aintenance Kanual 

Table 24 continued ... 

SSI NUMBER REFERENCED TASK AND ITEM INITIAL SUBSEQUENT 

DESCRIPTION INSPECTIOH INSPECTIOHS 

I 57-10-013 TASK 57-10-05-210-843 Rib 7 30000-40000 30000 f I ights 

- forward Landing Gear flights 

Support Fitting 

I 57-10-014 TASK 57-10-05-210-844 Rib 7 30000-40000 30000 f I ights 

- Aft Landing Gear Support flights 

fittings 

I 57-10-015 TASK 57-10-05-210-845 Rib 7 30000-40000 30000 flights 

as a Tank End Rib flights 

I 57-10-017 TASK 57-10-05-210-846 Rib 8 30000-40000 13900 F 1 ights 

- forward Landing Gear flights 

Support Fittings 

I 57-10-018 TASK 57-10-05-210-847 Rib 8 30000-40000 30000 F I i ghts 

- Aft Landing Gear Support Flights 

Fittings 

I 57-10-019 TASK 57-10-05-210-848 Rib 8 30000-40000 30000 flights 

as a Tank End Rib Flights 

I 57-10-021 TASK 57-10-05-210-849 Rib 9 30000-40000 21000 flights 

at flap Hinge fitting flights 

I 57-10-023 TASK 57-10-05-210-850 Rib 30000-40000 21000 flights 

12 at Flap Hinge Fitting flights 

I 57-10-025 TASK 57-10-05-210-851 Rib 30000-40000 30000 flights 

14 at Aileron Hinge Fitting flights 

I 57-10-027 TASK 57-10-00-210-850 Ribs 30000-36000 30000 flights 

16 and 18 at AIleron Hinge Flights 

Fittings 

I 57-I0-027A TASK 57-10-00-250-804 Ribs 20000-26000 30000 Flights 

16 and 18 at Aileron Hinge Flights 

Attachment Fi ttings 

57-10-029 TASK 57-10-00-210-855 Rib 20000-26000 10000 flights 

18 as a Tank End Rib Flights 

I 57-10-031 TASK 57-10-05-210-852 Rib 30000-40000 30000 flights 

20 at AIleron Hinge Fitting flights 

57-10-033 TASK 57-10-00-210-859 Front 26000-30000 18000 F I i ghts 

Spar Joint at Rib 1 Flights 

I" EFFECTIVITY : ALL 05-10-10 

Page 39 

FEB 15/09 
BRITISH AEROSPJIIIC6 

J~l Aircraft "aintenance " anual 

Tab le 24 continued ... 

SSI NUMBER REFERENCED TASK AN D ITEM INITI Al 

DESCRIPTION INSPECTION 

I 57-10- 034 TASK 57-10-05-210-854 Wing 35~00 F I i ghts 

leading Edge Attachment 

Br11ckets 

57-10-035 TASK 57-10-00-280-802 Front 30000-36000 

Spar Outboard of Rib I to Flights 

Rib 8 

57- 10-037 TASK 57-i0-00-280-801 Front 26000-30000 

Sp11r Outboard of Rib 8 to Flights 

Rib 20 

I 57-10-039 TASK 57-10-05-210-853 Front 30000 ~0000 

Spar at Kink Joint Rib 15 Flights 

*57-10-041 TASK 57-10-00-210-925 Rear 20000-26000 

Spar Joint at Rib I Flights 

57- 10-043 TASK 57-10-00-250-875 Rear 20000-26000 

Spar Outboard of Rib 3 and Flights 

Rib 6 

I 57-10 0~4 TASK 57-10-00- 280-803 Rear 30000- 36000 

Spar - General Flights 

I 57-10-0~5 TASK 57-10-00-280-804 Rear 30000-36000 

Spar in Region of Ribs 2, flights 

4, 5 and 7 to Rib 20 

57-10- 050 TASK 57-10-00- 210-885 Rib 7 26000-30000 

- Backup to Forward Upper Flights 

Engine/Nacelle Attachment 

Fitti ng 

57-10-051 TASK 57-10-00-210-886 Rib 7 26000- 30000 

- Backup to Aft Upper Flights 

Engine/Nacelle Attachment 

Fitting 

57-10-052 TASK 57-10-00-210-887 Rib 7 26000-30000 - Backup to Forward lower F I I ghts 

Engine/Nacelle Attachment 

Fitting 

t·' EFFECTIVITY : All 

SUBSEQUENT 

INSPECTIONS 

9000 Flights 

7100 F I ights 

29600 F I i ghts 

18000 F I ights 

8300 Flights 

5000 F I ights 

13400 F I i ghts 

13400 Flights 

30000 Flights 

30000 F I ights 

30000 F I i ghts 

05-10-10 

Page 40 

FEB 15/09 
I" 

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J41 Aircraft Ma intenance Manual 

Table 24 continued ... 

SSI NUMBER REFERENCED TASK AND ITEM INITIAL SUBSEQUENT 

DESCRIPTION INSPECTION INSPECTIONS 

57-10-053 TASK 57-10-00-210-888 Rib 7 26000-30000 30000 F I ights 

- Backup to Art Lower Flights 

Engine/Nacelle Attachment 

Fitting 

57-10-055 TASK 57-10-00-210-890 Rib 8 26000-30000 30000 Flights 

- Backup to forward Upper flights 

Engine/Nacelle Attachment 

fitting 

57-10-056 TASK 57-10-00-210-891 Rib 8 26000-30000 30000 f 1 i ghts 

- Backup to Aft Upper Flights 

Engine/Nacelle Attachment 

fitting 

57-10-057 TASK 57- 10-00-210-892 Rib 8 26000-30000 30000 Flights 

- Backup to forward Lower f lights 

Engine/Nacelle Attachmen t 

fItting 

57-10-058 TASK 57-10-00-210-893 Rib 8 26000-30000 30000 flights 

- Backup to Aft Lower flights 

Engine/Naclle Attachment 

fitting 

Wing Plates and Skins 

NOTE: Information on all SSI numbers preceeded by an asterisk (*)will be 

superseded by information given in service bul letin J41-51-001. 

Table 25 

SSI NUMBER REFERENCED TASK AND ITEM INITIAL SUBSEQUENT 

DESCRI PTION INSPECTION 1 NSPECTI ONS 

57-30-001 TASK 57-30-00-210-805 26000-30000 28200 F 1 ights 

Bottom Joint at Center Wing Flights 

(Rib 1) Joint Plate 

57- 30-003 TASK 57-30-00-210-810 26000-30000 6300 flights 

Bottom Joint at Center Wing flights 

(Rib 1) Stringer 

57-30-005 TASK 57-30-00-260-801 30000-36000 30000 F I i ghts 

Bottom Joint at Center Wing Flights 

(Rib I) Stringer Plate 

EFFECTIVITY : ALL 05-10-10 

Page 41 

FEB 15/07 
I 

SSI NUMBER 

57-30-007 

57- 30-011 

57-30-013 

57- 30-015 

57- 30-017 

57-30-019 

*57-30-021 

*57-30-023 

57-30-025 

BRITISH AEROSF'JIICE 

J41 Aircraft Maintenance Manua l 

Table 25 continued ... 

REFERENCED TASK AND ITEM 

DESCRIPT ION 

TASK 57-30-00- 210-819 

Bottom Joint at Center Wing 

(Rib 1) Skin 

TASK 57-30-00-260-802 

Bottom Joint at Center Wing 

(Rib 1) Joint Plate 

TASK 57-30-00- 210-824 

Stringer/Skin Panel 

Outboa rd of Rib 1 Bottom 

Surface 

TASK 57- 30-00-210-830 

Str inger/Skin Panel at Rib 

7 Bottom Surface 

TASK 57-30-00-210-831 

Stringer/Skin Panel at Rib 

8 - Bottom Surface 

INITIAL 

INSPECT ION 

20000-26000 

Flights 

30000- 36000 

Flights 

26000-30000 

Flights 

30000- 40000 

Flights 

26000-30000 

Flights 

TASK 57-30-00- 210-835 No 5 20000-26000 

Stringer/Skin Panel Just Flights 

Outboard of Rib 11 -Bottom 

Surface 

TASK 57-30-00-210-832 

Stringer/Skin Panel Just 

Outboard of Rib 15 - Bottom 

Surface 

TASK 57- 30-00-210-839 

Access Panel Surrounds 

Between Rib 1 and Rib 2 -

Bottom Surface 

TASK 57-30-00-2 10-847 

Access Panel Surrounds 

Between Rib 3 and Rib 8 -

Bottom Surface 

TASK 57-30-00-210-846 Fuel 

Booster Pump Access Hole 

Surround 

30000-40000 

flights 

20000-26000 

Flights 

20000-26000 

Flights 

26000-30000 

Flights 

EFFECTIVITY: All 

SUBSEQUENT 

INSPECTIONS 

8200 f I ights 

30000 F 1 i ghts 

9400 F I ights 

30000 F I ights 

30000 fl ights 

19400 Flights 

19400 Flights 

9000 Flights 

7900 F I i ghts 

21800 Flights 

05-10- 10 

Page 42 

FEB 15/07 
I 

SSI NUMBER 

*57- 30-027 

*57-30-029 

*57-30-031 

BRITISH AEROSPACE 

J41 Aircraft Maintenance Manual 

Table 25 continued ... 

REFERENCED TASK AND ITEM 

DESCRIPTION 

TASK 57-30-00- 210-838 

Access Panel Surrounds 

Between Rib 8 and Rib II -

Bottom Surface 

TASK 57-30-00-210-837 

Access Panel Surrounds 

Between Rib II and Rib 15-

Bottom Surface 

TASK 57-30-00-2 10-836 

Access Panel Surrounds 

Be tween Rib 15 and Rib 20 -

Bo ttom Surface 

INITIAL 

INSPECTION 

20000-26000 

flights 

20000-26000 

Flights 

20000-26000 

F I i ghts 

SUBSEQUENT 

INSPECTIONS 

7900 flights 

9000 f I i ghts 

9000 f I i ghts 

57-30-033 TASK 57-30-00-210-849 Drain 

Hole Surround Outboard of 

Rib 3 - Bottom Surface 

20000 flights 9900 Flights 

57-30-037 

57-30-039 

57-30-041 

TASK 57- 30-00-210-855 

Stringer/Skin Panel Rib 8 - Top Surface 

TASK 57-30-00-210-856 

Stringer/Skin Panel Just 

Outboard of Rib 11 -Top 

Surface 

TASK 57-30-00-210-857 

Stringer/Skin Panel Just 

Outboard of Rib 15 - Top 

Surface 

TASK 57- 30-00-210-860 

Str inger Fue l Drainage 

Holes Lowe r Surface 

Outboard of Rib 3 

At t achment Fittings 

EFFECTIVITY: All 

30000-40000 

Fl ights 

30000-40000 

fl ights 

30000-40000 

Flights 

30000-40000 

Flights 

30000 F 1 i ghts 

30000 F I i ghts 

30000 Flights 

30000 F I i ghts 

05-10-10 

Page 43 

FEB 15/07 
I 

SSI NUMBER 

57- 40-001 

57-40-003 

57-40-007 

57-40-009 

57-40-011 

57-40-013 

57-40-015 

57-40-016 

57-40-017 

57-40-019 

57-40-021 

57-40-023 

BRITISH AEROSP.ACE 

J41 Aircraft Maintenance Manual 

Table 26 

REFERENCED TASK AND ITEM 

DESCRIPTION 

TASK 57-10-15-290-801 Drag 

Attachment Fitting - Rib 1 

TASK 57-10-15-2 10-803 

Forward Attachment Fitting 

- Rib 3 

TASK 57-10-15-210-808 

Lateral Load Fitt ingFront Spar 

TASK 57-10- 15-210-848 

Lateral Load Fitting - Rear 

Spar- Lugs and Splice 

Plates 

TASK 57-10-15-210-820 Flap 

Hinge Fitting -Rib 3 

TASK 57-10-15-210-821 Flap 

Hinge Fitti ng -Rib 6 

TASK 57-10-15-210-822 

Forward Top Engine Nace lle 

Fitting at Rib 7 

TASK 57-10-15-210-823 Aft 

Top Engine Nacelle Fitting 

at Rib 7 

TASK 57-10-15-210-824 

Forward Bottom Engine 

Nacelle Fitting at Rib 7 

TASK 57-10-15-210-825 Aft 

Bottom Engine Nace lle 

Fitting at Rib 7 

TASK 57-10-15-210-830 

Forward Top Engine Nacelle 

Fitting at Rib 8 

TASK 57-10-15-210-831 Aft 

Top Engine Nacelle Fitting 

at Rib 8 

INITIAL 

INSPECTION 

30000-40000 

Flights 

30000-40000 

Flights 

30000-40000 

Fligh ts 

26000-30000 

Flights 

20000-26000 

F I i gh ts 

20000-26000 

Flights 

30000-40000 

F I ights 

30000-40000 

Flights 

30000-40000 

Flights 

30000-40000 

Flights 

30000-40000 

F I I ghts 

30000-40000 

Flights 

EFFECTIVITY: ALL 

SUBSEQUENT 

INSPECTIONS 

30000 F 1 ights 

30000 F I ights 

30000 F 1 i ghts 

14000 F I i ghts 

30000 F 1 i ghts 

30000 Flights 

30000 F 1 ights 

30000 F I i ghts 

30000 F II ghts 

30000 F II ghts 

30000 F I ights 

30000 F l i gh ts 

05-10-10 

Page 44 

FEB 15/07 
BRITISH AEROSF'JIICIE 

J~l Aircraft "aintenance "anual 

Table 26 continued ... 

SSI NU"BER REFERENCED TASK AND ITEM INITI AL 

DESCRIPTION INSPECTION 

57-~0-025 TASK 57-10-15-210-832 30000-~0000 

Forward Bottom Engine Flights 

Nacelle Fitting at Rib 8 

57-~0-027 TASK 57-10-15-210-833 Aft 30000-~0000 

Bottom Engine Nacelle Flights 

Fitting at Rib 8 

57-~0-029 TASK 57-10-15-210-835 30000-40000 

Engine Na cell e Attachment Flights 

Fitting on Front Spar 

Between Ribs 7 and 8 

57-~0-031 TASK 57-10-15-210-826 Flap 20000-26000 

Hinge Fitting- Rib 9 Flights 

57-40-033 TASK 57-10-15-210-828 Flap 20000-26000 

Hinge Fitting -Rib 12 Flights 

57-40-035 TASK 57-10-15-210-840 20000-26000 

Aileron Hinge Fitting - Rib Flights 

14 

57-~0 037 TASK 57-10-15- 210-842 20000-26000 

AIleron Hinge Fitting - Rib Flights 

16 

57-40-038 TASK 57- 10-15-2 10-844 20000-26000 

Aileron Hinge Fitting - Rib Flights 

18 

57-40-039 TASK 57-10-15-210-846 20000-26000 

Aileron Hinge Fi tting - Rib Flights 

20 

57-40-041 TASK 57-10-05- 210-804 Rib 7 20000-26000 

- Main Land i ng Gear Fitting Flights 

57-40-04 1A TASK 57-10-05-250-801 Ri b 7 30000-36000 

-Main Landing Gear Fitting Flights 

Lugs 

57-40-043 TASK 57- 10-05-210-809 Rib 8 20000-26000 

- Kain Land ing Gear Fi tting Fl ights 

EFFECT IVITY: ALL 

I 

SUBSEQUENT 

INSPECTIONS 

30000 Flights 

30000 Fl ights 

22300 F 1 ights 

12,600 Flights 

30000 F 1 i ghts 

30000 Flights 

30000 Flights 

30000 F 1 ights 

30000 Flights 

30000 Flights 

30000 F I ights 

13900 Fli ghts 

05-10-10 

Page 45 

AUG 15/ll 
I 

SSI NUMB ER 

57-40-043A 

BRITISH AEROSPACE 

J41 Aircraft Maintenance Manual 

Table 26 cont inued ... 

REFERENCED TASK AND ITEM 

DESCRIPTION 

TASK 57-10-05-250-803 Rib 8 

-Main Landing Gear Fitting 

Lugs 

IN ITIAL 

INSPECTION 

30000-36000 

Flights 

Flaps and Ailerons 

SUBSEQUENT 

INSPECTIONS 

30000 F I i ghts 

NOTE: Informat ion on all SSI numbers preceeded by an asterisk (*) will be 

superseded by Information given in service bulletin J41-51-001 . 

SSI NUMBER 

57-50-001 

57-50-002 

57-50-004 

57-50-005 

57-50-006 

57-50-007 

57-50-008 

57-50-009 

57-50-010 

Table 27 

REFERENCED TASK AND ITEM 

DESCRI PT ION 

TASK 57-50-00-290-809 Flap 

Structure 

TASK 57-50-00-210-815 flap 

Hinge Arm at Rib 3 - Arm 

TASK 57-50-00-210-820 Flap 

Hinge Arm at Rib 3 - Lug 

TASK 57-50-00-210-82 1 Flap 

Hinge Arm at Rib 3 -

Actuating Lug 

TASK 57-50-00-210-825 Flap 

Hinge Arm at Rib 6 - Arm 

TASK 57-50-00-210-822 Flap 

Hinge Arm at Rib 6- lug 

TASK 57-50-00-210-823 Flap 

Hinge Arm at Rib 9 - lug 

TASK 57-50-00-210-824 Flap 

Hinge Arm at Rib 9 - Arm 

TASK 57-50-00-210-826 Flap 

Hinge Arm at Rib 12 - lug 

TASK 57-50-00-210-830 Flap 

Hinge Arm at Rib 12 - Arm 

EFFECTIVITY: .ALL 

INIT IAL 

INSPECTION 

30000-40000 

Flights 

30000-40000 

Flights 

20000-26000 

Flights 

20000-26000 

Flights 

26000-28000 

Flights 

20000-26000 

Flights 

20000-26000 

Fl ights 

30000-40000 

Fl ights 

20000-26000 

Flights 

30000-40000 

F I i ghts 

SUBSEQUENT 

INSPECTIONS 

26800 F 1 ights 

16600 F I ights 

30000 Fl ights 

30000 Flights 

11000 Fl ights 

30000 F I ights 

30000 Flights 

22400 Flights 

30000 Flights 

30000 Flights 

05-10-10 

Page 46 

AUG 15/11 
BRITISH AERDSCJIICIE 

J~l Aircraft Maintenance Manual 

Table 27 continued ... 

SSI NUMBER REFERENCED TASK AND ITEM INITIAL 

DESCRIPTION INSPECTION 

*57-50-0 II TASK 57-60-00-260-801 20000-26000 

Aileron Front Spar Lower Flights 

Cap 

57-50-013 TASK 57-60-00-210-809 20000-26000 

Aileron Hinge at Rib I~ Flights 

57-50-015 TASK 57-60-00-210-81~ 20000-26000 

Aileron Hinge at Rib 16 Flights 

57-50-016 TASK 57-60-00-210-819 20000-26000 

Aileron Hinge at Rib 18 Flights 

57-50-017 TASK 57-60-00-210-824 20000-26000 

Aileron Hinge at Rib 20 Flights 

57-50-0 19 TASK 57-60-00- 290-829 Flap 30000-40000 

Hinges at Rib 6 and 9 Fl ights 

Attachment to Ribs 

I 4. Airframe Scheduled Maintenance - Published Repairs 

A. General 

SUBSEQUENT 

INSPECTIONS 

30000 F I i ghts 

30000 F I i ghts 

30000 F I i ghts 

30000 F I ights 

30000 Flights 

30000 F I I ghts 

Published repairs are issued in the Structural Repa ir Manual (SRM) (Ref. 

SA.4-4100/SRM/400). A damage tolerance evaluation of all of the repairs in 

the SRM has been performed, and damage tolerance inspections defined for 

all repairs which affect fatigue critical structure (Ref. 

SA.4-4100/SRM/400, at Revision 31 or later) . 

Pageblock 51-10-02 of the SRM quotes the inspection task description, 

threshold and repeat periods for alI repairs which affect fatigue critica l 

structure . These inspections are additional to the Inspections or the 

airframe detailed in AMM 05-10-10, paragraph 3. These Inspection tasks are 

only applicable if a repa ir is fitted to the aircraft subsequent to 

publication of the AMM at Revision 37 . 

EFFECTIVITY : All 05-10-10 

Page ~7 

JAN 15/13 

** FOR AIRCRAFT All** 

1. Genera l 

A. Approva 1 

BRITISH AERDSPJIICE 

J41 Aircraft "a intenance Manua l 

CERTIFICATION "AINTENANCE REQUIRE"ENTS 

DESCRIPTION AND OPERATION 

This Section Is JAA/FAA Approved. It gives the check procedures and the 

maximum pe rmitted time between checks necessary to maintain the 

certificated airworthiness standard of the airplane as determined in 

accordance with the requirements of JAR/FAR 25.1309. These Items are 

identified as Certification "a intenance Requirements (C"Rs). The Tables in 

paragraph 2 of this Section list the C~s. the maximum permitted time 

interval between each check In number of flight hours and the associated 

check procedure (AMX TASK REF). 

B. Airplane "aintenance Program 

The Airplane "aintenance Program must include all listed CMRs at intervals 

not exceeding the listed times. The maximum permitted time between CMR 

checks may not be increased without consultation with the airplane 

manufacturer and specific approva l from the r esponsible JAA/FAA Aircraft 

Certification Office. 

C. First Flight of the Day Items 

The C"R Tables contain some items that have a FIRST FLIGHT OF THE DAY check 

time. The se i tems are also shown in the Normal Procedures Chapter of the 

Airplane Flight "anual. These items must be included in the Operator's 

Flight Crew Check list. They may not be removed without consultation with 

the airplane manufacturer and specific approval from the responsible 

JAA/FAA Aircraft Certification Office . 

2. C~ Tables 

The CMR Tables are in ATA chapter sequence. Each CMR Is identified as a five 

digit sequence number, for example 21 -001 . The first two numbers identify 

the ATA section and the last three numbers are the CMR sequentia l number in 

that ATA section. 

A. Chapter 21 - Air Conditioning 

C~ NU"BER 

21-001 

EFFECTIV ITY: All 

Table 1 

ITEM DESCRIPTION 

Pressurization System 

Manua 1 Contro 1 -

Opera tiona I Test 

TI"E 

BETWEEN 

CHECKS 

(Fl T HRS) 

600 

CHECK PROCEDURES 

(AMX TASK REF) 

21-30-00-710-810 

05-10-20 

Page 1 

DEC 01/97 
BRITISH AEROSRIICIIT 

J41 Aircraft "aintenance "anual 

Table continued ..• 

C"R NU"BER ITE" DESCRIPTION TI"E CHECK PROCEDURES 

BETWEEN (AM TASK REF) 

CHECKS 

(FLT HRS) 

21-002 Pressurization System 3900 21-30-00-720-830 

Negative Pressure Relief 

"odule - Functional Test 

I 21-003 Environmental Control 10000 21-10-50-720-801 

System fault Control 

Relays - functional Test 

I 21-004 Pressure Regulating and 10000 21-10-15-760-801 

Shut-Off Valve Control 

solenoid - Functional Test 

21-005 Air Conditioning Pack 10000 21-10-25-720-805 

Overpressure SwitchesFunctional Test 

B. Chapter 24 - Electrical Power 

Table 2 

C"R NUMER ITE" DESCRIPTION TI"E CHECK PROCEDURES 

BETWEEN (AM TASK REF) 

CHECKS 

(FLT HRS) 

24-001 DC Generator System 600 24-31 -00-710-810 

Overvoltage ProtectionOperational Test 

24-002 DC Generator Control Unit 16000 24-31-10-000-801 

Acceptance Check - 24-3 1-10-400-805 

Removal/Bay (Ref. CM 24-31-10) Check/Insta ll ation/ 

Operational Test 

24-003 Emergency Busbar Supply 1000 24-32-00-710-805 

Diodes and Remote Control 

Circuit BreakersOperational Test 

24-004 Power Distr ibut ion Unit 25000 24-32-00-710-810 

Overcurrent Sensors -

Operational Test 

I'' EFFECTIVITY: ALL 05-10-20 

Page 2 

FEB 15/10 
I 

CMR NUMBER 

24-005 

24-006 

24-007 

BRITISH AERDSl'C'JIICE 

J41 Aircraft Maintenance Manua l 

Table 2 continued ..• 

ITEM DESCRIPTION 

BUS Tl E Swl teh - Operational Test 

Standby Power Supply Unit 

Capacity- Removal/Bay 

Cheek/Installation/ 

Operational Test 

Standby Power Supply Unit 

Dormancy - Operational 

Test 

TIME 

BETWEEN 

CHECKS 

(FLT HRS) 

10400 

3000 

3000 

C. Chapter 26- Fire Protection 

CIIR NUIIBER 

26-00I 

Table 3 

ITEM DESCRIPTION 

Fire Detection and 

Overheat Control Unit Self 

Test FacilityOperational Test 

TIME 

BETWEEN 

CHECKS 

(FLT HRS) 

FIRST 

FLIGHT OF 

THE DAY 

D. Chapter 27-Flight Controls 

CIIR NUIIBER 

27-001 

27-002 

EFFECTIVITY: ALL 

Table 4 

ITEM DESCRIPTION TillE 

BETWEEN 

CHECKS 

(FLT HRS) 

Elevator Disconnect Unit- 7900 

Functional Test 

Aileron Disconnect Unit- 7534 

Functional Test 

CHECK PROCEDURES 

(AM TASK REf) 

24-32-00-710-815 

24-34-05-000-801 

24-34-05-400-805 

Cllll 24-30-03 

24-34-00-710-805 

CHECK PROCEDURES 

(AII/I TASK REF) 

26-11-00-710-801 

CHECK PROCEDURES 

(AII/I TASK REF) 

27-30-00-720-825 

27-10-00-720-825 

05-10-20 

Page 3 

SEP 15/04 
I 

I 

CMR NU"BER 

27 -003 

27-004 

27-005 

EIR/TISH AEROSFtiiCE 

J41 Aircraft "alntenance Manual 

Table 4 continued ... 

lTE" DESCR IPTION 

Stall Warning and 

Protection-left and Right 

System Self Test - Operational Test 

Stall Warni ng and 

Protection-Angle-ofAttack and 

Aircraft-On-Ground 

Switching- Operational 

Test 

Stall Warning and 

Protection System -

Functional Test 

TIME 

BET\oiEEN 

CHECKS 

(FLT HRS) 

FIRST 

FLIGHT OF 

THE DAY 

300 

3000 

E. Chapter 31 - Indicating/Recording Systems 

CMR NUMBER 

31-001 

31-002 

31 -003 

I" 

EFFECTIVITY: All 

Table 5 

ITEM DESCRIPTION TIME 

BET\oiEEN 

CHECKS 

(FL T HRS) 

Take-Off Conf iguration and 50 

Warning System (TOCWS) 

Arming Circuitry -

Operational Test 

TOCWS-Input Trigger 

Circuitry- Functional 

Test 

landing Gear-Horn Contro l 

Relay and Assoc iated 

Circuitry- Functiona l 

Test (Aircraft on Ground) 

1200 

600 

CHECK PROCEDURES 

(AM TASK REF) 

27-31-00-710-801 

27-31-00-710-801 

27-31-00-720-805 

CHECK PROCEDURES 

(AM TASK REF) 

31-53-00-710-805 

31-53-00-720-810 

32- 61 -00- 720-801 

05-10-20 

Page 4 

OCT 15/99 
BRITISH AEROSMIICI!i' 

J41 Aircraft ~a intenance ~anual 

f. Chapter 52- Doors 

C~R NU~BER 

52-001 

52-002 

Table 6 

ITE~ DESCRIPTION 

~a in Entrance Door Speed 

Lock Check - Functional 

Test 

~ain Entrance 

Door-Pressurization 

Inhibit FunctionOperational Test 

Tl ~E 

BET\o/EEN 

CHECKS 

(FLT HRS) 

2706 

3000 

CHECK PROCEDURES A~~ TASK REF) 

S2-10-0S-720-8os 

52-10-05-710-801 

G. Chapter 73 - Engine Fuel and Control/Chapter 76 - Engine Control 

CIIR NU~BER 

73-001 

73-002 

I'' EFFECTIVITY: ALL 

Tab le 7 

ITE ~ DESCRIPTION TI~E 

BETWEEN 

CHECKS 

(FLT HRS) 

Flight Idle Baulk Solenoid 300 ~echanism - Operational 

Test 

Overspeed fuel Governor - 300 

Operational Test 

CHECK PROCEDURES 

(AM TASK REF) 

76-i2-15-710-801 

72-00-00-501 

Garrett On-Wing 

Manual 

05-10-20 

Page S 

DEC 01/97 

BRITISH AERDSFMCE 

J41 Airc r aft Maintenance Manual 

** FOR AIRCRAFT ALL** 

CRIT ICAL DESIGN CONFIGURATION CONTROL LI MITAT IONS (COCCl) - FUEl SYSTEM 

DESCRIPTION AND OPERAT ION 

1. Genera l 

The Cr itica l Design Configurat ion Control Limitations (CDCCLs) section 

identifies certain design configuration features, which must be maintained 

for the operational l ife of the aircraft in order to prec lude the development 

of ign i tion sources in the fuel tank system. CDCCls are mandatory and cannot 

be changed or deleted wi thout t he approva l of the European Aviation Safety 

Agency (EASA) or the National Regu latory Authority office that is responsib le 

for the Jetstream 41 Type Cert if icate. 

A crit ical fuel tank ignition source prevention feature may exist in the fuel 

system and its related installation or in s ystems that , if a failure 

condit ion were to develop, could interact wi th the fuel system in such a way 

that an unsafe condition would develop wi thout these limitations. Strict 

adherence to conf iguration, methods, techn iques and practices as prescr ibed 

is required to ensure compl iance wi t h the COCCl . Any use of parts, methods, 

techn iques or practices not conta ined in the applicable COCCL requires 

regulatory authority approval. 

The purpose of the COCCL is to prov ide instructions to retain a critical 

ignition source prevention feature during configuration change that may be 

caused by modification, repairs or maintenance act ions. 

2. The following are COCCLs: 

A. Fuel Quantity Indication System (FQIS) 

( 1) Cr i tical ignition source prevention feature: 

The fuel quantity ind ication system (FQIS) probes are current-carrying 

components. They must be installed with a minimum clearance from 

a ircraft structure. 

(2) lmpl ications of changing this feature: 

If the probes are not installed correctly, small air gaps may be 

created between the conductors and the wing s kins. During fault 

conditions, abnormally high voltages may be applied to the FQIS wiring 

and probes and electrical sparking (arc ing) may occur across this small 

air gap. 

(3) Instructions for retaining this feature: 

The proper installation of an FQIS probe to obtain the correct 

clearance is a COCCL. This must be carried out in accordance with AMM 

28-41-0$. 

EFFECTIVITY: All 05-10- 30 

Page 1 

FEB 15/08 
BRITISH AEHDSFJIICE 

J~l Aircraft Maintenance Manual 

B. Fuel Tank Wiring 

(1) Critical ignition source prevention feature: 

The electrical wiring inside the fuel tanks is designed to be 

continuous between the respective tank wall connectors and the affected 

components. Splicing of wires inside fuel tanks is not permitted . 

(2) lmpl ications of changing this feature: 

Repair of damaged wiring using splices creates joints in the wiring. 

Fa il ure of these joints could lead to electrical sparking (arcing) 

inside the fuel tank. Damaged tank wiring should be corrected by 

complete replacement of the affected wire. 

(3) Instructions for retaining this feature: 

Wiring inside fuel tanks must remain continuous between the tank wall 

connectors and the LRUs, with no extra joints permitted. This feature 

is a COCCL. Wire replacement inside fuel tanks should be carried out 

in accordance with AMM Ch 20. 

C. Fuel Boost Pump Wi r ing 

(1) Critical ignition source prevention feature: 

The boost pump power wiring inside the fue l tank is designed to be 

continuous between the tank wall connectors and the boost pump. Repair 

of this wiring harness is not permitted. 

(2) Implications of changing this feature: 

Repair of a damaged boost pump wiring harness using splices creates 

joints in the wiring. Fai lure of these joints could lead to electrical 

sparking (a rc ing) inside the fuel tank. Damaged boost pump wiring 

should be corrected by complete replacement of the affected harness. 

(3) Instructions for retaining t h is feature: 

The boost pump wiring should not be modified in any way. The type 

design specified by Modification JM41672 must be mainta ined, and is a 

CDCCL. Harness replacement should be carried out in accordance with 

AMM Ch 20. 

EFFECTIVITY: ALL 05-10-30 

Page 2 

FEB 15/08