Fokker 50/60 Amm 0050 Printed on: Dec 16/09 02:57
Cust: PT Indonesia Air Transport Issue Date: Aug 01/07
TASK 00-00-00-XX2-810-A - Manual Arrangement
EFFECTIVITY: 001999
1. Procedure
A. General
The manual is organized into:
• Front matter for the complete manual
• Chapters with their own front matter and technical content
• Transmittal letter and Highlights of revision.
(Refer to Fig. 00-00-00-990-010-A00)
(Refer to Fig. 00-00-00-990-020-A00)
(Refer to Fig. 00-00-00-990-030-A00)
(Refer to Fig. 00-00-00-990-040-A00)
B. Breakdown of the manual
(1) The front matter for the complete manual contains
(Refer to Fig. 00-00-00-990-010-A00)
:
(a) Title page
The Title page shows the manual title, aircraft type and model, name of operator or owner of the aircraft and the initial
issue date.
(b) Effectivity Cross Reference Index
The Effectivity Cross Reference Index provides the customer with information that relates aircraft registration, aircraft
serial number, airline id. no., name of the aircraft and effectivity code.
(c) Record of Revisions
The Record of Revisions lists the successive revision numbers, issue dates, insertion dates and incorporator's initials,
which must be kept current by the operator. For microfilm copies the list will be updated by Fokker.
(d) List of Effective Pages (LEP) Summary
The LEP Summary lists all chapter LEP's with the latest issue dates.
(e) LEP Front Matter
The LEP Front Matter lists all effective front matter pages of the manual and their latest issue dates.
(f) Table of Contents (TOC) Front Matter
The TOC Front Matter lists all front matter subjects.
(g) Modification List
(Refer to Fig. 00-00-00-990-040-A00)
The Modification List contains a list of Fokker-issued Service Bulletins (SB), vendor SB's and Customer Originated
Changes (COC), which have been reviewed for their effect on the AMM. When a SB or COC affects the content of the
AMM and the content of the AMM has been changed in accordance with the SB or COC, the list gives the date at which
this change has been incorporated in the AMM. If a SB does not affect the contents of the manual, the words NO
EFFECT are used in the column DATE OF INCORP.
(2) Maintenance Chapters
(a) Front Matter for the Chapters
(Refer to Fig. 00-00-00-990-020-A00)
1 Record of Temporary Revisions (ROTR)
The ROTR lists the successive revision numbers, issue dates, insertion dates, removal dates, and incorporator's
and remover's initials, which must be kept current by the operator.
For microfilm copies the list will be updated by Fokker to include Temporary Revisions issued up to the date of
the revision. Users of microfilm should check their microfilm supplement for any TR's issued subsequent to that
date.
2 List of Effective Pages (LEP)
The LEP lists all effective pages and their latest issue dates.
3 Table of Contents (TOC)
The TOC identifies and locates all the material in the chapter according to the ATA-100 sequence. It provides the
effectivity of all tasks. The task effectivity is placed in a effectivity column. If the effectivity column for a particular
task remains blank, this task is applicable to all aircraft given in the Effectivity Cross Reference Index.
(3) The transmittal letter advises the operator on pages to be removed, replaced or added by a revision. The highlights identify the
affected pages per chapter in a consecutive order and give the reason for each change. Each revision package contain a
transmittal letter and highlights.
(Refer to Fig. 00-00-00-990-030-A00)
C. Numbering System
(1) The ATA-100 system divides the primary system or function of the aircraft into groups of chapters:
•
Introduction - chapter 0
•
Aircraft general - chapters 5 - 12
•
Airframe systems - chapters 20 - 49
•
Structure - chapters 51 - 57
•
Propeller - chapter 61
Page 1 of 12
Fokker 50/60 Amm 0050 Printed on: Dec 16/09 02:57
Cust: PT Indonesia Air Transport Issue Date: Aug 01/07
TASK 00-00-00-XX2-810-A - Manual Arrangement
EFFECTIVITY: 001999
•
Power plant - chapters 70 - 80
•
Miscellaneous - chapters 90 - 99
(2) The ATA-100 Chapter/Section/Subject number is a six-digit number, composed of three elements of two digits (YY-YY-YY),
representing the chapter, section and subject numbers respectively.
The first two digits give the chapter number, which is assigned by ATA-100. This represents the system. The third digit, also
assigned by ATA-100, gives the sub-system number. The fourth digit, assigned by the aircraft manufacturer, represents the
sub-subsystem if applicable.
The fifth and the sixth digits represent the subject/component number. They are assigned by the aircraft manufacturer and run
consecutively from 01 to 99 as required.
Examples:
28-00-00 System : Fuel
28-10-00 Sub-system : Fuel-Storage
28-13-00 Sub-subsystem : Fuel-Storage-Center Wing Tank (CWT)
28-13-01 Component : Fuel-Storage-CWT-Drain Valve
(3) Systems, sub-systems, sub-subsystems and components can be broken down into page blocks. These page blocks are
assigned by ATA-100:
Page block Page numbers
Description and Operation 001 to 099
Fault Isolation 101 to 199
Maintenance Practices 201 to 299
Servicing 301 to 399
Removal/Installation 401 to 499
Adjustment/Test 501 to 599
Inspection/Check 601 to 699
Cleaning/Painting 701 to 799
Repairs 801 to 899
Within a page block, each maintenance procedure will be a task and will have a page numbering in its own right. In a Removal/
Installation page block for example, both the removal task and the installation task will start with page 401. Each task will start
on a right hand page.
(4) Other text items which have been allocated task numbers are:
• The paragraphs of the Introduction.
• The Description and Operation paragraphs; General, Component Information, and Operation and Control.
(5) The task numbers have the following format:
ELEMENT | 1 | 2 | 3 | 4 | 5 | 6
| CH | SE | SU | FFF | YYP | C
The description of each element is given below:
ELEMENT | FUNCTION
1 |ATA-100 chapter.
2 |ATA-100 section.
3 |ATA-100 subject.
4 |A three-digit number indicating the function code
|(Refer to TASK 00-00-00-XX5-810-A).
Page 2 of 12
Fokker 50/60 Amm 0050 Printed on: Dec 16/09 02:57
Cust: PT Indonesia Air Transport Issue Date: Aug 01/07
TASK 00-00-00-XX2-810-A - Manual Arrangement
EFFECTIVITY: 001999
ELEMENT | FUNCTION
5 |A three-digit number, of which the first two digits (YY) give
|the sequence number of the task with the same function code,
|within the pageblock. The last digit (P), gives the page block
|number of which the task is part of.
|There can be more than one task with the same function in a
|pageblock. In this case, the sequence number (YY) is raised by
|one for every consecutive task with the same function code.
|The sequence starts at 81 and can go up to 99. For example, a
|task with sequence number 825 is the second task with a specific
|function code, in a 501 (AJUSTMENT/TEST) pageblock.
6 |The configuration identifier of the task. In the All-Operator
|AMM for example, the task for the PW125B engine is given in the
|A configuration task, while the task for the PW127B engine is
|given in the B configuration task. A customized AMM will only
|show the task configuration applicable for the customer.
(6) Sorting of tasks in the AMM
(a) Tasks are first sorted by ATA-100 Chapter-Section-Subject (elements 1, 2 and 3 of task number, see tables above).
(b) Within the ATA-100 Subject, the tasks are sorted by pageblock (P in element 5 of task number, see tables above).
(c) Within the pageblock, the tasks are sorted by function code (element 4 of task number, see tables above).
(d) Tasks with the same function code are sorted in sequence by YY in element 5, see tables above.
(Refer to Fig. 00-00-00-990-050-A00)
D. Maintenance task arrangement
(1) The maintenance tasks (procedures in the page blocks 201 thru 801) have the following breakdown:
• Subject title (1)
• Page block title (2)
• Task number (3)
• Task title (4)
• Materials (5)
• Special Tools and Equipment (6)
• Standard Tools and Equipment (7)
• Consumable Materials (8)
• Expendable Parts (9)
• Referenced Procedures (10)
• Procedure (11)
• Paragraphs (12)
• Steps (13)
• Illustrations, when applicable, at the end of the task
(2) Footer information
The elements printed in the footer are:
• Effectivity block (14)
• Customer code (15)
• ATA-100 Chapter-Section-Subject (16), which also shows the first three elements of the task number
• Task function, sequence number, and configuration letter (17). The task function is directly related to the function code of
the task number and the configuration letter is directly related to the configuration letter of the task number. The sequence
number gives the sequence of the tasks with the same function code in the page block
• The last three elements of the task number (18)
• The page number of the task (19)
• The revision date of the task (20)
(Refer to Fig. 00-00-00-990-060-A00)
Page 3 of 12
Fokker 50/60 Amm 0050 Printed on: Dec 16/09 02:57
Cust: PT Indonesia Air Transport Issue Date: Aug 01/07
TASK 00-00-00-XX2-810-A - Manual Arrangement
EFFECTIVITY: 001999
E. Description and Operation arrangement
Description and Operation page blocks have the following breakdown:
• General (identified by function code XX1)
• Component Information (identified by function code XX2)
• Operation and Control (identified by function code XX3)
F. Technical Contents
(1) Maintenance Practices page blocks
(a) The maintenance practices page blocks contain (scheduled) tasks, servicing, removal/installation, adjustment/test,
inspection/check, cleaning/painting and repair tasks.
(b) Deactivation and reactivation tasks are provided at system level.
(2) Scheduled Tasks
(a) The Maintenance Planning Document (MPD) lists all the scheduled tasks. When these tasks require a maintenance
procedure, the MPD gives a reference to the applicable Chapter-Section-Subject in the AMM.
In reverse, the AMM gives the reference to the MPD task-number:
• In front of the AMM procedure (following the procedure title) between brackets
• In the Table Of Contents (TOC) (following the procedure title) between brackets.
(b) For scheduled MPD tasks which require off-aircraft maintenance, the removal and installation procedures of the
applicable components are given with reference to the MPD task-number.
(3) Servicing
The servicing page blocks contain tasks for preserving, depreserving, lubricating, fueling, defueling, de-icing, anti-icing,
disinfecting and sanitizing.
(4) Removal/Installation
(a) The removal tasks provide the removal instructions and if necessary, removal of a component for access purposes,
either by a reference to the appropriate removal page block or the required directions for the removal.
(b) The removal tasks include steps for the preparation of replacement of components and preparation for installation.
(c) The installation tasks include the installation procedure, simplified test and adjustment which must be accomplished
during the installation procedure.
(d) The installation tasks include tests required after the installation.
(5) Adjustment/Test
(a) There are three levels of test procedures given in this manual:
• Operational Tests
• Functional Tests
• System Tests.
1 An Operational Test makes sure that a system or component operates properly. No special equipment is
required.
2 A Functional Test makes sure that a system or component is operating within the minimum design specifications.
Values and tolerances are specified and special equipment may be required.
3 A System Test is a complete system check-out comparable to the test and adjustment requirements when the
system or component was initially installed in the aircraft. The test may require special test equipment,
particularly when values and tolerances are specified. This type of test is usually done at major maintenance
intervals.
(6) Inspection/Check
(a) The inspection/check page block contains the procedures necessary to inspect/check a system, component or area.
(b) The inspection/check defines the rejection criteria for the relevant equipment.
(7) Cleaning/Painting
(a) The cleaning/painting page block contains the methods and processes required for cleaning and/or painting specific
parts or areas.
(b) Only the different or unique aspects of the cleaning or painting for the applicable location are provided. For general
procedures applicable for the complete aircraft refer to chapters 12, 25 (cleaning of interior/exterior) and chapter 51
(painting).
(8) Approved Repairs
(a) The approved repairs page block contains procedures and techniques required to restore a worn or damaged part to a
serviceable condition (not included are structural repairs for which reference is made to the Structural Repair Manual).
(b) The procedures include repairs of vendor components that can be repaired without removal from the aircraft and for
repairs that can be performed during maintenance.
(c) Temporary allowable damage or temporary repairs are also provided.
(9) Description and Operation
(a) The Description and Operation page blocks give an explanation of the system by function, operation, configuration and
control.
(b) The Description and Operation page blocks cover the following levels: system, subsystem and sub-subsystem. Each
level of description is supportive of the level above it, and leads the reader through a system in a logical and functional
manner.
G. Effectivity and Configuration
Effectivity and Configuration Identification of tasks is given in the effectivity block at the lower LH margin of each page. When the task
applies to all aircraft of the fleet, the word ALL is shown in the effectivity block. If the information does not apply to all aircraft, only
those aircraft are shown to which the information applies.
The effectivity cross-reference index in the front of the manual shows the relationship between the effectivity number, aircraft serial
number and aircraft registration.
Page 4 of 12
Fokker 50/60 Amm 0050 Printed on: Dec 16/09 02:57
Cust: PT Indonesia Air Transport Issue Date: Aug 01/07
TASK 00-00-00-XX2-810-A - Manual Arrangement
EFFECTIVITY: 001999
The aircraft serial number is the permanent identification number for the aircraft. This number appears on the identification plate and
on the aircraft registration and airworthiness certificate. The registration number is the number or letter combination on the tail as
required by government regulations.
Configuration differences can be shown on paragraph level or task level. When the configuration difference is minor, paragraph
variants are given. When the configuration difference is major, task variants are given.
(Refer to Fig. 00-00-00-990-070-A00)
H. Service Bulletins (SB)
Fokker issued SB's and vendor component SB's are given in pre SB and post SB text variants. For mandatory SB's the applicable text
variants are always preceded by "PRE SB" and "POST SB" indications. Optional SB's only show these indications on customer
request.
When the SB has been built in on the aircraft, only the post SB text variant will be printed, without the "POST SB" indication, on
customer request.
Effectivity indentification (Refer to item numbers on example page):
(1) Aircraft which are not applicable to the SB. The text configuration for these aircraft is the same as for the aircraft in the pre SB
configuration.
(2) Aircraft which are applicable to the SB, and are in the phase of modification. The following text paragraph is only applicable for
when the aircraft are in the pre SB configuration.
(3) Aircraft which have been modified in accordance with the SB, or have had the modification factory incorporated. The text
configuration for these aircraft is the same as for the aircraft in the post SB configuration.
(4) Aircraft which are applicable to the SB, and are in the phase of modification. The following text paragraph is only applicable for
when the aircraft are in the post SB configuration.
J. Customer Originated Change (COC)
The COC will replace the original FOKKER data.
The COC starts with this sentence :
START OF ------------------------ CUSTOMER ORIGINATED PARAGRAPH
and will end with this sentence:
END OF -------------------------- CUSTOMER ORIGINATED PARAGRAPH
When the complete task is a COC, this task will be preceded by this sentence:
START OF ------------------------------ CUSTOMER ORIGINATED TASK
Page 5 of 12
Fokker 50/60 Amm 0050 Printed on: Dec 16/09 02:57
Cust: PT Indonesia Air Transport Issue Date: Aug 01/07
TASK 00-00-00-XX2-810-A - Manual Arrangement
EFFECTIVITY: 001999
Front Matter Breakdown
Figure 00-00-00-990-010-A00
Page 6 of 12
Fokker 50/60 Amm 0050 Printed on: Dec 16/09 02:57
Cust: PT Indonesia Air Transport Issue Date: Aug 01/07
TASK 00-00-00-XX2-810-A - Manual Arrangement
EFFECTIVITY: 001999
Front Matter - Maintenance Chapter
Figure 00-00-00-990-020-A00
Page 7 of 12
Fokker 50/60 Amm 0050 Printed on: Dec 16/09 02:57
Cust: PT Indonesia Air Transport Issue Date: Aug 01/07
TASK 00-00-00-XX2-810-A - Manual Arrangement
EFFECTIVITY: 001999
Transmittel Letter and Highlights of revision
Figure 00-00-00-990-030-A00
Page 8 of 12
Fokker 50/60 Amm 0050 Printed on: Dec 16/09 02:57
Cust: PT Indonesia Air Transport Issue Date: Aug 01/07
TASK 00-00-00-XX2-810-A - Manual Arrangement
EFFECTIVITY: 001999
Modification List
Figure 00-00-00-990-040-A00
Page 9 of 12
Fokker 50/60 Amm 0050 Printed on: Dec 16/09 02:57
Cust: PT Indonesia Air Transport Issue Date: Aug 01/07
TASK 00-00-00-XX2-810-A - Manual Arrangement
EFFECTIVITY: 001999
Maintenance-Task Arrangement
Figure 00-00-00-990-050-A00
Page 10 of 12
Fokker 50/60 Amm 0050 Printed on: Dec 16/09 02:57
Cust: PT Indonesia Air Transport Issue Date: Aug 01/07
TASK 00-00-00-XX2-810-A - Manual Arrangement
EFFECTIVITY: 001999
Description and Operation Arrangement
Figure 00-00-00-990-060-A00
Page 11 of 12
Fokker 50/60 Amm 0050 Printed on: Dec 16/09 02:57
Cust: PT Indonesia Air Transport Issue Date: Aug 01/07
TASK 00-00-00-XX2-810-A - Manual Arrangement
EFFECTIVITY: 001999
Service Bulletins
Figure 00-00-00-990-070-A00
Page 12 of 12
