2107

Question 1

The purpose of this subheading is
function, operation, and control of the componen on a matine such that the data can also be directly used as a manual for traming purposes for the component use in its normal operational setting.

Answer 1

Description and Operation

Question 2

is initiated by a logbook entry from the flight crew or maintenance crew.

Answer 2

Troubleshooting function

Question 3

SRM 7 Chapters

Answer 3

Chapter 51 – Structure–General
Chapter 52 – Doors
Chapter 53 – Fuselage
Chapter 54 – Nacelle/Pylons
Chapter 55 – Stabilizers
Chapter 56 – Windows
Chapter 57 – Wings

Question 4

This category of allowable damage is established in such a way that damage within this limit must be permanently repaired within a defined operating limit, i.e.: ‘x’ flight cycles or ‘x’ flight hours or ‘x’ flight calendar months

Answer 4

Temporary allowable Damage
Repair Category C

Question 5

CMS

Answer 5

Component Maintenance Sheet

Question 6

AEB

Answer 6

Airline Engineering Bulletin

Question 7

ACM

Answer 7

Abbreviated Component Maintenance Manual

Question 8

When a missing part introduces additional limitations, this limitations is included in the

Answer 8

Remarks and/or Exceptional Column

Question 9

Flight with certain secondary airframe parts missing is possible as indicated in the ___. Any part not included in this list, must be considered as necessary

Answer 9

Configuration Deviation List

Question 10

Category of MEL

Answer 10

Category A - for monitoring
Caregory B - 3 days
Category C - 10 days
Category D - 120 days

Question 11

serves as an entry point into the TSM using Fault Symptoms, Warnings/Malfunctions, or CFDS Fault Message, depending on the type of fault. The troubleshooter is directed to the procedure to isolate the fault.

Answer 11

Logbook entry

Question 12

is initiated by a logbook entry from the flight crew or maintenance crew.

Answer 12

Troubleshooting function

Question 13

are used by maintenance crews. They can be displayed alone without an associated warning or malfunction, in which case they may be the entry point for maintenance-related troubleshooting.

Answer 13

CFDS Fault Message

Question 14

is fault via text or keywords and ATA chapters.

Answer 14

TSM Entry

Question 15

are usually a single fault without an associated CFDS fault message.

Answer 15

Crew or Maintenance Observation

Question 16

Non-Monitored Faults

Answer 16

Crew or Maintenance Observations

Question 17

Monitored Faults

Answer 17

ECAM warnings, EFIS flags, CFDS

Question 18

Types of Faults

Answer 18

Monitored and Non-Monitored Faults

Question 19

It is used to provide coverage of all probable aircraft faults. This includes being a trouble shooting guide to faults monitored and displayed by the aircraft system. Faults not monitored by the aircraft are also covered

Answer 19

Troubleshooting Manual

Question 20

Is provided by Airbus Industry to enable the systematic identification, isolation and correction of aircraft warnings and malfunction reported in flight and in ground

Answer 20

Troubleshooting Manual

Question 21

Manuals usage

Answer 21

1. Determine Damage Classification
2. Identify Damaged Parts in the Manual
3. Determine Repair Procedures

Question 22

In the event of major structural damage the required replacement part can be ordered by means of the Spare Parts Identification

Answer 22

Determine Repair Procedures

Question 23

On the identification page for the part concerned refer to the action or repair” column and determine whether the part has a reference to a repair within the manual, either in the chapter concerned or in an other chapter

Answer 23

Determine Repair Procedures

Question 24

Locate the relevant figure, identify the damaged component and refer to the relevant identification page

Answer 24

Identify damaged parts in the manual

Question 25

Refer to the figure reference at section, subsection level.

Answer 25

Identify damaged parts in the manul

Question 26

Locate the section and subsection which refers to the damaged part in the table of contents

Answer 26

Identify damaged parts in the manual

Question 27

Refer to topic "allowable damage" in the relevant chapter

Answer 27

Determine Damage Classification

Question 28

Locate the section, which refers to the damaged part in the table of contents

Answer 28

Determine Damage Classification

Question 29

Minor damage which does not effect the structural integrity

Answer 29

Allowable damage

Question 30

Locate the chapter which refers to the damaged part using the manual chapter index

Answer 30

Determine Damage Classification

Question 31

Provide data for signiticant damage to the condition required to fulfill its design function.

Answer 31

Structural Repair Manual

Question 32

Serve as medium for advising developed by the manufacturers or by operators

Answer 32

Structural Repair Manual

Question 33

Define both damage that has no significant effect on the strength or life of the structure

Answer 33

Structural Repair Manual

Question 34

Contain descriptive information for aircraft's primary and secondary structure.

Answer 34

Structural Repair Manual

Question 35

Contains preparation for transportation, special handling, packaging, storage and preservation requirements associated with the component after assembly or test.

Answer 35

Storage including transportation

Question 36

Contain a listing of all tools, fixtures, competen, and consumable items necessary for maintenance actions given in the CMM.

Answer 36

Special tools, fixtures, equipment, and consumable

Question 37

Provides all fits and clearances and torque values used ip assembly, including, permissible In service wear and manufacturers design wear tolerances

Answer 37

Fits and clearance

Question 38

Provides step by step assembly instructions in a logical sequence, referencing figure item numbers from IPL illustration's where applicable

Answer 38

Assembly

Question 39

Contains detailed repair procedures and specifications necessary for restoring a component to serviceable condition.

Answer 39

Repair

Question 40

Specifies methods and processes, or refer to applicable standard practices, required for cleaning specific parts or areas of the component

Answer 40

Cleaning

Question 41

This section contains instructions tor a complete disassembly of the component which do not require opening permanent joints or unsoldering connections.

Answer 41

Disassembly

Question 42

The purpose of this subheading is function, operation, and control of the componen on a matine such that the data can also be directly used as a manual for traming purposes for the component use in its normal operational setting.

Answer 42

Description and operation

Question 43

are intended for work on the applicable components in a workshop environment.

Answer 43

Component Maintenance Manual

Question 44

Disassembly, test and assembly procedures detailed within the manual shall be verified by the actual performance

Answer 44

Component Maintenance Manual

Question 45

OD

Answer 45

Outside Diameter

Question 46

ID

Answer 46

Inside Diameter

Question 47

ATLAS

Answer 47

Abbreviated Test Language for All Systems

Question 48

ATA

Answer 48

Air Transport Association of America

Question 49

FIN

Answer 49

Functional Item Number

Question 50

Allowable Damage

Answer 50

Content of SRM

Question 51

This category of allowable damage is established in such a way that damage within this limit does not require a structural repair or additional inspections during the design service goal or the extended service goal as applicable of the aircraft.

Answer 51

Permanent Allowable Damage Repair Category A

Question 52

Contains only those items of airworthiness significance which may be inoperative prior to dispatch, provided limitations and appropriate procedures are observed

Answer 52

Minimum Equipment List

Question 53

Presents the detailed procedures required to determine the serviceability of a part, assembly, specific inter-relationship of parts that perform a functional operation

Answer 53

Inspection/Check

Question 54

This section contain specific tests and procedures required to determine the condition of a component, and return it to service.

Answer 54

Testing and Fault Isolation

Question 55

Shall contain sufficient detail for the return of the component to a serviceable condition.

Answer 55

Component Maintenance Manual