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AMT 2107 > 2107 > Flashcards

2107 Flashcards

1
Q

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.

A

Description and Operation

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2
Q

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

A

Troubleshooting function

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3
Q

SRM 7 Chapters

A

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

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4
Q

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

A

Temporary allowable Damage
Repair Category C

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5
Q

CMS

A

Component Maintenance Sheet

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6
Q

AEB

A

Airline Engineering Bulletin

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7
Q

ACM

A

Abbreviated Component Maintenance Manual

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8
Q

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

A

Remarks and/or Exceptional Column

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9
Q

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

A

Configuration Deviation List

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10
Q

Category of MEL

A

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

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11
Q

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.

A

Logbook entry

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12
Q

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

A

Troubleshooting function

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13
Q

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.

A

CFDS Fault Message

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14
Q

is fault via text or keywords and ATA chapters.

A

TSM Entry

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15
Q

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

A

Crew or Maintenance Observation

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16
Q

Non-Monitored Faults

A

Crew or Maintenance Observations

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17
Q

Monitored Faults

A

ECAM warnings, EFIS flags, CFDS

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18
Q

Types of Faults

A

Monitored and Non-Monitored Faults

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19
Q

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

A

Troubleshooting Manual

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20
Q

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

A

Troubleshooting Manual

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21
Q

Manuals usage

A
  1. Determine Damage Classification
  2. Identify Damaged Parts in the Manual
  3. Determine Repair Procedures
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22
Q

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

A

Determine Repair Procedures

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23
Q

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

A

Determine Repair Procedures

24
Q

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

A

Identify damaged parts in the manual

25
Q

Refer to the figure reference at section, subsection level.

A

Identify damaged parts in the manul

26
Q

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

A

Identify damaged parts in the manual

27
Q

Refer to topic “allowable damage” in the relevant chapter

A

Determine Damage Classification

28
Q

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

A

Determine Damage Classification

29
Q

Minor damage which does not effect the structural integrity

A

Allowable damage

30
Q

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

A

Determine Damage Classification

31
Q

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

A

Structural Repair Manual

32
Q

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

A

Structural Repair Manual

33
Q

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

A

Structural Repair Manual

34
Q

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

A

Structural Repair Manual

35
Q

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

A

Storage including transportation

36
Q

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

A

Special tools, fixtures, equipment, and consumable

37
Q

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

A

Fits and clearance

38
Q

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

A

Assembly

39
Q

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

A

Repair

40
Q

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

A

Cleaning

41
Q

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

A

Disassembly

42
Q

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.

A

Description and operation

43
Q

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

A

Component Maintenance Manual

44
Q

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

A

Component Maintenance Manual

45
Q

OD

A

Outside Diameter

46
Q

ID

A

Inside Diameter

47
Q

ATLAS

A

Abbreviated Test Language for All Systems

48
Q

ATA

A

Air Transport Association of America

49
Q

FIN

A

Functional Item Number

50
Q

Allowable Damage

A

Content of SRM

51
Q

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.

A

Permanent Allowable Damage
Repair Category A

52
Q

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

A

Minimum Equipment List

53
Q

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

A

Inspection/Check

54
Q

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

A

Testing and Fault Isolation

55
Q

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

A

Component Maintenance Manual

AMT 2107 (1 decks)

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