2107 Flashcards
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.
Description and Operation
is initiated by a logbook entry from the flight crew or maintenance crew.
Troubleshooting function
SRM 7 Chapters
Chapter 51 – Structure–General
Chapter 52 – Doors
Chapter 53 – Fuselage
Chapter 54 – Nacelle/Pylons
Chapter 55 – Stabilizers
Chapter 56 – Windows
Chapter 57 – Wings
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
Temporary allowable Damage
Repair Category C
CMS
Component Maintenance Sheet
AEB
Airline Engineering Bulletin
ACM
Abbreviated Component Maintenance Manual
When a missing part introduces additional limitations, this limitations is included in the
Remarks and/or Exceptional Column
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
Configuration Deviation List
Category of MEL
Category A - for monitoring
Caregory B - 3 days
Category C - 10 days
Category D - 120 days
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.
Logbook entry
is initiated by a logbook entry from the flight crew or maintenance crew.
Troubleshooting function
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.
CFDS Fault Message
is fault via text or keywords and ATA chapters.
TSM Entry
are usually a single fault without an associated CFDS fault message.
Crew or Maintenance Observation
Non-Monitored Faults
Crew or Maintenance Observations
Monitored Faults
ECAM warnings, EFIS flags, CFDS
Types of Faults
Monitored and Non-Monitored Faults
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
Troubleshooting Manual
Is provided by Airbus Industry to enable the systematic identification, isolation and correction of aircraft warnings and malfunction reported in flight and in ground
Troubleshooting Manual
Manuals usage
- Determine Damage Classification
- Identify Damaged Parts in the Manual
- Determine Repair Procedures
In the event of major structural damage the required replacement part can be ordered by means of the Spare Parts Identification
Determine Repair Procedures
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
Determine Repair Procedures
Locate the relevant figure, identify the damaged component and refer to the relevant identification page
Identify damaged parts in the manual
Refer to the figure reference at section, subsection level.
Identify damaged parts in the manul
Locate the section and subsection which refers to the damaged part in the table of contents
Identify damaged parts in the manual
Refer to topic “allowable damage” in the relevant chapter
Determine Damage Classification
Locate the section, which refers to the damaged part in the table of contents
Determine Damage Classification
Minor damage which does not effect the structural integrity
Allowable damage
Locate the chapter which refers to the damaged part using the manual chapter index
Determine Damage Classification
Provide data for signiticant damage to the condition required to fulfill its design function.
Structural Repair Manual
Serve as medium for advising developed by the manufacturers or by operators
Structural Repair Manual
Define both damage that has no significant effect on the strength or life of the structure
Structural Repair Manual
Contain descriptive information for aircraft’s primary and secondary structure.
Structural Repair Manual
Contains preparation for transportation, special handling, packaging, storage and preservation requirements associated with the component after assembly or test.
Storage including transportation
Contain a listing of all tools, fixtures, competen, and consumable items necessary for maintenance actions given in the CMM.
Special tools, fixtures, equipment, and consumable
Provides all fits and clearances and torque values used ip assembly, including, permissible In service wear and manufacturers design wear tolerances
Fits and clearance
Provides step by step assembly instructions in a logical sequence, referencing figure item numbers from IPL illustration’s where applicable
Assembly
Contains detailed repair procedures and specifications necessary for restoring a
component to serviceable condition.
Repair
Specifies methods and processes, or refer to applicable standard practices, required for cleaning specific parts or areas of the component
Cleaning
This section contains instructions tor a complete disassembly of the component which do not require opening permanent joints or unsoldering connections.
Disassembly
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.
Description and operation
are intended for work on the applicable components in a workshop environment.
Component Maintenance Manual
Disassembly, test and assembly procedures detailed within the manual shall be verified by the actual performance
Component Maintenance Manual
OD
Outside Diameter
ID
Inside Diameter
ATLAS
Abbreviated Test Language for All Systems
ATA
Air Transport Association of America
FIN
Functional Item Number
Allowable Damage
Content of SRM
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.
Permanent Allowable Damage
Repair Category A
Contains only those items of airworthiness significance which may be inoperative prior to dispatch, provided limitations and appropriate procedures are observed
Minimum Equipment List
Presents the detailed procedures required to determine the serviceability of a part, assembly, specific inter-relationship of parts that perform a functional operation
Inspection/Check
This section contain specific tests and procedures required to determine the condition of a component, and return it to service.
Testing and Fault Isolation
Shall contain sufficient detail for the return of the component to a serviceable condition.
Component Maintenance Manual
