Structural Repair Manual

Which unit system is used in Station Dimensions in the SRM?. milimeters. Pulgadas. Metros.

Which Authority Approve the SRM A320 family?. EASA. FAA. CIO.

Which Non-Customized Manual gives us the Material Specification materials like sealants, cleaning solvents, Primers, etc.?. CML. SRM. SRI.

Which of the following list gives us the Register, MSN and WV of an Aircraft?. Aircraft cross reference table. Structural Repair manual. International aero engine and CFM international.

What concept belongs to the following definition "Calls attention to methods which make the job easier or provide supplementary or explanatory information.". Notes. Concepts. Chapters.

Which Manual do we have to use if we need repair an Engine Cowling?. Nacelle Structural Repair manual SRM Engine. Standar manual. Chapters.

What is the first document to be used to repair, assess the damage, and identify the affected aircraft structure?. SRM. CIO. CML.

The SRM breakdown is... (Choose the best option). Front pages manual introduction chapter SRI information and chapters from 51 to 57. Piererence table. Aircraft cross reference table.

Structure Repair Inspections (SRI) gives inspection information... Category B repair and allowable damage category B. For permanent repair and allowable damages limits. Allowable damage.

Regarding the SRM numbering system, what is the correct statement?. The third element identifies the subsection and is assigned by ATA 100 (ATA ispec 2200). In the second element, the first digit is assigned by the ATA SPEC 100 (ATA ispec 2200). The first element designates the chapter which is assigned by AIRBUS.

What does SM mean?. Standard manual. Structural manual.

The WV number listed in SRM is not necessarily the actual status of the Aircrafts. True,it can change. No. it doesn't change.

In the following part number D53370354202,which drawing number is ?. D53370354. D51330976. D53360355.

Due to SRM is a non-Customized Manual, which effectivity Numbers are necessary?. Generic and Envelope. Envelope.

Which Damages and Repairs have Future Structure Repair Inspections (SRI) requirements?. Category B repair and allowable damage category B. Repair and allowable categoría A. Category A repair and allowable damage.

In according the following P/N D53231715201, where it is located in the Aircraft?. RH side fuselage. LH side fuselage.

How "Non-Repairable Damages" are repaired?. Repair by replacement. Damage not’repairable. Permanent repairable.

Which Damages and Repairs have Future Structure Repair Inspections (SRI) requirements?. Category B repair and allowable damage category B. For permanent repair and allowable damages limits. Nacelle Structural Repair manual SRM Engine.

Talking about Function Codes, i.e. 53-21-11-283-001, which information the 283 code shows?. Allowable damage limits. Detailed Drawings. Alternative fastener.

In according the following P/N D53231715202, where is located in the Aircraft?. LH. RH. LH and RH.

What is the concept that belong to the following definition "CALLS ATTENTION TO USE OF MATERIAL, PROCESSES, METHODS, PROCEDURES OR LIMITS WHICH MUST BE FOLLOWED PRECISELY TO AVOID INJURY OR DEATH TO PERSONS". Warning. Cation.

What is the concept of "Allowable damage"?. Damage that has no significant effect on the strength or fatigue life of the structure. Repair and allowable categoría A. International aero engine and CFM international.

What is the concept of the following definition "CALLS ATTENTION TO METHODS AND PROCEDURES WHICH MUST BE FOLLOWED TO AVOID DAMAGE TO EQUIPMENT",. Caution. Warning.

How Information related to allowable damage is shown in the SRM?. General info and diagramas of allowable damage. Nacelle Structural Repair manual SRM Engine. Information and chapters from 51 to 57.

In the identification Table, column, Action or Repair, the word "Replace" can appears, what does mean?. Is A recomendations. Modifications. Inspection.

How Structure Identification is shown in SRM?. Chapters 52-57. Chapters 53-55. Chapters 51-56.

About Function Codes, ie, 53-51-12-205-001, which information does the 205-code show.?. Inspection. Modifications. Reparations.

About Function Codes, i.e., 53-11-12-300-003, which information does the 300-code show?. Repairs. Recomendations. Limits.

During the structural identification process can appear the next status number A2003K0002D, what is the meaning of the prefix A letter?. Or after (A letter SB or modificatión A Permanent no requiere reinspeccion. Repair and allowable categoría A. For permanent repair and allowable damages limits.

Effectivity in SRM is also showed by Configuration codes, and are always in ascending, sequential numerical order, how is shown?. Confí 1, confi 2, confi 3. Chapters 1, chapters 2 , chapters 3.

What is the veracity of the following "The SRM used to evaluate damage to an A319 can also be used to assess damage to an A318 aircraft.". True. False.

What type of Drawings is shown by the following P/N D53231715202?. Detailed Drawing. Alternative fasteners.

Which Dents dimensions are necessary to perform the Damage Assessment?. X,Y,A,D. X,Y,Z,D. Y,Z,AX.

The Chapter 53 has the following Repair Types: Permanent and temporary. Temporary. Repair inspection.

When a fastener hole is damaged and outside the tolerances for the original fastener nominal diameter. An Oversize fastener must be installed. Allowable damage limits. Nacelles Structural Repair manual SRM Engine.

The fasteners of the same diameter that can be used instead of the original are called. Alternative fastener. General info and diagrams.

-Which Non-Customized Manual gives us the information of Standard Codes, i.e., NAS1097DD, ASN-A30128677 etc.?. SM. RH. CML.

Function Code 912: Chapter 51 Description. Allowable Damage Limits. Repair.

Function Code 283: Allowable Damage Limits. Repair. Inspections.

Function Code 300: Repair. Inspections. Chapter 51 Description.

Function Code 205: Inspections. Chapter 51 Description. Allowable Damage Limits.