Export Control
EAR Export Classification: Not subject to the EAR per 15 C.F.R. Chapter 1, Part 734.3(b)(3), except for the following Service Bulletins which are currently published as EAR Export Classification 9E991: SBE70-0992, SBE72-0483, SBE72-0580, SBE72-0588, SBE72-0640, SBE73-0209, SBE80-0024 and SBE80-0025.Copyright
© IAE International Aero Engines AG (2001, 2014 - 2021) The information contained in this document is the property of © IAE International Aero Engines AG and may not be copied or used for any purpose other than that for which it is supplied without the express written authority of © IAE International Aero Engines AG. (This does not preclude use by engine and aircraft operators for normal instructional, maintenance or overhaul purposes.).Applicability
All
Common Information
TASK 79-21-42-200-401 Air Cooled Oil Cooler (ACOC) - Related Parts - Examine The ACOC Brackets, Inspection-001
General
This TASK gives the procedure for the inspection of the ACOC brackets. For other ACOC parts, refer to Inspection/Check-000 TASK 79-21-42-200-400 and TASK 79-21-42-200-100 in the Component Maintenance Manual (CMM-THD-V2500-1IA).
Fig/item numbers in parentheses in the procedure agree with those used in the IPC. Only primary Fig/item numbers are used. For the service bulletin alpha variants refer to the IPC.
All the parts must be cleaned before they are examined. Refer to TASK 79- 21-42-100-400.
All the parts must be visually examined for damage, corrosion and wear. Defects that are not identified in the procedure must be referred to IAE.
Do not discard the part until you are sure there are no repairs available. Refer to the instructions in Repair before a discarded part is used again or oversize parts are installed.
Parts which must be discarded can be held although no repair is available. The repair of a discarded part could be shown to be necessary at a later date.
All the parts must be examined to make sure that all the repairs have been completed satisfactorily.
The practices and processes referred to in the procedure by the TASK/SUBTASK number are in the SPM.
References
Refer to the SPM for data on these items.
Definitions of Damage, SPM TASK 70-02-02-350-501.
Inspection Policy and Inspection of Parts, SPM TASK 70-20-01-200-501.
Some data on these items is contained in this TASK. For more data on these items refer to the SPM.
Method of Testing for Crack Indications.
Chemical Processes.
Surface Protection.
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
NONEConsumables, Materials and Expendables
NONESpares
NONESafety Requirements
NONEProcedure
Reject.
Cracked
Examine all the surfaces for cracks
SUBTASK 79-21-42-220-056 Examine the Bracket (01-084, 01-088, 01-090 and 01-350) for Cracks
SUBTASK 79-21-42-220-057 Examine the Surface of the Bracket (01-084, 01-088, 01-090 and 01-350)
Reject.
Bolt hole burred
Reject.
Other than in Step
Worn
Examine the mounting bolt hole
Reject.
Other than in Step
Worn
Examine the center clip position bolt hole
Reject.
Other than in Step
Worn
Examine the remaining clip position bolt holes
SUBTASK 79-21-42-220-058 Examine the Bracket (01-084 and 01-350) Bolt Hole
