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 71-51-42-200-401 EEC Fan Harness And Ignition Supply Harness - Related Parts - Examine The EEC And Ignition Supply Harness Raceways, Inspection-001
General
NOTE
This TASK gives the procedure for the inspection of the EEC and Ignition supply harness raceway. For the other EEC and Ignition supply harness parts, refer to TASK 71-51-42-200-400 (71-51-42, Inspection/Check-000, Page 801) and Inspection/Check-000 TASK 71-51-42-200-300 in the Component Maintenance Manual - Electrical Harnesses and Cables (CMM-EHC-V2500-1IA) .
Fig/item numbers in parentheses in the procedure agree with those used in the IPC. Only the primary Fig/item numbers are used. For the service bulletin alpha variants refer to the IPC.
The policy which is necessary for inspection is given in SPM TASK 70-20-01-200-501.
All the parts must be cleaned before they are examined, refer to Cleaning-000 TASK 71-51-42-100-400.
All the parts must be visually examined for damage, corrosion and wear.
Defects which are not identified in the procedure must be referred to IAE.
The procedure for those parts which must have a crack test is given in the relevant SUBTASK. Do a crack test before the part is visually examined.
Do not discard any 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 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:
Definition of Damage, SPM TASK 70-02-02-350-501.
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
Clean the part. Refer to Cleaning-000 TASK 71-51-42-100-400.
Reject
Cracked
Raceway (05-100 or 05-300). Refer to SPM TASK 70-23-00-230-501.
Do the crack test on the parts that are given below. Use the applicable penetrant inspection procedure.
SUBTASK 71-51-42-230-001 Examine the Raceway for Cracks
Refer to Figure.
Reject
Limits more than in Step.
Distorted
SPM VRS7001 (Repair-001) TASK 70-35-24-300-501.
Limits more than in Step.
Nicked, scratched or scored.
SUBTASK 71-51-42-220-001 Examine the Surfaces of the Raceway
Refer to Figure.
SPM VRS7001 (Repair-001) TASK 70-35-24-300-501.
Cracked or damaged.
SPM VRS7001 (Repair-001) TASK 70-35-24-300-501.
Bent or distorted.
SUBTASK 71-51-42-220-002 Examine the Raceway Clips
Refer to Figure.
Accept
The distance between edge and worn hole is not less than 0.05 in. (1.3 mm).
SPM VRS7001 (Repair-001) TASK 70-35-24-300-501.
Less than 0.05 in. (1.3 mm).
Worn
SPM VRS7001 (Repair-001) TASK 70-35-24-300-501.
Burred
SUBTASK 71-51-42-220-003 Examine the Raceway Bolt Holes
Figure: Inspection of the Raceway
Inspection of the Raceway

