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 72-41-31-200-008 HPC Blank - Examine, Inspection-008
General
This TASK gives the procedure for the inspection of the support tool blanks.
Fig/item numbers in parentheses in the procedure agree with those used in the EIPC.
The policy that is necessary for inspection is given in the SPM TASK 70-20-01-200-501.
All the parts must be cleaned before any part is examined.
All the parts must be visually examined for damage, corrosion and wear. Any defects that are not identified in the procedure must be referred to IAE.
A ** following repair referenced in this inspection indicates that the repair is not yet published in the current revision of the manual and the part must be rejected. Contact IAE for additional information concerning FAA approved repair date.
The procedure for the parts which must have a crack test is given in Step. Do the 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 should be discarded can be held although no repair is available. The repair of a discarded part can be shown to be necessary at a subsequent date.
All the parts must be examined to make sure that all the repairs have been completed satisfactory.
The practices and processes referred to in the procedure by the TASK numbers are in the SPM.
References
Refer to the SPM for data on these items
Definitions of Damage, TASK 70-02-02-350-501
Record and Control of the Lives of Parts, TASK 70-05-00-220-501
Inspection of Parts, TASK 70-20-01-220-501.
Some data on these items is contained in this TASK. For more data on these items refer to the SPM
Methods 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 parts. Refer to TASK 72-41-31-100-000.
SUBTASK 72-41-31-230-058 Examine the Support Tool Blanks (01-120) for Cracks
Refer to Figure.
Repair, VRS6274 TASK 72-41-31-300-013
Galled or scored
SUBTASK 72-41-31-220-091 Examine the Support Tool Blanks (01-120) Faces at Locations 1 and 2
Refer to Figure.
Repair, VRS6274 TASK 72-41-31-300-013
Burred edges
Repair, VRS6274 TASK 72-41-31-300-013
Scored
SUBTASK 72-41-31-220-092 Examine the Support Tool Blanks (01-120) Bolt Holes at Location 3
Repair, VRS6274 TASK 72-41-31-300-013
More than in step A.(1)
Nicked, dented and scratched.
SUBTASK 72-41-31-220-116 Examine the Support Tool Blanks (01-120) all Remaining Surfaces
Figure: Support tool blanks - Inspection locations
Support tool blanks - Inspection locations

