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 72-00-50-200-005-B00 LPT Module - Manifold Brackets - Examine, Inspection-005
General
This TASK gives the procedure for the inspection of the manifold brackets. For other LP turbine module parts, refer to TASK 72-00-50-200-000 (INSPECTION/CHECK-000).
Fig/item numbers in parentheses in the procedure agree with those used in the IPC.
The policy that is necessary for check is given in the SPM TASK 70-20-01-200-501.
All the parts must be cleaned before any part is examined. Refer to TASK 72-00-50-100-000 (CLEANING-000).
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.
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 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 procedure for crack test is given in Step. Do the test before the part is visually examined.
The practices and processes referred to in the procedure by the TASK number are in the SPM.
References
Refer to the SPM for data on these items.
Definitions of Damage, TASK 70-02-02-350-501
Inspection of PARTS, TASK 70-20-01-200-501
Some data on these items are contained in this TASK. For more data on these items refer to the SPM.
Method of Testing for Crack Indications
Checical Processes
Surface Protection
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
NONEConsumables, Materials and Expendables
NONESpares
NONESafety Requirements
NONEProcedure
Clean the parts. Refer to TASK 72-00-50-100-000 (CLEANING-000).
SUBTASK 72-00-50-220-166 Examine the Manifold Brackets (01-450 and 01-470) for Cracks
Refer to Figure.
Repair, VRS1055 TASK 72-00-50-300-008 (REPAIR-008)
Damage
Repair, VRS1055 TASK 72-00-50-300-008 (REPAIR-008)
Loosened rivet
Examine the plate nuts at location 2.
SUBTASK 72-00-50-220-168 Examine the Manifold Brackets (01-450 and 01-470) Plate Nuts
Refer to Figure.
Repair, VRS1062 TASK 72-00-50-300-007 (REPAIR-007)
Any nicks
Nicked.
Repair, VRS1062 TASK 72-00-50-300-007 (REPAIR-007)
Any scratches
Scratches.
Examine all the surface.
SUBTASK 72-00-50-220-169 Examine the Manifold Brackets (01-450 and 01-470) Surface
Figure: Location on the manifold bracket
Location on the manifold bracket

