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 72-41-34-200-001-A00 HPC Vane Ring Control Rods - Examine, Inspection-001
Effectivity
FIG./ITEM | PART NO. |
|---|---|
01-200 | UP11076 |
01-200 | 6A4519 |
01-250 | 6A2564 |
01-300 | 6A2564 |
01-300 | 6A4515 |
01-350 | 6A3530 |
01-450 | UP11076 |
07-100 | UP11073 |
General
This TASK gives the procedure for the inspection of the stator vane actuating ring control rods.
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 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.
The procedure for the parts which must have a crack test is given in Step Do the crack test before a 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 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:
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 72-41-34-100-000 (CLEANING-000).
SUBTASK 72-41-34-240-051 Do a Crack Test on the Stator Vane Actuating Ring Control Rods
Refer to Figure.
SUBTASK 72-41-34-220-052 Examine the Stator Vane Actuating Ring Control Rods Threads at Locations 1, 2, 3 and 4
Refer to Figure.
SUBTASK 72-41-34-220-053 Examine the Stator Vane Actuating Ring Control Rods Holes at Locations 4 and 5
Refer to Figure.
The SPM TASK 70-38-35-380-001.
Chipped.
The SPM TASK 70-38-35-380-001.
Peeled.
SUBTASK 72-41-34-220-054 Examine the Stator Vane Actuating Ring Control Rods Body Surface Protection at Locations 6, 7 and 8
Figure: Stator Vane Actuating Ring Control Rods - Inspection Locations
Stator Vane Actuating Ring Control Rods - Inspection Locations
