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 72-60-31-200-003 Deoiler Air Port Casing - Examine, Inspection-003
General
This TASK gives the procedure for the inspection of the casing air port. For the other parts of the deoiler case and cover, refer to TASK 72-60-31-200-001 (INSPECTION-001).
Fig/item numbers in parentheses in the procedure agree with those used in 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. Refer to the SPM TASK 70-11-03-300-503.
All 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 those parts which must have a crack test is given in the SPM TASK 70-23-00-230-501. Do the test before the part is visually examined. Limits for cracks are given in the SUBTASK for each part.
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 parts must be examined to make sure that all the repairs have been completed satisfactorily.
Do dimensional inspections only if the visual inspection or some other condition makes it necessary.
The practices and the processes referred to in the procedure by the TASK numbers are in the SPM.
References
Refer to the SPM for data on these items:
Definition of Damage, SPM TASK 70-02-02-350-501,
Record and Control of the Lives of the Parts, SPM TASK 70-05-00-220-501,
Inspection of Parts, SPM 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,
Chemical Processes,
Surface Protection.
NOTE
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| FPI Inspection station | LOCAL | FPI Inspection station | ||
| Workshop inspection equipment | LOCAL | Workshop inspection equipment |
Consumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 02-140 TRIANGULAR INDIA STONE, FINE GRIT | LOCAL | CoMat 02-140 |
Spares
NONESafety Requirements
NONEProcedure
Clean the part. Refer to TASK 72-60-31-100-000 (CLEANING-000).
SUBTASK 72-60-31-230-005 Do a Crack Test on the Casing Air Port (72-60-31,01-090) and (72-60-31,01-125) Fluorescent Penetrant
Refer to Figure.
Refer to the SPM TASK 70-35-03-300-501.
Repair the surface protection.
Refer to the SPM TASK 70-38-02-300-503.
Hand polish and blend.
The maximum depth of the blending is 0.04 in. (1.0 mm).
More than in Step.
SUBTASK 72-60-31-220-083 Examine the Casing Air Port (72-60-31,01-090) and (72-60-31,01-125) Rough Surfaces at Location 1
Refer to Figure.
The maximum depth of the blending is 0.010 in. (0.25 mm).
Refer to the SPM TASK 70-35-03-300-501.
Repair the surface protection.
Refer to the SPM TASK 70-38-02-300-503.
Hand polish and blend.
More than in Step.
SUBTASK 72-60-31-220-084 Examine the Casing Air Port (72-60-31,01-090) and (72-60-31,01-125) Machined not Seal Surfaces at Location 2
Refer to Figure.
More than in Step.
The maximum depth of the blending is 0.004 in. (0.10 mm).
Refer to the SPM TASK 70-35-03-300-501.
Repair the surface protection.
Refer to the SPM TASK 70-38-02-300-503.
Hand polish and blend.
SUBTASK 72-60-31-220-085 Examine the Casing Air Port (72-60-31,01-090) and (72-60-31,01-125) Machined Seal Surfaces at Location 3
Refer to the SPM TASK 70-38-02-300-503.
SUBTASK 72-60-31-220-086 Examine the Casing Air Port (72-60-31,01-090) and (72-60-31,01-125) Protective Finish
Refer to the SPM TASK 70-35-08-300-501, SUBTASK 70-35-08-350-001 , SUBTASK 70-35-08-350-002 and SUBTASK 70-35-08-220-001 .
SUBTASK 72-60-31-220-087 Examine the Casing Air Port (72-60-31,01-090) and (72-60-31,01-125) Helicoil Inserts
Refer to Figure.
SUBTASK 72-60-31-220-088 Examine the Casing Air Port (72-60-31,01-090) and (72-60-31,01-125) Tube Bore at Location 4
Refer to Figure.
SUBTASK 72-60-31-220-089 Examine the Casing Air Port (72-60-31,01-090) and (72-60-31,01-125) Seal Housing Bore at Location 4005
Refer to Figure.
SUBTASK 72-60-31-220-090 Examine the Casing Air Port (72-60-31,01-090) and (72-60-31,01-125) Pilot Diameter at Location 5
Figure: Casing Air Port - Inspection Locations
Sheet 1

Figure: Casing Air Port - Inspection Locations
Sheet 2

