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 72-32-87-200-001 Fan Case Liner Panel Rubber Seal - Examine, Inspection-001
Effectivity
FIG/ITEM | PART NO. |
|---|---|
01-100 | 5A0819 |
01-100 | 5A1601 |
01-100 | 5A2139 |
01-150 | 5A0823 |
01-150 | 5A2140 |
01-150 | 5A2179 |
01-150 | 5A2190 |
01-200 | 5A0824 |
01-200 | 5A2141 |
01-250 | 5A0825 |
01-250 | 5A2142 |
01-300 | 5A0827 |
01-300 | 5A2143 |
01-300 | 5A2180 |
01-300 | 5A2191 |
01-350 | 5A0828 |
01-350 | 5A2144 |
01-400 | 5A0829 |
01-400 | 5A2145 |
01-400 | 5A2181 |
01-400 | 5A2192 |
01-450 | 5A0830 |
01-450 | 5A2146 |
01-500 | 5A0831 |
01-500 | 5A2147 |
01-550 | 5A0832 |
01-550 | 5A2148 |
01-550 | 5A2182 |
01-550 | 5A2193 |
General
This TASK gives the procedure for the inspection of the panel rubber seal.
The policy that is necessary for inspection is given in the SPM TASK 70-20-00-200-501.
All the parts must be cleaned before any part is examined. Refer to the TASK 72-32-87-100-000 (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.
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 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:
Definition of Damage, SPM TASK 70-02-02-350-501.
Inspection of Parts, SPM TASK 70-20-00-200-501.
Some data on these items are contained in this TASK. For more data on these items refer to the SPM:
Chemical Processes
Surface Protection
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
NONEConsumables, Materials and Expendables
NONESpares
NONESafety Requirements
NONEProcedure
Refer to Figure.
Repair, VRS1940 TASK 72-32-87-300-007 (REPAIR-007)
Not more than 0.118 in. (3.00 mm) in length and any number of cracks
Repair, VRS1940 TASK 72-32-87-300-007 (REPAIR-007)
Not more than 0.197 in. (5.00 mm) in length and the number of bushes with cracks is two or less
More than 0.197 in. (5.00 mm) in length Step
Cracks which go to or come from the edge of groove. Refer to Figure at detail A.
Repair, VRS1940 TASK 72-32-87-300-007 (REPAIR-007)
If the number of grooves with cracks is two or less
More than in Step
Cracked.
Examine the panel rubber seal around the bushes at location 1.
SUBTASK 72-32-87-220-051 Examine the Panel Rubber Seal Around the Bushes
Refer to Figure.
Repair, VRS1940 TASK 72-32-87-300-007 (REPAIR-007)
More than in Step
Scored or scratched.
Repair, VRS1940 TASK 72-32-87-300-007 (REPAIR-007)
Any number of cracks
Repair, VRS1940 TASK 72-32-87-300-007 (REPAIR-007)
Not more than one crack
More than in Step
More than in Step
Cracked.
Examine the edge surfaces at location 3.
SUBTASK 72-32-87-220-053 Examine the Panel Rubber Seal Edge Surfaces
Refer to Figure.
Repair, VRS1940 TASK 72-32-87-300-007 (REPAIR-007)
Any number of cracks
Repair, VRS1940 TASK 72-32-87-300-007 (REPAIR-007)
Not more than one crack
More than in Step
More than in Step
Cracked.
Repair, VRS1940 TASK 72-32-87-300-007 (REPAIR-007)
More than in Step
Nicked, dented, worn or pitted (caused by erosion).
Examine the curved area at location 4.
SUBTASK 72-32-87-220-054 Examine the Panel Rubber Seal Curved Area
Refer to Figure.
Repair, VRS1940 TASK 72-32-87-300-007 (REPAIR-007)
More than in Step
Scored or scratched.
Repair, VRS1940 TASK 72-32-87-300-007 (REPAIR-007)
Any number of cracks
Repair, VRS1940 TASK 72-32-87-300-007 (REPAIR-007)
If the number of groove with cracks is two or less
More than in Step
Cracked.
Examine the grooves at location 5.
SUBTASK 72-32-87-220-086 Examine the Panel Rubber Seal Grooves
Refer to Figure.
Repair, VRS1940 TASK 72-32-87-300-007 (REPAIR-007)
Any number of cracks
Repair, VRS1940 TASK 72-32-87-300-007 (REPAIR-007)
Not more than one crack
More than in Step
More than in Step
Cracked.
Repair, VRS1940 TASK 72-32-87-300-007 (REPAIR-007)
More than in Step
Nicked, dented, worn or pitted (caused by erosion).
Examine the remaining surfaces which do not include the identified locations before.
SUBTASK 72-32-87-220-087 Examine the Panel Rubber Seal Remaining Surfaces
Figure: Locations on the Panel Rubber Seal
Locations on the Panel Rubber Seal

