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 72-32-85-300-018 Fan Case - Repair The Attrition Lining Below The GRC Layer, Repair-018 (VRS1557)
Material of component
DESCRIPTION | SYMBOL | MATERIAL |
|---|---|---|
Casing | Titanium alloy | |
Attrition lining | Aluminum honeycomb | |
Attrition lining | Non-metallic honeycomb | |
Attrition lining | Glass reinforced composite | |
Attrition lining | Filling compound |
General
Price and availability - Refer to IAE
This Repair scheme gives the procedure for repair of attrition lining by filling with filler and can be applied below the Glass Reinforced Composite (GRC) layer.
The practices and processes referred to in the procedure by the TASK number ar in the SPM.
NOTE
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| Hand held pneumatic grinder | LOCAL | Hand held pneumatic grinder | ||
| Rotary files | LOCAL | Rotary files | ||
| Plastic scraper | LOCAL | Plastic scraper | ||
| Putty knife | LOCAL | Putty knife | ||
| Vacuum cleaner | LOCAL | Vacuum cleaner |
Consumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 01-076 METHYL ETHYL KETONE | LOCAL | CoMat 01-076 | ||
| CoMat 02-099 LINT-FREE CLOTH | LOCAL | CoMat 02-099 | ||
| CoMat 05-016 GARNET PAPER, 80-GRIT | LOCAL | CoMat 05-016 | ||
| CoMat 08-006 FILLER, TWO PACK | LOCAL | CoMat 08-006 |
Spares
NONESafety Requirements
NONEProcedure
Be careful not to cause damage to the inner surface of the fan case assembly.

CAUTION
CHECK THE TOTAL REPAIR AREA PRIOR TO STARTING THE REPAIR. DO NOT CARRY OUT REPAIR BY FILLING THE ATTRITION LININGS IF THE TOTAL REPAIRED AREA EXCEEDS 20 PERCENT OF THE TOTAL FAN CASE ATTRITION LINING AREA. THESE REPAIR LIMITS MUST BE APPLIED TO THE FULL DEPTH OF THE GRC LAYER.
CAUTION
THE FAN CASE IS MADE FROM TITANIUM ALLOY AND IS THIN IN SOME AREAS. IF YOU HIT THE FAN CASE WITH A CHISEL OR SCRAPER YOU CAN MAKE IT UNSERVICEABLE.
CAUTION
YOU MUST USE THE CHISEL, SHARP BLADE OR SCRAPER IN A CIRCUMFERENTIAL DIRECTION TO PREVENT THE EDGES OF THE BLADE SCORING THE FAN CASE.
CAUTION
YOU MUST ALWAYS TRY TO POINT THE CHISEL OR SHARP BLADE PARALLEL WITH THE SURFACE OF THE FAN CASE.
CAUTION
STOP MACHINING AS SOON AS THE FILES, CUTTERS OR MACHINING BITS ARE THROUGH THE LINING MATERIAL. USE A STOP-MACHINING OR SLEEVE OR OTHER PENETRATION LIMITING DEVICE TO PREVENT DAMAGE TO THE CASING MATERIAL.
CAUTION
DO NOT USE POWERED TOOLS WITH STEEL CHISEL OR SIMILAR BITS.
CAUTION
DO NOT OPERATE WITHOUT SAFETY GOGGLES AND OTHER GUARD EQUIPMENT. FLYING PARTICLES CAN CAUSE INJURY.NOTE
Remove the minimum quantity of material necessary to remove all the damage.Remove loose and damaged material from repair area.
A hollow sound is indicative of a suspect bond.
Remove any unsound material.
If damage is more than 4 sqin (25.8 sqcm) in front attrition area, Repair, refer to VRS1538 TASK 72-32-85-300-022(REPAIR-022).
Examine the repaired area, ratio not more than 20 percent of total rear attrition area and/or rear attrition area of one segment of attrition lining.
If more than 20 per cent, repair, refer to VRS1538 TASK 72-32-85-300-022 (REPAIR-022).
NOTE
These repair limits must be applied to the full depth of GRC layer.Examine the GRC layer and check for indications of blistering or lack of bond by pressing or tapping.
If necessary, do Repair, VRS1554 TASK 72-32-85-300-016 (REPAIR-016).
Examine the fan case inner surface of the repair area.
SUBTASK 72-32-85-350-073 Remove Defective Areas of Damage
Refer to SPM TASK 70-11-26-300-503.
Fully remove the grease from the area.
SUBTASK 72-32-85-110-071 Remove the Grease from the Repair Area

WARNING
ALWAYS MAKE SURE THERE IS SUFFICIENT VENTILATION IN THE WORK AREA. EYE PROTECTION MUST ALWAYS BE USED. DO NOT LET THE SOLVENT CLEANER OR ITS VAPOR TOUCH THE EYES OR SKIN. PROTECTIVE CLOTHING AND FACE MASK MUST ALWAYS BE USED. ALWAYS KEEP OPEN FLAMES AWAY FROM THE WORK AREA. IT IS THE RESPONSIBILITY OF THE OPERATOR TO OBTAIN AND OBSERVE THE MANUFACTURERS MATERIAL SAFETY SHEETS FROM THE CONSUMABLE MATERIALS INFORMATION SUCH AS HAZARDOUS INGREDIENTS, PHYSICAL/CHEMICAL CHARACTERISTICS, FIRE, EXPLOSION, REACTIVITY, HEALTH HAZARD DATA, PRECAUTIONS FOR SAFE HANDLING, USE AND CONTROL MEASURES AND ALSO TO TAKE LOCAL REGULATIONS INTO CONSIDERATION.Refer to SPM TASK 70-36-02-360-501.
Measure out materials by weights.
SUBTASK 72-32-85-360-060 Prepare Filler Material
Refer to the SPM TASK 70-36-02-360-501.
Use air powered sealant gun.
Make sure that the repair area is fully filled with no air pockets.
The filler will gradually set.
If any sagging is apparent, locally produced supports will be necessary.
Fill the filler slightly more than necessary in the damaged area.
The cure times and temperatures are given in Figure.
Cure the filler.
Refer to Figure.

CAUTION
DO NOT OPERATE WITHOUT SAFETY GOGGLES AND OTHER GUARD EQUIPMENT. FLYING PARTICLES CAN CAUSE INJURY.NOTE
The minimum cure time is one hour.Blend filler to the contours.
SUBTASK 72-32-85-350-074 Apply Filler Material
A step is acceptable if less than 0.02 in. (0.5 mm).
Refer to Figure.
Examine the surface of repair area.
SUBTASK 72-32-85-220-082 Examine the Repair Area
Figure: Filling repair the attrition lining
Filling repair the attrition lining

Figure: Curing chart for filling material (CoMat 08-006)
Curing chart for filling material (CoMat 08-006)

