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 72-32-85-300-003 Fan Case - Repair The Attrition Lining Below The GRP Layer, Repair-003 (VRS1412)
Effectivity
FIG/ITEM | PART NO. |
|---|---|
01-100 | 5W0093 |
01-100 | 5W0094 |
01-100 | 5W0069 |
01-100 | 5W0100 |
01-100 | 5W0072 |
01-100 | 5W0081 |
01-100 | 5W0184 |
01-100 | 5W0186 |
01-100 | 5W0187 |
01-100 | 5W0188 |
01-100 | 5W0189 |
01-100 | 5W0190 |
Material of component
DESCRIPTION | SYMBOL | MATERIAL |
|---|---|---|
Casing | Titanium alloy | |
Attrition lining | Aluminum alloy 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 the attrition lining by filling with blue filler and can be applied below the GRC layer.
The practices and processes referred to in the procedure by the TASK numbers are 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 | ||
| Sealant gun | LOCAL | Sealant gun | Air powered | |
| 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
Refer to Figure.
Be carefull 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 damage.Remove all loose and damaged material from repair area.
A hollow sound is indicative of suspect bond.
Remove any unsound material.
If damage more than 4 sqin. (25.8 sqcm) in front attrition area, repair, refer to VRS1955 TASK 72-32-85-300-007 (REPAIR-007).
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 percent, repair, refer to VRS1956 TASK 72-32-85-300-008 (REPAIR-008).
NOTE
These repair limits must be applied to the full depth of the GRC layer.Examine the Glass Reinforced Composite (GRC) skin and check for indications of blistering or lack of bond by pressing or tapping.
If necessary do repair, VRS1405 TASK 72-32-85-300-005 (REPAIR-005).
Examine the fan case inner surface of the repair area.
SUBTASK 72-32-85-350-055 Prepare Areas of Damage
Refer to the SPM TASK 70-11-26-300-503.

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 RESPONSILIBILTY 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.Fully remove the grease from the area.
SUBTASK 72-32-85-110-069 Remove the Grease from the Repair Area
Refer to the SPM TASK 70-36-02-360-501.
Measure out materials by weight.
SUBTASK 72-32-85-350-056 Prepare the 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.
If the complete fan track is to be filled to the depth of the GRC layer.
Start at the bottom and work both sides.
The filler will gradually set.
If any sagging is apparent, locally produced supports will be necessary.
Fill the filler slightly more than necessary level 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 the filler to the contours.
SUBTASK 72-32-85-350-057 Apply the Filler Material
Step is acceptable if less than 0.02 in. (0.5 mm).
If necessary do this TASK again.
Refer to Figure.
Examine the surface of repaired area.
SUBTASK 72-32-85-220-053 Examine the repair Area
Figure: Filling repair of attrition linings
Filling repair of attrition linings

Figure: Curing Chart of Filling Material (CoMat 08-006)
Curing Chart of Filling Material (CoMat 08-006)

