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 72-32-85-300-039 Fan Case - Repair The Filling Compound, Repair-039 (VRS1823)
Effectivity
FIG/ITEM | PART NO. |
|---|---|
01-100 | 5W0144 |
01-100 | 5W0149 |
01-100 | 5W0154 |
01-100 | 5W0169 |
01-100 | 5W0172 |
01-100 | 5W0194 |
01-100 | 5W0195 |
01-100 | 5W0196 |
01-100 | 5W0197 |
01-100 | 5W0198 |
01-100 | 5W0217 |
01-100 | 5W0218 |
01-100 | 5W0219 |
01-100 | 5W0220 |
01-100 | 5W0221 |
01-100 | 5W0222 |
01-100 | 5W0223 |
01-100 | 5W0224 |
01-100 | 5W0225 |
01-100 | 5W0226 |
01-100 | 5W0307 |
01-100 | 5W0313 |
General
Price and availability - refer to IAE
This repair scheme gives the procedure for repair of gap between anti-ice impact panel and acoustic lining by filling with filling compound.
The practice and processes referred to in the procedure by the TASK numbers are in SPM.
NOTE
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| Hand Tools | LOCAL | Tools, Hand | ||
| Putty knife | LOCAL | Putty knife | ||
| Vacuum cleaner | LOCAL | Vacuum cleaner |
Consumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 01-031 ACETONE (CH3)2CO | LOCAL | CoMat 01-031 | ||
| CoMat 01-076 METHYL ETHYL KETONE | LOCAL | CoMat 01-076 | ||
| CoMat 01-124 ISOPROPYL ALCOHOL | LOCAL | CoMat 01-124 | ||
| CoMat 02-099 LINT-FREE CLOTH | X222X | CoMat 02-099 | ||
| CoMat 05-016 GARNET PAPER, 80-GRIT | LOCAL | CoMat 05-016 | ||
| CoMat 08-006 FILLER, TWO PACK | 00BB6 | CoMat 08-006 | ||
| CoMat 08-024 SEALANT | 23354 | CoMat 08-024 | ||
| CoMat 08-142 POLYSULPHIDE COMPOUND | LOCAL | CoMat 08-142 |
Spares
NONESafety Requirements
NONEProcedure
Use CoMat 05-016 GARNET PAPER, 80-GRIT or hand tools.
Take care not to damage the anti-ice impact panel and acoustic lining.
Refer to Figure. Be careful not to cause damage to inner surface of the fan case assembly.

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.Remove damaged material from repair area.
If damaged, repair, refer to Repair, VRS1821 TASK 72-32-85-300-037 (REPAIR-037) and/or VRS1822 TASK 72-32-85-300-040 (REPAIR-040).

WARNING
DO NOT OPERATE WITHOUT SAFETY GOGGLES AND OTHER GUARDS EQUIPMENT. FLYING MATERIAL CAN CAUSE EYE INJURY.NOTE
Keep the material removal to the minimum necessary, to remove damaged area.Examine the anti-ice impact panel and acoustic lining.
If necessary, do Repair, VRS1805 TASK 72-32-85-300-042 (REPAIR-042) or VRS1818 TASK 72-32-85-300-044 (REPAIR-044).

WARNING
AIR BLAST CREATE FLYING PARTICLES. YOU MUST USE THE SAFETY SHIELD AND OTHER PROTECTIVE EQUIPMENT. FLYING PARTICLES CAN CAUSE EYE INJURY.Examine the fan case inner surface of the repair area.
SUBTASK 72-32-85-350-091 Remove Defective Area of Damage
Refer to 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 MASKS 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 DATA SHEETS FOR 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 repair area, except the blue filler surface.
SUBTASK 72-32-85-110-059 Remove the Grease from the Repair Area
Prepare the filler (CoMat 08-006 FILLER, TWO PACK).
Refer to SPM TASK 70-36-02-360-501.
Measure out materials by weight.
Prepare the sealant (CoMat 08-024 SEALANT or CoMat 08-142 POLYSULPHIDE COMPOUND).
Use CoMat 08-024 SEALANT 75 parts of base compound and 10 parts of curing compound (accelerator) or CoMat 08-142 POLYSULPHIDE COMPOUND 100 parts of base compound 10 parts of curing compound (accelerator) by weight.
Measure out materials by weight.
SUBTASK 72-32-85-360-078 Prepare Filler Material
Option 1: Apply the filler (CoMat 08-006 FILLER, TWO PACK).
Refer to SPM TASK 70-36-02-360-501.
Use air powered sealant gun or equivalent. Make sure that the repair area is fully filled with no air pockets. 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.
Make sure that the repair area is fully filled with no air pockets. Start at the bottom and work both sides. The filler will gradualy set. If any sagging is apparent, locally produced supports will be necessary. Cure the sealant for 10 hours at 77 deg F (25 deg C) or 1.5 hours at 113 deg F (45 deg C).

CAUTION
THE MAXIMUM TEMPERATURE WHICH CAN BE USED TO CURE THE FILLER IS 176 DEG F (80 DEG C).NOTE
The minimum cure time is one hour.Option 2: Apply the sealant (CoMat 08-024 SEALANT or CoMat 08-142 POLYSULPHIDE COMPOUND).
Refer to Figure.

CAUTION
THE MAXIMUM TEMPERATURE WHICH CAN BE USED TO CURE THE SEALANT IS 120 DEG F (49 DEG C).
CAUTION
DO NOT OPERATE WITHOUT SAFETY GOGGLES AND OTHER GUARD EQUIPMENT. FLYING PARTICLES CAN CAUSE INJURY.NOTE
The minimum cure time is 1.5 hours. Sealant cure times with relative humidity of 50 percent.Blend the filler to the contours.
SUBTASK 72-32-85-360-079 Apply Filler Material
A step is acceptable if less than 0.02 in. (0.5 mm).
Refer to Figure.
Examine the surface of repaired area.
SUBTASK 72-32-85-220-105 Examine the Repair Area
Figure: Repair Details and Dimensions
Repair Details and Dimensions

Figure: Repair Details and Dimensions
Repair Details and Dimensions

