Local Reconditioning of the Abradable Material- Defects less than 0.12 in. (3 mm) deep and 0.50 sq in (3.2 sq cm) [CFMB]
TASK 72-23-00-300-040-A
Local Reconditioning of the Abradable Material- Defects less than 0.12 in. (3 mm) deep and 0.50 sq in (3.2 sq cm)
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
C. Referenced Information
3. Job Set-up
Subtask 72-23-00-941-078-A ** ON A/C NOT FOR ALL
Subtask 72-23-00-320-053-A ** ON A/C NOT FOR ALL
Subtask 72-23-00-410-083-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.04.01 02:41:58 UTC
Local Reconditioning of the Abradable Material- Defects less than 0.12 in. (3 mm) deep and 0.50 sq in (3.2 sq cm)
WARNING:
BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
1. Reason for the JobSelf explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | ACCESS PLATFORM 1M (3 FT)-ADJUSTABLE |
| No specific | 1 | HEAT SOURCE - RADIANT |
| No specific | AR | MAT - PROTECTIVE |
| No specific | AR | SPATULA - NON METALLIC |
| No specific | AR | VACUUM CLEANER |
| No specific | AR | WARNING NOTICE(S) |
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.CP1039) | acetone |
| (Material No.CP1041) | isopropyl alcohol |
| (Material No.CP2011) | stoddard solvent |
| (Material No.CP2239) | 3M 301D |
| (Material No.CP2297) | RTV 147 A |
| (Material No.CP2298) | Catalyst 147 B |
| (Material No.CP2559) | ardrox 552 |
| (Material No.CP2560) | turco ind 79 |
| (Material No.CP2566) | mag-chem teksol |
| (Material No.CP2584) | degreasol 99 R |
| (Material No.CP2656) | mag-chem skysol |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 72-21-00-000-005-A | Removal of the Spinner Front Cone |
| TASK 72-21-00-000-006-A | Removal of the Spinner Rear Cone |
| TASK 72-21-00-000-007-A | Removal of the Fan Rotor Blades |
| TASK 72-21-00-400-005-A | Installation of the Spinner Front Cone |
| TASK 72-21-00-400-006-A | Installation of the Spinner Rear Cone |
| TASK 72-21-00-400-007-A | Installation of the Fan Rotor Blades |
Subtask 72-23-00-941-078-A ** ON A/C NOT FOR ALL
A. Safety Precautions
(1) On the center pedestal, on the ENG panel 115VU:
(a) Put a WARNING NOTICE(S) to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure.
(3) On the overhead maintenance panel 50VU:
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off.
(b) Put a WARNING NOTICE(S) to tell persons not to energize the FADEC 1(2).
Subtask 72-23-00-010-089-A ** ON A/C NOT FOR ALL (1) On the center pedestal, on the ENG panel 115VU:
(a) Put a WARNING NOTICE(S) to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure.
(3) On the overhead maintenance panel 50VU:
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off.
(b) Put a WARNING NOTICE(S) to tell persons not to energize the FADEC 1(2).
B. Get Access
(1) Put an ACCESS PLATFORM 1M (3 FT)-ADJUSTABLE in position.
(2) Install MAT - PROTECTIVE in the lower half of the inlet cowl.
(3) Remove the spinner front cone (Ref. AMM TASK 72-21-00-000-005).
(4) Remove the spinner rear cone (Ref. AMM TASK 72-21-00-000-006).
(5) Remove a sufficient number of fan blades to get access to repair area (Ref. AMM TASK 72-21-00-000-007).
4. Procedure(1) Put an ACCESS PLATFORM 1M (3 FT)-ADJUSTABLE in position.
(2) Install MAT - PROTECTIVE in the lower half of the inlet cowl.
(3) Remove the spinner front cone (Ref. AMM TASK 72-21-00-000-005).
(4) Remove the spinner rear cone (Ref. AMM TASK 72-21-00-000-006).
(5) Remove a sufficient number of fan blades to get access to repair area (Ref. AMM TASK 72-21-00-000-007).
Subtask 72-23-00-320-053-A ** ON A/C NOT FOR ALL
A. Prepare the Repair Area
(1) Remove the damaged area from the abradable shroud, until only an area without damage is there.
(3) Blow the dust out of the shroud or VACUUM CLEANER.
Subtask 72-23-00-110-052-A ** ON A/C NOT FOR ALL (1) Remove the damaged area from the abradable shroud, until only an area without damage is there.
NOTE: All oil contaminated areas must be removed.
(2) Make the surface of the repair area rough with an 3M 301D (Material No.CP2239) (3) Blow the dust out of the shroud or VACUUM CLEANER.
B. Degrease the Area
(1) Clean the area to be repaired with acetone (Material No.CP1039) or stoddard solvent (Material No.CP2011) or ardrox 552 (Material No.CP2559) or turco ind 79 (Material No.CP2560) or mag-chem teksol (Material No.CP2566) or degreasol 99 R (Material No.CP2584) or mag-chem skysol (Material No.CP2656) or isopropyl alcohol (Material No.CP1041) .
Subtask 72-23-00-340-051-A ** ON A/C NOT FOR ALL (1) Clean the area to be repaired with acetone (Material No.CP1039) or stoddard solvent (Material No.CP2011) or ardrox 552 (Material No.CP2559) or turco ind 79 (Material No.CP2560) or mag-chem teksol (Material No.CP2566) or degreasol 99 R (Material No.CP2584) or mag-chem skysol (Material No.CP2656) or isopropyl alcohol (Material No.CP1041) .
C. Prepare the Base and Hardener for the Repair
(2) Stir the mixture by hand or mechanically until it becomes a homogenous compound.
Subtask 72-23-00-350-052-A ** ON A/C NOT FOR ALL WARNING:
PUT ON PROTECTIVE GLOVES WHEN YOU USE THE BASE AND HARDENER. IF YOU DO NOT OBEY THIS PRECAUTION, INJURY TO PERSONS OR DAMAGE TO EQUIPMENT CAN OCCUR.
(1) Mix, by weight, 100 parts of the RTV 147 A (Material No.CP2297) and 10 parts of the Catalyst 147 B (Material No.CP2298) . (2) Stir the mixture by hand or mechanically until it becomes a homogenous compound.
NOTE: The compound has a pot life of 2 hours after mixing, at ambient temperature.
(3) Apply the compound with a SPATULA - NON METALLIC. Lighthy hit the compound to remove the air bubbles (if any). NOTE: It is permitted to apply multiple layers of compound. Each layer can have a maximum depth of 0.12 in. (3 mm), if you obey the compound cure time between applications. Layers can be combined to get a total depth of 0.31 in. (8 mm).
D. Cure the Compound with a HEAT SOURCE - RADIANT and obey the curing cycle which follows:
(1) 1 hour at 210 deg.F (98.9 deg.C).
(2) 1/2 hour at 300 deg.F (150 deg.C).
Subtask 72-23-00-320-054-A ** ON A/C NOT FOR ALL (1) 1 hour at 210 deg.F (98.9 deg.C).
(2) 1/2 hour at 300 deg.F (150 deg.C).
E. Complete the Repair as follows:
(1) Make sure the cured compound is constant in color. Make sure it does not contain air bubbles.
(2) Use an 3M 301D (Material No.CP2239) to make the repaired surface smooth with all adjacent areas of the abradable shroud.
(3) Clean the repair area and the inlet cowl with a VACUUM CLEANER.
5. Close-up(1) Make sure the cured compound is constant in color. Make sure it does not contain air bubbles.
(2) Use an 3M 301D (Material No.CP2239) to make the repaired surface smooth with all adjacent areas of the abradable shroud.
(3) Clean the repair area and the inlet cowl with a VACUUM CLEANER.
Subtask 72-23-00-410-083-A ** ON A/C NOT FOR ALL
A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the fan blades (Ref. AMM TASK 72-21-00-400-007).
(3) Install the spinner rear cone (Ref. AMM TASK 72-21-00-400-006).
(4) Install the spinner front cone (Ref. AMM TASK 72-21-00-400-005).
(5) Remove the protective mats from the inlet cowl.
(6) Remove the access platform(s).
(7) Remove the WARNING NOTICE(S).
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Install the fan blades (Ref. AMM TASK 72-21-00-400-007).
(3) Install the spinner rear cone (Ref. AMM TASK 72-21-00-400-006).
(4) Install the spinner front cone (Ref. AMM TASK 72-21-00-400-005).
(5) Remove the protective mats from the inlet cowl.
(6) Remove the access platform(s).
(7) Remove the WARNING NOTICE(S).