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 72-31-11-100-001 Annulus Filler - Clean The Annulus Filler
Effectivity
FIG/ITEM | PART NO. |
|---|---|
01-100 | 5A6533 |
01-100 | 5A0353 |
01-100 | 5A1459 |
01-100 | 5A1611 |
01-100 | 5A1638 |
01-100 | 5A1710 |
01-100 | 5A1750 |
01-100 | 5A1752 |
01-100 | 5A1753 |
01-100 | 5A1854 |
General
This TASK gives the procedure to clean the annulus fillers.
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.
Cleaning - General Information the SPM TASK 70-10-00-100-501
NOTE
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
NONEConsumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 01-016 PHOSPHORIC ACID H3PO4 | LOCAL | CoMat 01-016 | ||
| CoMat 01-023 CHROMIUM TRIOXIDE CrO3(CHROM.ACID) | LOCAL | CoMat 01-023 | ||
| CoMat 01-171 RUBBER DIGESTER | LOCAL | CoMat 01-171 | ||
| CoMat 01-339 ALKALI CLEANER (GENERAL PURPOSE) | LOCAL | CoMat 01-339 | ||
| CoMat 02-001 ADHESIVE TAPE (MASKING) | LOCAL | CoMat 02-001 | ||
| CoMat 02-099 LINT-FREE CLOTH | LOCAL | CoMat 02-099 |
Spares
NONESafety Requirements
NONEProcedure
Remove the soft dirt and the dust. Refer to the SPM TASK 70-11-26-300-503
SUBTASK 72-31-11-110-051 Remove the Soft Dirt and the Dust
Soak until the rubber is removed. Use CoMat 01-171 RUBBER DIGESTER.
Soak to remove the seals and bumper pads. Refer to the SPM TASK 70-11-04-300-503
SUBTASK 72-31-11-110-052 Remove the Seals and Bumper Pads
Remove the grease. Refer to the SPM TASK 70-11-03-300-503
Remove the paint. Refer to the SPM TASK 70-11-60-110-503
SUBTASK 72-31-11-110-104 Remove the Paint
Remove the dry film lubricant. Refer to the SPM TASK 70-11-29-300-503
SUBTASK 72-31-11-110-054 Remove the Dry Film Lubricant (PL 237)
NOTE
Do this procedure only if more cleaning is required to complete the inspection requirement.Do this procedure if SUBTASK 72-31-11-110-107 is required to remove the red primer paint.Remove the locating pin. Refer to TASK 72-31-11-300-005 (REPAIR-005) VRS1010
Remove the seals and bumper pads. Refer to Step
Remove the screw thread insert. Refer to TASK 72-31-11-300-014 (REPAIR-014) VRS1013 or TASK 72-31-11-300-023 (REPAIR-023) VRS1017
Remove the dry film lubricant. Refer to Step
SUBTASK 72-31-11-110-105 Prepare the Anodize Coating for Removing

CAUTION
CARE MUST BE TAKEN NOT TO DAMAGE PARENT MATERIAL BY EXCESSIVE BLAST.NOTE
Do this procedure only if more cleaning is required to complete the inspection requirement.Anodize coating must be removed if this procedure is done. Refer to SUBTASK 72-31-11-110-073 and SUBTASK 72-31-11-110-106.Mask the area where the paint is not applied.
Remove the paint. Refer to the SPM TASK 70-12-06-120-501
SUBTASK 72-31-11-110-107 Remove the Paint (Red Primer)
NOTE
Do this procedure only if more cleaning is required to complete the inspection requirement.This SUBTASK 72-31-11-110-073 is an alternative to SUBTASK 72-31-11-110-106.Do this procedure if SUBTASK 72-31-11-110-107 is done to remove the red primer paint.Remove the anodize coating. Refer to the SPM TASK 70-33-58-330-501
SUBTASK 72-31-11-110-073 Remove the Anodize Coating

WARNING
CHROMIC ACID SPRAY IS INJURIOUS IF INHALED, CAUSING ULCERS IN THE NOSE AND IN SOME CASES, PERFORATION OF THE NASAL SEPTUM. CHROMIC ACID SALTS AND SOLUTIONS IN CONTACT WITH THE SKIN MAY CAUSE CHROME SORES. ULCERS MAY BE FORMED IF CHROMIC ACID GETS INTO CUTS AND ABRASIONS.
WARNING
CHROMIC ACID SOLUTION MUST NEVER BE USED UNLESS THE FUME EXTRACTION PLANT IS IN OPERATION AND IS FULLY SERVICEABLE.
WARNING
BARRIER CREAM SHOULD BE APPLIED TO THE HANDS AND FOREARMS BEFORE STARTING WORK.
WARNING
PROTECTIVE GLOVES, OVERALLS, GOGGLES OR FACE VISOR AND SAFETY SHOES OR BOOTS MUST BE WORN.
WARNING
SMOKING AND THE CONSUMPTION OF FOOD NEAR THE CHROMIC ACID BATH ARE PROHIBITED.
WARNING
CUTS AND ABRASIONS, WHICH APPEAR NOT TO BE HEALING READILY SHOULD BE REPORTED, WITHOUT DELAY, TO THE MEDICAL DEPARTMENT.
WARNING
CHROMIC ACID IS STRONGLY OXIDIZING AND ENTAILS SOME FIRE RISK, POSSIBLE SPONTANEOUS COMBUSTION OF ORGANIC MATERIALS, SUCH AS RAGS AND SAWDUST, WHICH HAVE ABSORBED CHROMIC ACID SOLUTION. SUCH CONTAMINATED MATERIALS SHOULD BE IMMERSED IN A SOLUTION OF SODIUM BISULPHATED TO NEUTRALISE THE CHROMIC ACID, THE SOLUTION SHOULD THEN BE DISPOSED OF AS SPECIAL WASTE. THE SOLID MATERIAL SHOULD THEN BE RINSED WITH WATER PRIOR TO DISPOSAL.
CAUTION
THE PARTS MUST ONLY STAY IN THE SOLUTION FOR THE TIMES SPECIFIED IN THE ENGINE MANUAL. THIS IS TO PREVENT INTERGRANULAR ATTACK OR A DECREASE IN FATIGUE STRENGTH.NOTE
Do this procedure only if more cleaning is required to complete the inspection requirement.This SUBTASK 72-31-11-110-106 is an alternative to SUBTASK 72-31-11-110-073.Do this procedure if SUBTASK 72-31-11-110-107 is done to remove the red primer paint.Chromic acid solution.
Soak the part in solution for 10 to 30 minutes, at temperature of 122 to 140 deg F (50 to 60 deg C). Use CoMat 01-339 ALKALI CLEANER (GENERAL PURPOSE) primary cleaner of 15 to 30 per cent volume.

WARNING
OPERATORS MUST WEAR THE PROTECTIVE CLOTHING PROVIDED, INCLUDING RUBBER GLOVES AND EYE PROTECTION.
WARNING
TREAT EYE SPLASHES IMMEDIATELY BY PROLONGED WATER IRRIGATION OF THE EYES AND THEN GET IMMEDIATE MEDICAL TREATMENT.Clean the part.
Soak in the solution for 5 to 15 minutes, at temperature of 176 to 212 deg F (80 to 100 deg C). Make up the solution. Use CoMat 01-023 CHROMIUM TRIOXIDE CrO3(CHROM.ACID) chromium trioxide 2.0 to 3.3 oz/gal (15 to 25 g/l), CoMat 01-016 PHOSPHORIC ACID H3PO4 phosphoric acid 4.7 to 8.0 oz/gal (35 to 60 g/l).
Remove the anodize coating.
NOTE
Make sure that the anodize coating is removed. If it is not removed, go toStepDry.
Phosphoric acid solution.
SUBTASK 72-31-11-110-106 Remove the Anodize Coating
NOTE
Do this procedure if Step is done to remove the red primer paint.Clean and etch the part. Refer to the SPM TASK 70-33-08-100-501, SUBTASK 70-33-08-100-003
SUBTASK 72-31-11-110-108 Clean the Annulus Fillers
