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
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Common Information
TASK 70-38-03-380-501 Apply The Dry Film Lubricants
Table of Contents
Consumable Materials Safety Precautions Introduction | |
Prepare the Surface of the Part | |
Method to Apply the Dry Film Lubricant | |
Dry Film Lubricant Cure for Parts that Can be Heated | |
Dry Film Lubricant Cure for Parts that Cannot be Heated | |
Examine the Layer of Dry Film Lubricant | |
Correct the Defective Layer of Dry Film Lubricant | |
Removal of the Dry Film Lubricant |
Introduction
This TASK specifies the procedure to apply graphite or molybdenum disulfide dry film lubricants. It is permitted to use this procedure only when it is specified by the Engine Manual.
The maximum operation temperature of the graphite-type lubricants is 752 deg F (400 deg C) in oxidizing conditions or 932 deg F (500 deg C) in non-oxidizing conditions.
The maximum operation temperature of the molybdenum disulfide-type lubricants is 572 deg F (300 deg C).
The lubricants are applied in a thin layer. The use of heat cured type of dry film lubricant is preferred. Air drying dry film lubricant must only be used if elevated temperature curing is not possible, or if specifically specified by the Engine Manual.
NOTE
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
NONEConsumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 02-018 BRUSH, PAINT | LOCAL | CoMat 02-018 | ||
| CoMat 05-003 ABRASIVE MEDIUM ALUMINUM OXIDE, 120/220 GRADE | X222X | CoMat 05-003 | ||
| CoMat 05-004 ABRASIVE MEDIUM, ALUMINUM OXIDE, 140/400 GRADE | X222X | CoMat 05-004 | ||
| CoMat 05-156 ALUMINUM OXIDE ABRASIVE | 27715 | CoMat 05-156 | ||
| CoMat 05-198 ALUMINUM OXIDE, 320-GRIT | IE531 | CoMat 05-198 | ||
| CoMat 05-230 ABRASIVE MEDIUM ALUMINUM OXIDE, 280/500 GRADE | C5214 | CoMat 05-230 | ||
| CoMat 07-009 THINNER | K3504 | CoMat 07-009 | ||
| CoMat 10-002 DRY FILM LUBRICANT | LOCAL | CoMat 10-002 | ||
| CoMat 10-003 COLLOIDAL GRAPHITE DRY FILM LUBRICANT | 70079 | CoMat 10-003 | ||
| CoMat 10-004 DRY FILM LUBRICANT | LOCAL | CoMat 10-004 | ||
| CoMat 10-005 COLLOIDAL MOLYBDENUM DISULFIDE IN TOLUENE | LOCAL | CoMat 10-005 | ||
| CoMat 10-106 BONDED LUBRICANT | LOCAL | CoMat 10-106 | ||
| CoMat 10-140 DRY FILM LUBRICANT, MOLYBDENUM DISULFIDE | LOCAL | CoMat 10-140 |
Spares
NONESafety Requirements
WARNING
Procedure
Clean the repair area of the part. Refer to SPM TASK 70-11-03-300-503 or SPM TASK 70-11-26-300-503.
Apply masking tape as necessary to give protection from the abrasive blast to the part surfaces that are adjacent to the areas that needs to be applied with dry film lubricant. Refer to SPM TASK 70-34-18-380-501 for applicable masking tapes.
For steel parts, use CoMat 05-004 ABRASIVE MEDIUM, ALUMINUM OXIDE, 140/400 GRADE, CoMat 05-156 ALUMINUM OXIDE ABRASIVE, or CoMat 05-198 ALUMINUM OXIDE, 320-GRIT. When a surface finish coarser than 70 microinches (1.6 micrometers) is specified, it is permitted to use CoMat 05-003 ABRASIVE MEDIUM ALUMINUM OXIDE, 120/220 GRADE with the specified pressure.
For titanium parts, use CoMat 05-230 ABRASIVE MEDIUM ALUMINUM OXIDE, 280/500 GRADE.
Do the abrasive blast surface preparation of the surfaces that needs to be applied with dry film lubricant. Refer to SPM TASK 70-12-02-120-501 (dry blast) or SPM TASK 70-12-01-120-501 (wet blast), but use the abrasive grit that the applicable repair instructions specify to use. If the applicable repair instructions do not specify the abrasive grit, use the applicable abrasive grit from the subsequent list:
If the Engine Manual specifies to do abrasive blast surface preparation for the areas that needs to be applied with dry film lubricant, do the procedure that follows:
Remove the masking tape. If there are remaining tape adhesive on the part, use SPM TASK 70-11-26-300-503 to remove the remaining adhesive.
If you use a wet abrasive blast procedure to do the abrasive blast surface preparation, use SPM TASK 70-11-03-300-503 to clean the part.
If you use a dry abrasive blast procedure to do the abrasive blast surface preparation, use clean, dry compressed air to blow the remaining abrasive off of the part.
Do the applicable procedure to remove the remaining abrasive from part:
For aluminum parts, use SPM TASK 70-33-20-300-503 to anodize the part, or use SPM TASK 70-38-02-300-503 to apply chromate conversion coating to the repair area.
SUBTASK 70-38-03-120-001 Prepare the Surface of the Part for the Application of the Dry Film Lubricant
Clean the repair area with SPM TASK 70-11-26-300-503.
Mask the part where specified by the Engine Manual. Use a tape from SPM TASK 70-38-24-300-503
Apply by brush the dry film lubricant to produce a thickness of between 0.0001 in. to 0.0003 in. (0.003 mm to 0.008 mm), unless specified differently in the Engine Manual. Use a clean CoMat 02-018 BRUSH, PAINT to apply the dry film lubricant.
To prevent air locks, slowly put the part fully into the lubricant and rotate the part. After a small number of seconds remove the part at a constant rate of 0.20 in. (5.00 mm) every minute. Repeat as necessary to produce a thickness of between 0.0001 in. to 0.0003 in. (0.003 mm to 0.008 mm). If the Engine Manual gives a different thickness of layer then follow the procedure given in the Engine Manual. Let the part become dry for a minimum time of 10 minutes between each layer.
Put the part fully into a diluted mixture of the dry film lubricant. Refer to the manufacturer's instruction for mixture make-up.
Apply the dry film lubricant as specified by the Engine Manual by one of the methods as follows:
SUBTASK 70-38-03-380-004 Method to Apply the Dry Film Lubricants
For CoMat 10-003 COLLOIDAL GRAPHITE DRY FILM LUBRICANT, typically permit the coating to cure for 1 hour before it is touched.
For CoMat 10-005 COLLOIDAL MOLYBDENUM DISULFIDE IN TOLUENE, typically permit the coating to cure for 8 hours before it is touched.
For CoMat 10-106 BONDED LUBRICANT or CoMat 10-140 DRY FILM LUBRICANT, MOLYBDENUM DISULFIDE, typically the coating is dry to touch after 30 minutes and is cured fully after 4 hours.

CAUTION
IF THE ENGINE MANUAL SPECIFIES CURE IN AIR DO NOT HEAT CURE, EVEN WHEN THE LUBRICANT CAN BE HEAT CURED.Let the part dry in air to the manufacturer's instructions.
SUBTASK 70-38-03-380-006 Dry Film Lubricant Cure for Parts that Cannot be Heated (with CoMat 10-003, or CoMat 10-005, or CoMat 10-106, or CoMat 10-140)
Examine the layer of dry film lubricant on the part. Make sure the layer is equal in color on all the surface. The layer must be smooth and bonded correctly to the surface of the part. The layer must not have any cracks or flakes. Refer to the Step to correct any defects found in the layer of dry film lubricant.
SUBTASK 70-38-03-220-001 Examine the Layer of Dry Film Lubricant
Correct any defects found in the layer of dry film lubricant by reapplication of the specified lubricant. Use a clean CoMat 02-018 BRUSH, PAINT to apply the lubricant. Refer to Step.
SUBTASK 70-38-03-380-007 Correct the Defective Layer of Dry Film Lubricant
To remove the layer of dry film lubricant from the part before the heat cure procedure, use CoMat 07-009 THINNER.
SUBTASK 70-38-03-160-001 Removal of the Dry Film Lubricant From Unwanted Areas
