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 70-33-66-300-503 Procedure Used In The Stripping Of MCrAlY Protective Surface Coatings From Nickel And Cobalt Alloys
General
The SPM TASK 70-33-66-300-503 is approved to:
Strip (remove) IAE 33, IAE 68, IAE 258, IAE 261, IAE 264, IAE 265, IAE 266, IAE 268, IAE 270, IAE 276, IAE 286, IAE 36095, IAE 36261, IAE 36301, IAE 36302, IAE 36309, IAE 36330, IAE 36395, IAE 36841, and IAE-IM-6260 coatings from IAE 647, IAE 653, IAE 654, IAE 655, IAE 657, IAE 663, IAE 1019, IAE 1038, IAE 1422, IAE 1426, IAE 1435, IAE 1447, IAE 1449, IAE 1451, IAE 1455, IAE 1480 and IAE 1484 parts.
Strip IAE 254-1 coating from IAE 1038 parts.
Strip IAE 252 coating from IAE 647 and IAE 653 parts.
Strip IAE 53-5 coating from IAE 1038 parts.
NOTE
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
NONEConsumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 02-021 MASKING WAX COMPOUND | 59460 | CoMat 02-021 | ||
| CoMat 02-038 MASKING WAX COMPOUND (HIGH TEMPERATURE) | IE514 | CoMat 02-038 | ||
| CoMat 02-067 STRIPPABLE COATING | 71410 | CoMat 02-067 | ||
| CoMat 02-226 WATERBORNE MASKANT | 01TB5 | CoMat 02-226 | ||
| CoMat 02-259 CHEMICAL MASKANT | IE350 | CoMat 02-259 | ||
| CoMat 02-370 MASKING WAX COMPOUND | E0129 | CoMat 02-370 | ||
| CoMat 02-388 URETHANE ACRYLIC, UV LIGHT-CURABLE | 46733 | CoMat 02-388 | ||
| CoMat 02-389 MASKANT, AIRFOIL, UV LIGHT-CURABLE | 46733 | CoMat 02-389 | ||
| CoMat 05-192 ALUMINUM OXIDE GRIT | IE531 | CoMat 05-192 | ||
| CoMat 05-046 ALUMINUM OXIDE GRIT | 62596 | CoMat 05-046 |
Spares
NONESafety Requirements
WARNING
Procedure
This subtask is deleted. Refer to Step and SUBTASK 70-33-66-110-002.
SUBTASK 70-33-66-300-001 Stripping Procedure
Remove the grease and oil by the SPM TASK 70-11-03-300-503.

CAUTION
CONTAMINATION OF THE GRIT BLAST MEDIA WITH COATING OXIDES AND PARTICLES WILL OCCUR IF YOU DO COATING REMOVAL PROCEDURES IN THE SPM TASK 70-34-18-380-501. COATING ADHESION WILL BE UNSATISFACTORY IF YOU DO THE SPM TASK 70-34-18-380-501 PRE-COATING SURFACE PREPARATION WITH GRIT BLAST MEDIA THAT HAS THIS CONTAMINATION.Dry grit blast the areas that are to be stripped to remove oxides from the surface of the coating by the SPM TASK 70-12-09-120-501.
For parts other than turbine airfoils, it is permitted to do the subsequent procedure to remove the ceramic top coat from multiple layer coatings that have a ceramic coat.
Abrasive blast with CoMat 05-192 ALUMINUM OXIDE GRIT or CoMat 05-046 ALUMINUM OXIDE GRIT 60 grit aluminum oxide by the procedure in the SPM TASK 70-12-09-120-501 to remove the ceramic top coat. Refer to the SPM TASK 70-12-09-120-501, SUBTASK 70-12-09-120-501.
It is not permitted to use abrasive blast to remove coatings that are in direct contact with (that is, the part material), such as hardface coatings or bond coatings, because too much erosion of the substrate can occur and cracks will be more difficult to find during FPI.
Although the SPM TASK 70-34-18-380-501 specifies to use 60 grit aluminum oxide, it is not permitted to do coating removal procedures with blasting equipment that you use for the SPM TASK 70-34-18-380-501 preparation prior to coating. Contamination in the SPM TASK 70-34-18-380-501 abrasive grit with removed coating material will cause contamination of part surfaces and subsequent coating bond problems.
CoMat 02-038 MASKING WAX COMPOUND (HIGH TEMPERATURE) High temperature masking wax compound.
Before you apply a wax mask, apply CoMat 02-067 STRIPPABLE COATING to cooling holes, slots, edges and other part features that must retain (keep) coating to close (small) tolerances.
Before you apply a wax mask, apply CoMat 02-067 STRIPPABLE COATING to cooling holes, slots, edges and other part features that must retain (keep) coating to close (small) tolerances.
Before you apply a wax mask, apply CoMat 02-067 STRIPPABLE COATING to cooling holes, slots, edges and other part features that must retain (keep) coating to close (small) tolerances.

CAUTION
IF YOU DO NOT CORRECTLY APPLY THE MASKING ON THE HARDFACE THERMAL SPRAY COATINGS, THIS PROCEDURE WILL CAUSE DAMAGE TO THE COATING AND MAKE IT NECESSARY TO REPLACE THE COATING.Apply a mask to the part areas that are not to be stripped. Use one of the mask materials in the subsequent list and the applicable procedure in the SPM TASK 70-38-24-300-503.
SUBTASK 70-33-66-180-001 Preparation Procedure
When you use this procedure to remove IAE 36095, or IAE 36361, or IAE 36395, or other platinum aluminide coatings, it is permitted to decrease the minimum solution temperature limit to room temperature. The reaction between the solution and the coating is exothermic, which will cause the solution temperature to increase during the strippping operation, and thus it will be necessary to make sure that the solution temperature does not increase to more than 160 deg F (71 deg C). Solution temperatures higher than 125 deg F (52 deg C) will increase very much the reaction rate.
Put the parts fully in Solution Code 90 Stripping Solution at 140 to 160 deg F (60 to 71 deg C) for two hours maximum.
Dry grit blast the parts to remove oxidation or smut on the parts. Refer to the SPM TASK 70-12-09-120-501.

CAUTION
IF THE SOLUTION DOES NOT HAVE SUFFICIENT AGITATION, THE SOLUTION CAN CAUSE PITS IN LOCAL AREAS OF THE PARTS.Use mechanical agitation (corrosion resistant stainless steel solution pump, mixer, or up/down lift) to cause continuous movement of the solution while the parts are in the stripping solution.
Put the parts fully in Solution Code 90 Stripping Solution at 140 to 160 deg F (60 to 71 deg C) for 5 minutes maximum.

CAUTION
IF THE TOTAL TIME IN THE STRIPPING SOLUTION IS MORE THAN FIVE HOURS, THE SOLUTION WILL CAUSE TOO MUCH STOCK LOSS (REMOVAL OF PART MATERIAL).If there is coating remaining on the parts, do the steps above in this procedure again until the coating is fully removed, but the total time in the stripping solution must not be more than five hours.
Remove the mask materials. Use the SPM TASK 70-38-24-300-503.
SUBTASK 70-33-66-300-002 Stripping Procedure
