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 70-38-41-380-501 Procedure For Touch-Up Of Diffused Aluminide Coatings On Nickel-Base Alloys
General
This task is a touch-up for the aluminide coat: IAE 73, IAE 252, IAE 273 and IAE 275.
Limits of CoMat 07-177 Aluminum Silicon Paint: Use on turbine hardware
Unless specified differently by the Engine Manual, the subsequent limits apply to the turbine hardware below.
Vanes that are more than the subsequent limits shall have a total replacement of coat.
A maximum of three areas/airfoil (1 square inch or 645 square millimeters combined, with no one area greater than 0.5 square inch or 322 square millimeters) can be repaired in this procedure.
Leading edge, trailing edge, inner platform to airfoil radius and outer platform to airfoil radius can be included in any one repair.
When the blade limits are more than what is in the subsequent list, a total replacement of the coat is necessary.
No repairs are permitted on leading edges and it is recommended that there should be no touch-up repairs on trailing edges.
A maximum of three areas/airfoil (0.5 square inch or 322 square millimeters combined) can be repaired by this procedure on the remaining gaspath surfaces.
Turbine airfoil surfaces
Do not use CoMat 07-177 Aluminum Silicon Paint to overcoat an entire turbine airfoil.
Ceramic coated areas
CoMat 07-177 Aluminum Silicon Paint shall not be painted on, or be permitted to touch, any ceramic coat area of the part because the aluminide coat is harmful to the ceramic bond.
Operator training
Training courses shall be held at regular intervals to make sure that the operating personnel responsible for performing coat operations (furnace operation, setting up of the furnace workload etc.) is familiar with all details of the process. The training shall invariably be documented.
Subsequent heat treatments
Subsequent heat treatments carried out in the scope of the repair process shall be performed in accordance with the repair procedure.
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
NONEConsumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 07-177 Aluminum Silicon Paint | LOCAL | CoMat 07-177 | ||
| CoMat 05-022 ALUMINUM OXIDE ABRASIVE | 62596 | CoMat 05-022 |
Spares
NONESafety Requirements
WARNING
Procedure
Make sure you keep the CoMat 07-177 Aluminum Silicon Paint tightly sealed in the initial container in a cool place when not in use. Shelf life is unlimited, but the solid particles in the slurry will fall (settle) to the bottom of the container.
Before use, stir or agitate the CoMat 07-177 Aluminum Silicon Paint in the initial container to suspend the powder or break up agglomerates. Stir or agitate until all solids are equally dispersed. It is recommended to stir or shake the slurry during use to keep the powder in suspension.
SUBTASK 70-38-41-380-051 Material Preparation, CoMat 07-177 Slurry, Aluminium-Silicon
Aqueous degrease the part. Refer to the SPM TASK 70-11-03-300-503.
Apply masking tape from the SPM TASK 70-34-18-380-501, to areas that are not to be coated. Make sure you apply the mask tape with an overlap of 0.010 in. to 0.100 in. (0.254 mm to 2.540 mm) around the defect.
Component specific blasting data is specified on the operation sheet.
During all operations following the dry abrasive blast in Step, the surfaces to be coated shall be handled with clean gloves only. Contamination by chlorides (hand sweat) shall be avoided.
If the part will not be oxidized by the Oxidizing step in Step, the interval between blasting and coating shall not be more than 8 hours.
Protect the part from dust until the start of the next operation and during the intervals between all subsequent operations in this task.
Dry abrasive blast the surfaces to be coated. Use TASK 70-12-09-120-501 dry grit blast (No. 240 or No. 320 Aluminum Oxide Grit). The grit blast material used shall be either new or used and not contaminated with impurities. This can be obtained with appropriate filters or cyclone systems.
Remove masking
Oxidizing
Apply a masking tape again or mask to the areas that are not to be coat. Make sure you apply the masking tape or mask with an overlap of 0.010 in. to 0.100 in. (0.254 mm to 2.540 mm) around the blasted area.
SUBTASK 70-38-41-380-101 Surface Preparation
If such segregation has taken place and the coating is subjected to diffusion annealing, deposits or speckling may form on the component, which irreversibly damages the component.
If the specialist personnel is uncertain about the exact amount of slurry to be applied in each step, specimens shall be coated prior to and/or during slurry application and inspected.
The CoMat 07-177 Aluminum Silicon Paint shall be applied in steps. In the process, make sure not to apply too much slurry at a time, as this may cause segregation of the constituents of the coating applied.
The areas exposed by dressing shall be covered completely with slurry.
SUBTASK 70-38-41-380-151 Application of Aluminium-Silicon Slurry
A high-quality paint brush shall be used for paint application.
A uniform coat shall be applied by brush onto the component surfaces prepared by Step.
The components shall then be aired at room temperature until the color of the paint has changed from dark grey to light grey or until the paint coat is dry.
NOTE
The color change may be affected by both the temperature and the humidity of the room.
SUBTASK 70-38-41-380-151-001 Coat By Brushing
Spray gun nozzle diameter: 0.020 in. - 0.060 in. (0.508 mm - 1.524 mm).
Working pressure: 1 bar - 3 bar (100 kPa - 300 kPa, 14.503 psi - 43.511 psi).
A uniform coat shall be applied with a spray gun onto the components which have been prepared by Step. Make sure the coating is wet and does not show a sandy structure.
Dry at 60 C - 150 C (140 F - 302 F) for a minimum of 10 minutes.
Apply a second uniform coat with the spray gun.
Dry at 60 C - 150 C (140 F - 302 F) for a minimum of 10 minutes.
If necessary, apply a third uniform coat with the spray gun, then dry at 60 C - 150 C (140 F - 302 F) for a minimum of 10 minutes.
SUBTASK 70-38-41-380-151-002 Coat By Spraying
SUBTASK 70-38-41-220-001 Visual Inspection By The Person Executing The Work
The diffusion heat treatment may be performed in argon or in hydrogen.
Prior to the diffusion heat treatment, the air shall be removed from the retort by flushing with argon, or by evacuation. Heating may commence as soon as an oxygen content of 0.2 percent by volume maximum is attained in the retort.
Before production is commenced, trials shall be carried out to determine the heat treatment temperature and the soaking time needed to produce the specified coat thickness on the component being processed.
Heat treatment temperatures: 870 C - 900 C (1598 F - 1652 F).
Typical soaking times: 2 hours - 4 hours.
SUBTASK 70-38-41-370-051 Diffusion Heat Treatment
Use one of the subsequent procedures to remove (clean off) undiffused powdery residues and oxide film.
Scrub with a stiff brush and water, and then dry with a blast of shop air.
Blasting of the coated surfaces by SPM TASK 70-12-09-120-501 dry grit blast (No. 240 or No. 320 Aluminum Oxide Grit).
SUBTASK 70-38-41-120-051 Cleaning Of The Components After The Diffusion Heat Treatment
Batch: A group of parts which have been processed together through a complete diffusion heat treatment cycle in the same furnace at the same time.
Definitions
If a specimen from a batch does not fulfill the acceptance limits, the entire batch represented by the specimen in question shall be rejected.
Flaking
Chipping
Blisters
Uncoated areas
Exceptionally speckled appearance (leopard fur)
Unacceptable conditions are:
Steps in the transition area between old and new coating that can be felt with the finger are not permitted.
Components exhibiting visually discernible steps that can, however, not be felt shall be subjected to cosmetic blasting. Following this blasting operation, no steps are permitted.
Surfaces that were covered by adhesive tape or paste have a dull, dark grey appearance, whereas the repair coated areas can be lighter.
The repair coated areas can be surrounded by a light, metallic bright strip several millimeters in width.
Visual Inspection
In the area of the new coat, measured at not less than three places, however outside the old/new coating overlap, refer to the repair procedure.
If the thickness is not specified in the repair it shall be between 0.040 mm and 0.120 mm.
Coating Thickness (measured on a representative process sample by metallographic evaluation)
Acceptance limits
If inspection shows that the diffusion coating is too thin, the components may be recoated provided the coat is satisfactory in all other respects. If possible, the same quality control specimens should be recoated with the components. Otherwise, a component from the same batch shall be used as quality control specimen. The diffusion heat treatment parameters shall be determined by Step.
Imperfect coatings
SUBTASK 70-38-41-200-051 Quality Assurance And Process Inspection
