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 70-38-34-300-503 Application Of Stoving Primer And Enamel (Epoxy type)
General
This process gives the application of the stoving epoxy primer and enamel scheme to parts of various materials (specially magnesium alloys) for protection against corrosion at temperatures up to 429 deg F (220 deg C). The enamel is resistant to engine lubricants, fuels and hydraulic fluids.
NOTE
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
NONEConsumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 02-019 TAPE, ADHESIVE PAPER HEAT RESISTING MASKING | 94960 | CoMat 02-019 | ||
| CoMat 05-020 WATERPROOF SILICON CARBIDE | LOCAL | CoMat 05-020 | ||
| CoMat 05-021 WATERPROOF SILICON CARBIDE | 44197 | CoMat 05-021 | ||
| CoMat 07-062 TWO-PACK EPOXY FINISH, GREY, AIRCRAFT, BS381C 693 | LOCAL | CoMat 07-062 | ||
| CoMat 07-080 TWO-PACK EPOXY PRIMER AND CATALYST | LOCAL | CoMat 07-080 | ||
| CoMat 07-081 EPOXY PRIMER CATALYST | 0AM53 | CoMat 07-081 | ||
| CoMat 07-082 THINNER | LOCAL | CoMat 07-082 | ||
| CoMat 07-086 CHROMATE EPOXY PRIMER | LOCAL | CoMat 07-086 | ||
| CoMat 07-087 EPOXY ENAMEL GREY | LOCAL | CoMat 07-087 | ||
| CoMat 07-088 THINNER | LOCAL | CoMat 07-088 |
Spares
NONESafety Requirements
WARNING
WARNING
WARNING
WARNING
Procedure
Aluminum parts must be annodised, refer to the SPM TASK 70-33-20-100-501, or alocrom treated, refer to the SPM TASK 70-38-02-100-501, and oven dried for 1 hour at 250 to 300 deg F (120 to 150 deg C).
Steel parts must be abrasive blasted, refer to the SPM TASK 70-12-01-120-501. After processing, parts can be oven dried for 1 hour at 250 to 300 deg F (120 to 150 deg C).
The parts must be pre-treated according to their base material as follows:
Vapour degrease the parts, refer to the SPM TASK 70-11-01-100-501.
Stop off the areas which are to be left unvarnished with correct blanking plates, plugs and CoMat 02-019 TAPE, ADHESIVE PAPER HEAT RESISTING MASKING.
NOTE
Obey the viscosity requirements in SUBTASK 70-38-34-100-001.
Prepare the parts.
NOTE
On close tolerance surfaces, spray one coat of primer to give a minimum dry film thickness of 0.0005in. (0.0127 mm) and allow to dry for 15 to 20 minutes.On surfaces where no large thickness of primer is permitted, spray one coat of primer and, using a clean solvent moistened lint-free cloth, wipe off the bulk of the primer.On general surfaces, spray one coat of primer and stand for 3 minutes.
NOTE
It is recommended to remove the masking tape before stoving at 385 deg F (195 deg C).On parts which are to be coated only with primer heat to 385 deg F (195 deg C) in the limits of 375 to 395 deg F (190 to 200 deg C) and maintain this temperature for 1 hour unless specially instructed differently in the Engine Manual.
NOTE
Where static ovens are used, the air drying time immediately before stoving is important. If conveyor ovens are used, the temperature increase is slow and continuous and air drying is not necessary.Where enamelling is to follow, stove the primer by heating the part to 300 deg F (150 deg C) within the limits of 290 to 310 deg F (145 to 155 deg C) and keep this temperature for 30 minutes.
Apply the primer.
Stop-off areas which are not to be enamelled, with applicable plates, plugs or CoMat 02-019 TAPE, ADHESIVE PAPER HEAT RESISTING MASKING.
Spray one coat of CoMat 07-087 EPOXY ENAMEL GREY on to the part and allow it to stand for 3 minutes.
NOTE
When a static oven is used the air drying time must be obeyed. With a conveyer type oven, when the temperature increase is slow and continuous and the stoving cycle is longer, air drying is not necessary.Spray a second coat of CoMat 07-087 EPOXY ENAMEL GREY on to the part to give a minimum dry film thickness of 0.001in. (0.025 mm) and allow to air dry for 15 to 20 minutes.
If the coating is frequently unsatisfactory, strip the paint as given in TASK 70-11-10-300-502 and apply the coating again. If local damage has occurred do the local application as detailed in Step.
NOTE
Obey the viscosity requirements in SUBTASK 70-38-34-100-001.Apply the enamel.
SUBTASK 70-38-34-300-001 Processing - General Application
Rub down the paint surface immediately adjacent to the damaged area, feathering the edges of the paint, using an applicable grade of CoMat 05-020 WATERPROOF SILICON CARBIDE or CoMat 05-021 WATERPROOF SILICON CARBIDE which is given by the roughness of the surface.
Cold liquid degrease the prepared surface as given in the SPM TASK 70-11-14-300-503.
Where possible touch up the damaged surfaces with CoMat 07-086 CHROMATE EPOXY PRIMER and/or CoMat 07-087 EPOXY ENAMEL GREY and stove again.
Using a clean, good quality brush apply one coat of mixed CoMat 07-080 TWO-PACK EPOXY PRIMER AND CATALYST and CoMat 07-081 EPOXY PRIMER CATALYST prepared according to the SPM TASK 70-38-24-100-501 thinned as necessary with CoMat 07-082 THINNER.
Using a clean, good quality brush apply one coat of CoMat 07-062 TWO-PACK EPOXY FINISH, GREY, AIRCRAFT, BS381C 693 prepared according to the SPM TASK 70-38-34-100-501.
When stoving again in not practicable, during or after assembly, touch-up the damaged surfaces as follows.
SUBTASK 70-38-34-300-002 Processing - Local Application
