DMC:V2500-00-70-38-09-00A-609A-DIssue No:001.00Issue Date:2013-03-20
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 70-38-09-300-503 The Procedure Used To Apply An Aluminum Coating
NOTE
To identify the consumable material refer to the PCI.
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
NONEConsumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 03-252 WIRE, SPRAY-ALUMINUM | LOCAL | CoMat 03-252 |
Spares
NONESafety Requirements
NONEProcedure
Use one of the two vapor degrease or the solvent cleaning procedure - (Refer to the SPM TASK 70-11-01-300-503 or SPM TASK 70-11-33-300-503).
Clean the parts.
SUBTASK 70-38-09-340-001 Prepare the Parts to be Aluminized
Use CoMat 03-252 WIRE, SPRAY-ALUMINUM. Alternative consumable materials can be used.
SUBTASK 70-38-09-340-002-001 Apply the Aluminum Coating
NOTE
The metal content of the slurry or the paint must not be less than 99 percent aluminum. A maximum of 5 percent of iron or nickel can be used instead of aluminum.Use a suitable aluminum slurry or paint. This can be applied by spray, brush, or dipping. (Refer to the SPM TASK 70-38-09-100-501).

CAUTION
DO NOT USE A VACUUM AS THE PROTECTIVE ATMOSPHERE. THE ALUMINUM COATING WILL BECOME A GAS AND DISAPPEAR AT THIS TEMPERATURE IN A VACUUM.NOTE
Step C. is not necessary if the increase in temperature in Step is sufficiently slow to give a temperature of 1150 to 1450 deg F (621 to 788 deg C) for 7 to 10 minutes.Prediffuse the parts at 1335 to 1365 deg F (724 to 741 deg C) for 7 to 10 minutes. Use a pure dry hydrogen atmosphere with a dew point of -40 degrees or better. The pure dry hydrogen must have a zero percent oxygen content.
SUBTASK 70-38-09-340-002-003 Apply the Aluminum Coating
