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 70-33-20-300-503 Anodic Coatings For Aluminium Base Alloys - Chromic Acid Process
Safety Precautions
Chromic acid solutions
General
Chromic acid anodizing gives a gray coating to aluminium and its alloys. When it is not sealed, it gives a very good bond for organic finishes. When sealed in boiling water - (Or a dichromate solution), it gives protection against corrosion.
NOTE
NOTE
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
NONEConsumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 07-014 STOPPING-OFF LACQUER | LOCAL | CoMat 07-014 | ||
| CoMat 01-076 METHYL ETHYL KETONE | LOCAL | CoMat 01-076 |
Spares
NONESafety Requirements
WARNING
WARNING
WARNING
WARNING
WARNING
WARNING
WARNING
WARNING
CAUTION
Procedure
Clean the parts with kerosine - (Refer to the SPM TASK 70-11-14-300-503).
When necessary, remove the grease from the parts - (Refer to the SPM TASK 70-11-01-300-503).
When necessary, apply the CoMat 07-014 STOPPING-OFF LACQUER to the parts.
NOTE
Suspenders with titanium contact faces are recommended; although aluminium is also satisfactory.Suspenders made from aluminium must have the anodic coating removed, as specified in the SPM TASK 70-33-58-330-501. All contact faces must be cleaned, with a wire-brush, before they are used again.Jigs that have become defective, because of continuous use, must be discarded.If the Engine Manual instructions do not recommend a special suspender, attach the parts with aluminium wire; but always make sure that there is a good electrical connection, between the wire and the part. The wire must always be discarded, after use.Remove the grease from the parts - (Refer to the SPM TASK 70-11-01-300-503), then dry in air; to remove the remaining solvent.
Preparation of parts.
NOTE
The solution must be constantly mixed, by a pump or with clean compressed air, to make sure that the temperature is kept constant, through the full bath.Put the parts fully into the chromic anodizing solution - (Refer to SUBTASK 70-33-20-100-001), at a temperature of 100 to 108 deg F (38 to 42 deg C). Install the parts so that air bubbles can not occur, then connect them to the positive pole of the DC electrical power supply; to make a good electrical contact.
With the solution temperature kept at 77 to 86 deg F (25 to 30 deg C), apply the current so that the voltage across the bath is continuously increased - (In maximum steps of 5 volts, from 0 to 40 volts), during the first 10 minutes. Keep at 40 volts for 30 minutes then decrease, to zero volts, during the subsequent minute.
NOTE
When specified in the Engine Manual the alternative anodizing procedure, that follows, can be applied. This procedure is better for aluminium alloys that are close to the maximum permitted alloy structure - (That is, a total of 7 percent copper, nickel and iron; or more than 5 percent copper).Apply the current so that the voltage across the bath is increased - (In maximum steps of 5 volts, from 0 to 40 volts), during the first 10 minutes. Keep at 40 volts for 20 minutes then continuously increase, from 40 to 50 volts, during the subsequent 5 minutes. Keep at 50 volts for 5 minutes then decrease, to zero volts, during the subsequent minute. These times are the minimum times permitted.
NOTE
Highly porous aluminium parts - (For example castings) are better if put into clean, cold, water - (Or alternatively, hot water at a temperature of 158 deg F (70 deg C)) for a maximum of 1 hour, to make sure that all the solution is removed.Remove the parts from the solution, quickly drain, then fully flush in a clean, cold, water flow, until all the solution is removed.
NOTE
When paint is to be applied to the anodic coating - (That is, when specified in the Engine Manual), the full procedure must be completed in less than 16 hours.Put the parts fully into clean, hot, water at a maximum temperature of 158 deg F (70 deg C). Remove the parts and dry with clean, dry, compressed air.
Chromic anodize the parts.
Let the parts become cool. When necessary, remove the stopping-off lacquer with CoMat 01-076 METHYL ETHYL KETONE.
NOTE
When specified in the Engine Manual, dichromate sealing must be done immediately after Step above.Dichromate seal the parts.
Examine the parts.
NOTE
A chromate conversion coating - (Refer to the SPM TASK 70-38-02-300-503) can be used to give protection against corrosion; to small areas where the anodic coating is damaged, or is not complete.The anodic coating must only be removed from the parts, when specified in the Engine Manual.
SUBTASK 70-33-20-300-001 Anodic Coating Procedure
