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 70-37-28-370-501 Stress-Relief For Martensitic Corrosion Resistant Steels
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
NONEConsumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 03-010 ARGON GAS | LOCAL | CoMat 03-010 | ||
| CoMat 03-120 HELIUM GAS | 0B434 | CoMat 03-120 | ||
| CoMat 03-138 HYDROGEN GAS (PROTECTIVE ATMOSPHERE) | 0B434 | CoMat 03-138 |
Spares
NONESafety Requirements
WARNING
Procedure
Increase the temperature of the part to 1775 to 1825 deg F (968 to 996 deg C) and hold for not less than one hour. CoMat 03-010 ARGON GAS standard purity, CoMat 03-120 HELIUM GAS, CoMat 03-138 HYDROGEN GAS (PROTECTIVE ATMOSPHERE), argon or helium + hydrogen, vacuum, vacuum + fast cool, vacuum + hydrogen + argon or helium, exothermic or endothermic is an acceptable atmosphere. Semi-machined parts can be austenitized in air when subsequent machining will remove at least 0.010 inch (0.254mm) from previously machined surfaces. The rate at which the temperature is increased is optional.
Decrease the temperature of the part to below 300 deg F (149 deg C). The rate at which the part decreases in temperature between 1650 deg F (899 deg C) and 1000 deg F (538 deg C) is to be 35 deg F (19 deg C)/minute or faster with 50 deg F (28 deg C)/minute or faster recommended. Any convenient rate can be used below 1000 deg F (538 deg C). Subsequent tempering should be done as soon as possible.
Austenitizing.
It is permitted to harden and/or temper the part again when the hardness requirement is not met in the initial heat treatment.
ALLOY TEMPERING TEMPERATURES
Hardness Range
AMS 5613/5504 CRES
(AISI 410)
AMS 5616/5508 CRES
(Greek Ascoloy)
25 to 33 HRC
1060 to 1090 deg F
(571 to 588 deg C)
1175 to 1225 deg F
(635 to 663 deg C)
30 to 38 HRC
1005 to 1035 deg F
(541 to 557 deg C)
1085 to 1135 deg F
(585 to 613 deg C)
32 to 38 HRC
Not Applicable
1085 to 1135 deg F
(585 to 613 deg C)
35 HRC Minimum
450 to 600 deg F +/- 10 deg F
(232 to 316 deg C +/- 5 deg C)
As required by Specific Repair
Not Applicable
35 to 40 HRC
Not Applicable
1080 to 1110 deg F
(582 to 599 deg C)
45 HRC Minimum
Not Applicable
450 to 600 deg F +/- 10 deg F
(232 to 316 deg C +/- 5 deg C)
As required by Specific Repair

CAUTION
BE CAREFUL WITH AUSTENIZED PARTS. AUSTENIZED PARTS ARE BRITTLE AND BREAK EASILY.
CAUTION
KEEP THE PARTS CLEAN AND DRY UNTIL AFTER TEMPERING TO PREVENT CRACKING. IT IS RECOMMENDED THAT YOU TEMPER PARTS LESS THAN 24 HOURS AFTER AUSTENITIZING (LESS THAN 12 HOURS IS BETTER).Tempering.
SUBTASK 70-37-28-370-001 Stress-relieve Martensitic Corrosion Resistant Steels
