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 70-31-02-310-501-004 Argonarc Welding Repairs - Post Weld Heat Treatment
General
This TASK gives general guidance on the post weld heat treatments necessary for different materials. The specific heat treatments will be given in the Engine Manual. If the information in this TASK is different from that in the Engine Manual use the heat treatment specified in the Engine Manual. Refer to the SPM TASK 70-37-00-370-501 for the control of the heat treatment and to the SPM TASK 70-31-02-310-501-001 for other welding related TASKS.
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
NONEConsumables, Materials and Expendables
NONESpares
NONESafety Requirements
WARNING
Procedure
These heat treatments are primarily for stress relieving treatments to decrease the risk of distortion.
Group
Material and Code
Post Weld Heat Treatment
1G
Al 5Cu 1.5Ni
Stress relieve at 410 deg F (210 deg C) for 2 Hours.
1H
Al 2.5Si 1.1Cu 1.1Fe 0.9Ni 0.2Ti
Stress relieve at 338 deg F (170 deg C) for 2 Hours.
SUBTASK 70-31-02-370-016 Aluminum Alloys
After the heat treatment it may be necessary to remove any Alpha case formed on the Titanium. Even parts treated in vacuum or inert atmosphere can develop an Alpha case if the temperature is high enough. The level of Alpha case will depend on the temperature and quality of the protective atmosphere and the total surface area of Titanium in the furnace. Keeping the temperature below 1112 deg F (600 deg C) will minimize the build up of alpha case.
The need for descaling will be specified in the Engine Manual. Descaling may be carried out using abrasive blasting or chemical etching. Refer to the SPM TASK 70-11-09-300-503.
Group
Material and Code
Post Weld Heat treatment
Comments
3A
Commercial Purity Titanium (IMI 115, IMI 125, IMI 130, IMI 160)
Stress relief not generally required. (If stress relief is necessary, heat at 1112 deg F (600 deg C) for 1 Hour).
If descaling will be a problem use 977 deg F (525 deg C) for 30 minutes
3B
Ti 2.5Cu (IMI 230) Aging specifications.
Age at 752 deg F (400 deg C) for 8 Hours + 887 deg F (475 deg C) for 8 Hours to develop full properties in the weld metal.
3B
Ti 2.5Cu (IMI 230) Non Aging specifications.
Stress relief not generally required. (If stress relief is necessary, heat at 1112 deg F (600 deg C) for 30 minutes).
3C
Ti 6Al 4V (Ti64, IMI 318)
Stress relief not generally required. (If stress relief is necessary, heat at 1112 deg F (600 deg C) for 1 Hour.
Alternatively, stress relieve at 1022-1292 deg F (550-700 deg C) for 30 minutes may be used. Below 1112 deg F (600 deg C) the effectiveness of the stress relieve treatment is reduced. Above 1112 deg F (600 deg C) oxide film growth is significantly increased.
3E
Ti 5.5Al 3.5Sn 3Zr 1Nb (Ti 5331 IMI 829)
Stress relieve at 1157 deg F (625 deg C) for 2 Hours.
3G
Ti 6Al 4Zr 2Mo 2Sn (Ti 6242)
Stress relieve at 1103 deg F (595 deg C) for 4 Hours.
SUBTASK 70-31-02-370-017 Titanium Alloys

CAUTION
CONTAMINANTS CAN CAUSE CORROSION OF TITANIUM WHEN IT IS HEAT TREATED. PARTS MUST BE CLEANED FULLY BEFORE HEAT TREATMENT.Heat treatment parameters for some Group 5 materials are given in the table as follows:
Group
Material and Code
Post Weld Heat Treatment
Comment
5A
18-8 Stainless steel
18-11 Stainless steel
23-11 Stainless steel - Crown Max
Not required
5D
(See notes at the end of the table)
Jethete M152
EAK
EBP
ECP
EAP
EXY
EBJ
EAK EBP
Heat at 1202 deg F (650 deg C) for 1 Hour.
ECP
Heat at 1202 deg F (650 deg C) for 1 Hour.
EAP
Heat at 1057 deg F (575 deg C) for 3 hours.
EXY
Heat at 635 deg F (335 deg C) for 3 Hours.
EBJ
Heat at 1031 deg F (555 deg C) for 2 Hours.
Jethete M190
EAD
EAD
Heat at 1202 deg F (650 deg C) for 1 Hour.
FV 535
EAX
EBH
EEJ
EAX EEJ
Heat at 1130 deg F (610 deg C) for 1 Hour.
EBH
Heat at 1076 deg F (580 deg C) for 2 Hours.
NOTE
The 3 Alpha codes quoted are for the most common types for other codes refer to the material specification for details of the heat treatment.Components must be tempered before further work is carried out.The mechanical properties of the Group 5D materials are determined by the tempering temperature so it is important to use the correct temperature for the material code specified.
SUBTASK 70-31-02-370-018 Corrosion Resistant Steels

CAUTION
GROUP 5D MATERIALS ARE HARD AND BRITTLE IN THE WELDED CONDITION. THEY MUST BE HANDLED WITH CARE IN THE "AS WELDED" CONDITION.Heat treatment parameters for some Group 6 materials are given in the table as follows:
Group
Material
Pre weld heat treatment
Post weld heat treatment
6A
Nimonic 75
None
6B
Nimonic 80A
Heat treat at 1688 deg F (920 deg C) for 1 Hour.
See the SPM TASK 70-31-02-310-501-009 for the specific appendix for Nimonic 80A.
Nimonic 90
Heat at 1976 deg F (1080 deg C) for 30 minutes.
(Optional heat at 1742 deg F (950 deg C) for 20 minutes). Heat at 1292 deg F (700 deg C) for 16 Hours, or at 1382 deg F (750 deg C) for 4 Hours.
6D
C263
Heat at 1472 deg F (800 deg C) for 2 Hours.
Inconel 901
Heat at 1364 deg F (740 deg C) for 4 Hours.
6G
Haynes 25
None
6P
Inconel 718
Heat at 1796 deg F (980 deg C) for 5 Minutes (treatment is optional).
(Heat at 1796 deg F (980 deg C) for 5 minutes Optional).
Heat at 1382 deg F (750 deg C) for 4 Hours, then heat at 1202 deg F (650 deg C) for 4 Hours
or
Heat at 1328 deg F (720 deg C) for 8 Hours and then at 1148 deg F (620 deg C) for 8 Hours (for castings).
Inconel 718
Compressor blades
Heat at 1400 deg F (760 deg C) for 2 Hours and then at 1148 deg F (620 deg C) for 4 Hours.
Optional preweld heat treatment is to improve weldability and weld mechanical properties.
Optional post weld heat treatment is to improve the weld mechanical properties.
SUBTASK 70-31-02-370-019 Heat Resisting Alloys
