SAE MA1943A
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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NUTS, SELF-LOCKING, UNS N07001, 760 DEGREE C, 1100 MPA AND 1210 MPA, PROCUREMENT SPECIFICATION FOR, METRIC
Hardcopy , PDF
15-10-2019
English
01-01-2012
1. SCOPE
2. REFERENCES
3. TECHNICAL REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PREPARATION FOR DELIVERY
6. ACKNOWLEDGMENT
7. REJECTIONS
8. NOTES
APPENDIX A - MEASUREMENT OF PERPENDICULARITY
VARIATION OF THE BEARING SURFACE
APPENDIX B - WRENCH TORQUE TEST
APPENDIX C - PUSH OUT TEST
APPENDIX D - TORQUE OUT TEST
APPENDIX E - PERMANENT SET TEST
APPENDIX F - REUSABILITY TEST AT ROOM TEMPERATURE
AFTER 730 DEGREES C BAKE
APPENDIX G - REUSABILITY AT ROOM TEMPERATURE AS
RECEIVED CONDITION
APPENDIX H - THREE-CYCLE TEST AT ROOM TEMPERATURE
APPENDIX J - ACCEPTANCE CRITERIA OF SURFACE
DISCONTINUITIES ON SELF-LOCKING NUTS
Covers aircraft quality self-locking nuts for wrenching (hex, spline) and anchor (plate, gang channel, shank) type of nuts made from a corrosion and heat resistant nickel-base alloy of the type identified under the Unified Numbering System as UNS N07001.
Committee |
E-25
|
DocumentType |
Standard
|
Pages |
46
|
PublisherName |
SAE International
|
Status |
Superseded
|
SupersededBy | |
Supersedes |
SAE MA3378C | BOLTS AND SCREWS, UNS N07001, TENSILE STRENGTH 1210 MPA, THREAD AND FILLET RADIUS ROLLED BEFORE AGING, PROCUREMENT SPECIFICATION, METRIC |
MIL L 7808 : K (1) | LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE |
SAE AMS2645K | FLUORESCENT PENETRANT INSPECTION |
SAE MA 1586 : 2013 | WRENCH CONFIGURATION, 12 SPLINE DRIVE, METRIC |
SAE AMS5707M | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS 57NI - 19.5CR - 13.5CO - 4.3MO - 3.0TI - 1.4AL - 0.05ZR - 0.006B CONSUMABLE ELECTRODE REMELTED OR VACUUM INDUCTION MELTED 1825 TO 1900 DEGREES F (996 TO 1038 DEGREES C) SOLUTION, STABILIZATION, AND PRECIPITATION HEAT TREATED |
SAE MA1566A | GAGING PRACTICE AND GAGE REQUIREMENTS FOR MJ METRIC SCREW THREADS |
MIL-STD-2073-1 Revision E:2008 | STANDARD PRACTICE FOR MILITARY PACKAGING |
SAE AMS5709H | NICKEL ALLOY, CORROSION AND HEAT RESISTANT, BARS AND FORGINGS, 58NI - 19.5CR - 13.5CO - 4.3MO - 3.0TI - 1.4AL - 0.05ZR - 0.006B, CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED, 1975 DEGREE F (1079 DEGREE C) SOLUTION, STABILIZATION, AND PRECIPITATION HEAT TREATED |
SAE AMS5544K | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, SHEET, STRIP, AND PLATE, 57NI - 19.5CR - 13.5CO - 4.2MO - 3.0TI - 1.4AL - 0.05ZR - 0.006B, CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED, ANNEALED |
ASME B46.1 : 2009 | SURFACE TEXTURE (SURFACE ROUGHNESS, WAVINESS, AND LAY) |
NA 0012 : REV 2 | FIXTURE, BEARING SURFACE SQUARENESS TEST, SELF-LOCKING NUTS, METRIC |
SAE MA 1370 : 2012 | SCREW THREADS - MJ PROFILE, METRIC |
SAE AMS2411H | PLATING, SILVER FOR HIGH TEMPERATURE APPLICATIONS |
SAE MA1520A | AREAS FOR CALCULATING STRESS OR LOAD VALUES FOR METRIC MJ EXTERNALLY THREADED FASTENERS |
SAE AMS5706M | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, FORGINGS, AND RINGS, 57NI - 19.5CR - 13.5CO - 4.3MO - 3.0TI - 1.4AL - 0.006B - 0.05ZR, CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED, 1825 TO 1900 DEGREES F SOLUTION HEAT TREATED |
SAE AMS5708L | NICKEL ALLOY, CORROSION AND HEAT-RESISTANT, BARS, WIRE FORGINGS, AND RINGS, 58NI - 19.5CR - 13.5CO - 4.3MO - 3.0TI - 1.4AL - 0.05ZR - 0.006B, CONSUMABLE ELECTRODE OR VACUUM INDUCTION MELTED, 1975 DEGREES F (1079 DEGREES C) SOLUTION HEAT TREATED |
MIL-STD-105 Revision E:1989 | SAMPLING PROCEDURES AND TABLES FOR INSPECTION BY ATTRIBUTES |
SAE AS 1310 : 2012 | FASTENER TORQUE FOR THREADED APPLICATIONS, DEFINITIONS OF |
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