SAE AIR1471B
Current
The latest, up-to-date edition.
Torque Tightening Threaded Fasteners
Hardcopy , PDF
English
04-03-2018
Important note : Users cannot be edited or removed once added to your Multi user PDF.
1 SCOPE
2 REFERENCES
3 REQUIREMENTS
4 NOTES
Covers the aerospace propulsion industry with recommended assembly torque limits for commonly used aircraft propulsion system threaded fasteners when a common torque value per size is the objective.
| DocumentType |
Standard
|
| Pages |
9
|
| ProductNote |
THIS STANDARD IS NOW STABILIZED
|
| PublisherName |
SAE International
|
| Status |
Current
|
| Supersedes |
The purpose of this SAE Aerospace Information Report (AIR) is to provide the aerospace propulsion industry with recommended assembly torque limits for commonly used aircraft propulsion system threaded fasteners when a common torque value per size is the objective.
| SAE AS9359A | NUT, CASTELLATED, HEXAGON, SILVER PLATED, CRES UNS S66286, 130 KSI MIN |
| MIL-PRF-7808 Revision L:1997 | LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE |
| MS9881 Revision B:1982 | NUT, PLAIN, HEXAGON - AMS 6322, CADMIUM PLATE MIL-S-8879 |
| SAE AS 8879 : 2004 | SCREW THREADS - UNJ PROFILE, INCH CONTROLLED RADIUS ROOT WITH INCREASED MINOR DIAMETER |
| SAE AS5377A | Nut, Self-Locking, 0.7500 thru 1.5000 Thread Sizes, UNS S66286, 160,000 psi, 800 °F, UNJ Thread – Procurement Specification |
| SAE AS 1310 : 2012 | FASTENER TORQUE FOR THREADED APPLICATIONS, DEFINITIONS OF |
| SAE AS3068B | Nut, Self-Locking, Double Hexagon, Reduced Envelope, AMS7251 |
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