SAE AIR 1471 : 2018
Current
The latest, up-to-date edition.
TORQUE TIGHTENING THREADED FASTENERS
Hardcopy , PDF
English
04-03-2018
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.
Committee |
E-25
|
DocumentType |
Standard
|
Pages |
9
|
ProductNote |
THIS STANDARD IS NOW STABILIZED
|
PublisherName |
SAE International
|
Status |
Current
|
Supersedes |
SAE AS 9359 : 2012 | 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:2000(S2024) | 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 AS 3068 : 2012 | NUT, SELF-LOCKING, DOUBLE HEXAGON, REDUCED ENVELOPE, AMS 7251 |
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