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SAE AIR 1471 : 2018

Current

Current

The latest, up-to-date edition.

TORQUE TIGHTENING THREADED FASTENERS

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

04-03-2018

€89.37
Excluding VAT

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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