TORQUE TIGHTENING THREADED FASTENERS

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

04-03-2018

Publisher

SAE International

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 R-430 : 2015 SAE AIR 1471 : 2000

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