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Standard

High Strength Elevated Temperature Bolting Practice

2019-05-03
CURRENT
ARP700C
This SAE Aerospace Recommended Practice (ARP) provides general information on the design and installation of threaded fasteners in high strength and high temperature applications in propulsion systems. Some of the more common definitions of fastener terminology are also provided.
Standard

Flaring (Swaging) and Removal of Shank Nuts

2019-03-18
CURRENT
ARP4848A
To specify the approved method of flaring the shank of self-locking shank nuts, and to provide the preferred method for removal of damaged nut.
Standard

High Strength Elevated Temperature Bolting Practice

2018-08-23
HISTORICAL
ARP700B
This SAE Aerospace Recommended Practice (ARP) provides general information on the design and installation of threaded fasteners in high strength and high temperature applications in propulsion systems. Some of the more common definitions of fastener terminology are also provided.
Standard

Flaring (Swaging) and Removal of Shank Nuts

2018-08-23
HISTORICAL
ARP4848
To specify the approved method of flaring the shank of self-locking shank nuts, and to provide the preferred method for removal of damaged nut.
Standard

White Paper to Support Supersession of MIL-S-8879C With AS8879C

2018-08-23
HISTORICAL
AIR5926
This paper was prepared to support supersession of MIL-S-8879C with Screw Thread Conformity Task Force selected industry standard AS8879C, published by the Society of Automotive Engineers (SAE). Other documentation changes will be covered by separate papers. Separate papers are anticipated for thread gaging issues, and thread gage calibration procedures. The STC-TF decided that the thread design standard needed to be completed before thread gage definition could be addressed. Thread gage definition has to be known before calibration procedures can be addressed.
Standard

Control Lever Connections (60° V Serrations)

2018-04-28
CURRENT
ARP260E
This SAE Aerospace Recommended Practice (ARP) provides the definition for a control lever connection with 60° "V" serrations for aircraft engine to aircraft power or control levers.
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