Standard
ROD END - THREADED, AIRCRAFT
2024-03-22
CURRENT
AS49011C
Search Results
Standard
Lubricant, Solid Film
2022-04-01
CURRENT
AS1701F
This document covers the performance requirements for solid dry film lubricants, air dried or heat cured, for use in aerospace applications. These lubricants are intended to prevent galling, and may be capable of remaining effective for extended periods of time after exposure to extreme environmental conditions.
Standard
Groove Design - Metal Face Seal
2019-06-06
CURRENT
AIR1108A
Groove designs presented herein are applicable for use with machined or formed metal seals which are similar in configuration to those shown in figure 3, which operate under internal pressure or in vacuum service and which have been specifically qualified or recommended by the purchaser or the manufacturer for use with this AIR. They are also applicable for use with metal o-rings (e.g., MS9142, MS202 thru MS9205) where interchangeability with machined or formed metal seals is desired. For metal o-ring groove designs where inter-changeability is not a requirement refer to ARP 674.
Standard
PROPELLER SHAFT ENDS - FLANGED SMALL AIRCRAFT ENGINE
2018-11-28
CURRENT
ARP502A
Standard
REMOTE TRIMMING ATTACHMENT FOR AIRCRAFT TURBINE ENGINE CONTROLS
2018-11-27
CURRENT
AS903A
Standard
STUD, LOCKED IN-RING LOCKED, SERRATED
2018-09-28
CURRENT
AS51989C
Standard
Orientation of Engine Axis, Coordinate and Numbering Systems for Aircraft Gas Turbine Engines
2018-09-11
CURRENT
ARP246D
Orientation of the engine, engine axis and coordinate system referred to herein shall be the conventional terminology used in all references to aircraft gas turbine engines.
Standard
Operating Instructions for Aircraft Engines (Preparation of)
2018-09-11
CURRENT
AS177C
This specification covers the requirements for format and outline of contents of operating instructions in published form or in manuscript form suitable for publication.
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
Definitions, Aircraft Reciprocating Engine Performance
2018-06-20
CURRENT
AS20D
This document lists definitions that are commonly used in describing aircraft reciprocating engine performance.
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.
Standard
Number 70-90, 70L-90, 80-100, and 80L-100 Propeller Shaft Ends Dual Rotation (Propeller Supplied Bearing)
2018-04-19
CURRENT
AIR26B
This SAE Aerospace Information Report (AIR) records the dimensions for the No. 70-90, 70L-90, 80-100, and 80L-100 dual rotation propeller shaft ends, which have been deleted from ARP375.
Standard
Altitude Graphs Aircraft Reciprocating Engine Performance
2018-04-19
CURRENT
AS1C
This SAE Aerospace Standard (AS) provides for aircraft reciprocating engines formats for altitude graph sheets recommended for use when presenting engine performance data.
Standard
STUD, LOCKED IN-RING LOCKED, SERRATED
2016-04-20
HISTORICAL
AS51989B
Standard
Lubricant, Solid Film
2014-12-28
HISTORICAL
AS1701E
This document covers the performance requirements for solid dry film lubricants, air dried, or heat cured for use in aerospace applications. These lubricants are intended to prevent galling, and may be capable of remaining effective for extended periods of time after exposure to extreme environmental conditions.
Standard
PADS, OIL INLET AND OUTLET, TYPES I, II & III - FOR AIRPLANE CONNECTIONS AIRCRAFT ENGINES
2014-08-12
CURRENT
AS131B
Standard
STUD, LOCKED IN-RING LOCKED, SERRATED
2014-04-24
HISTORICAL
AS51989A
Standard
Gas Turbine Engine Power Take-Off Pad Requirements
2014-02-06
CURRENT
ARP748B
This document summarizes the need for power take-off pads on gas turbine engines intended for helicopter power plant installations.
Standard
Splines, Involute (Full Fillet)
2014-02-06
CURRENT
AS84D
This SAE Aerospace Standard (AS) defines an involute with a 30° pressure angle and a full radius at the roots thus reducing the stress concentration in the area of the root.
Standard
Lubricant, Solid Film
2014-01-09
HISTORICAL
AS1701D
Delete AS7108, clarify thickness requirements for coating of threads, clarify tape test requirements, update references, and general revision.
