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CURRENT
2018-01-09
Standard
AS7474D
This specification covers bolts and screws made from a corrosion and heat resistant, martensitic iron base alloy of the type identified under the Unified Numbering System as UNS S17400. The following specification designations and their properties are covered: AS7474: 140 ksi minimum ultimate tensile strength at room temperature, 100 ksi stress corrosion test, 72 ksi to 7.2 ksi tension-tension fatigue AS7474-1: 140 ksi minimum ultimate tensile strength at room temperature, 100 ksi stress corrosion test, 88 ksi minimum ultimate shear strength at room temperature
2018-01-05
WIP Standard
AIR6972
To inform users on proper use, procedures and common errors when using electronic compensation for tooling on horizontal and vertical balancing machines
CURRENT
2018-01-02
Standard
AS1349B
This SAE Aerospace Standard (AS) covers helical coil locking screw thread inserts made from formed wire in which the inner surface of the coil, after assembly, provides threads of standard Unified 60 degrees form as specified on the assembly drawing. This document also covers the performance requirements of the locking feature of the insert which will retain United ANSI B1.1 (UN Profile) or AS8879 (UNJ Profile) external threaded parts.
CURRENT
2018-01-02
Standard
AS919A
To establish external dimensions for shafts requiring shallow grooves and internal dimensions for mating locking devices when used with parts dimensionally equivalent to Bearing Retaining Spanner Nuts, MS172236 thru MS172270.
CURRENT
2018-01-02
Standard
AS1229D
This SAE Aerospace Standard (AS) covers helical coil stud locking screw thread inserts made from formed wire in which the inner surface of the coil, after assembly provides threads of standard Unified 60° form as specified on the assembly drawing. This standard also covers the performance requirements of the locking feature of the insert which will retain Unified ANSI B1.1 (UN Profile) or AS8879 (UNJ Profile) external threaded parts.

To establish the performance requirements of helical coil stud locking screw thread inserts.

2017-12-31
WIP Standard
AS1C
This SAE Aerospace Standard (AS) provides for aircraft reciprocating engines formats for altitude graph sheets recommended for use when presenting engine performance data.
2017-12-31
WIP Standard
ARP953C
This document establishs limits or parameters for designing bolt heads with proper control of flowlines to assure sufficient strength to resist stresses induced by static or dynamic loads without being affected by lightening and lockwire holes.
2017-12-30
WIP Standard
AS3229B
No scope available.
2017-12-19
WIP Standard
AS9358B
No scope available.
CURRENT
2017-12-18
Standard
ARP5305A
This SAE Aerospace Recommended Practice (ARP) is written for individuals associated with the ground-level testing of large and small gas turbine engines and particularly for those who might be interested in constructing new or adding to existing engine test cell facilities.
2017-12-07
WIP Standard
AS7232A
This procurement specification covers aircraft quality solid rivets and tubular end rivets made form a corrosion and heat resistant nickel base alloy of the type identified under the Unified Numbering System as UNS N06600. Primarily for fastener applications requiring corrosion resistance and heat and oxidation resistance up to 2000 degrees F, but with reduced strength at the elevated temperatures. Rivets shall not be hand peened during driving.
2017-12-07
WIP Standard
AS848A
No scope available.
2017-12-07
WIP Standard
MA3287A
Scope is unavailable.
2017-12-07
WIP Standard
MA3344A
Scope is unavailable.
2017-12-07
WIP Standard
MA3350A
Scope is unavailable.
2017-12-07
WIP Standard
MA1421A
This SAE Aerospace Standard (MA) establishes the diameter-pitch combinations of ISO metric 60° screw threads recommended for use in the aerospace industry for metric module shaft or bearing retaining screw threads.
2017-12-07
WIP Standard
AS24586C
SCOPE IS UNAVAILABLE.
CURRENT
2017-11-29
Standard
AIR5301A
This SAE Aerospace Information Report (AIR) was written because of the growing interest in aircraft installed outdoor engine testing by the Federal Aviation Administration, airlines, charter/commercial operators, cargo carriers, engine manufacturers and overhaul and repair stations. This document was developed by a broad cross section of personnel from the aviation industry and government agencies and includes information obtained from a survey of a variety of operators of fixed and rotary wing aircraft and research of aircraft and engine maintenance manuals.
CURRENT
2017-11-29
Standard
AIR6364
The paper discusses in general terms the activities required to be undertaken or demonstrated during the establishment of the facility such as: the assessment checks prior to forwarding to the end users site for embodiment into the facility system the establishment of the facility such as trial installations of hardware, functionality checking of lifting transportation and access systems, centerline pull checks, pressure testing of fuel and air start systems, flushing of wet systems and electrical continuity checking. the commissioning of the facility such as instrumentation calibrations, engine starts, engine running, assessment of command and control system, assessment of DAS system, aerodynamic and acoustic surveys. The paper will concentrate on the main engineering engine related aspects of the facility and will not necessarily contain information on the construction validation activities such as HVAC, electrical, facility fire system, waste water etc.
Viewing 1 to 30 of 2474

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