Standard
BOLTS, SCREWS AND STUDS, SCREW THREAD REQUIREMENTS
1974-08-01
HISTORICAL
AS3062A
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Standard
BOLTS, SCREWS AND STUDS, SCREW THREAD REQUIREMENTS
1970-03-01
HISTORICAL
AS3062
Standard
Bolts and Screws, Titanium Alloy 6Al - 4V, UNS R56400 Fatigue-Rated, Procurement Specification for
2023-02-14
CURRENT
AS7461F
This procurement specification covers aircraft-quality bolts and screws made from 6Al - 4V titanium alloy of the type identified under the Unified Numbering System as UNS R56400. The following specification designation and its properties are covered:
Standard
Bolts and Screws, Titanium Alloy 6Al - 4V, UNS R56400 Procurement Specification for
2023-02-14
CURRENT
AS7460D
This procurement specification covers aircraft-quality bolts and screws made of 6Al - 4V titanium alloy of the type identified under the Unified Numbering System as UNS R56400. The following specification designation and its properties are covered.
Standard
CHIP DETECTOR, ELECTRICAL CONNECTION, REMOTE INDICATING
1995-05-01
HISTORICAL
ARP843
This Aerospace Recommended Practice is applicable to the design of remote indicating magnetic chip detectors installed in the lube systems, hydraulic systems, controls systems, gearboxes, constant speed drives, etc. of Aerospace Power Plants. It is not applicable to the touch-to-test type terminal models.
Standard
Chip Detector, Electrical Connection, Remote Indicating
2012-11-01
HISTORICAL
ARP843A
This Aerospace Recommended Practice is applicable to the design of remote indicating magnetic chip detectors installed in the lube systems, hydraulic systems, controls systems, gearboxes, constant speed drives, etc. of Aerospace Power Plants. It is not applicable to the touch-to-test type terminal models.
Standard
Chip Detector, Electrical Connection, Remote Indicating
2021-05-28
CURRENT
ARP843B
This Aerospace Recommended Practice is applicable to the design of remote indicating magnetic chip detectors installed in the lube systems, hydraulic systems, controls systems, gearboxes, constant speed drives, etc. of Aerospace Power Plants. It is not applicable to the touch-to-test type terminal models.
Standard
DEFINITIONS, AIRCRAFT ENGINE
1941-11-01
HISTORICAL
AS20
Standard
FINAL REPORT ON COLD STARTING OF AIRCRAFT ENGINES
1946-09-01
HISTORICAL
AIR13
Standard
FINAL REPORT ON COLD STARTING OF RECIPROCATING AIRCRAFT ENGINES
1951-10-01
CURRENT
AIR13A
INTRODUCT ION Conventional internal conbustion a i r c r a f t engines require the same basic conditions for starting in cold weather as they do in warn weather. These are: (1) The engine must be cranked a t a reasonable speed. ( 2 ) A combustible mixture must be delivered t o the cylinders. (3) An ignition spark must be supplied which is capable of igniting t'ne charge a t the proper t i m e . (4) The fits and olearanoes of mating parts in the engine m u s t be such that normal Sunctions occur a t a l l temperatures. (5) The engine must receive a usable lubricant. (6) The engine must develop s u f f i c i e n t power t o overcome its own f r i c t i o n and accelerate itself t o the desired operating speed.
Standard
GENERAL PRACTICES FOR USE OF SAFETY WIRE, KEY WASHERS, AND COTTER PINS FOR PROPULSION SYSTEMS
1989-08-11
HISTORICAL
AS567G
This standard covers those devices whose primary function is retaining and excludes those devices that have integral locking features incorporated into the item being retained.
Standard
INSTALLATION PROCEDURES AND TORQUES FOR FLUID CONNECTIONS
1976-09-01
HISTORICAL
AS683A
These procedures cover the following:
Standard
INSTALLATION PROCEDURES AND TORQUES FOR FLUID CONNECTIONS
1995-05-01
HISTORICAL
AS683B
These procedures cover the following:
Standard
Installation Procedures and Torques for Fluid Connections
2006-05-04
HISTORICAL
AS683C
These procedures cover the following: Paragraph 3 - Cone end connections for flared tube and brazed ferrule, with and without gasket. Paragraph 4 - Boss end connections, positioned type, with back-up ring. Paragraph 5 - Boss end connections, positioned type, without back-up ring Paragraph 6 - Boss end connections, non-positioned type. Paragraph 7 - Bulkhead connections.
Standard
SAFETY WIRE, KEY WASHERS, AND COTTER PINS FOR PROPULSION SYSTEMS, GENERAL PRACTICES FOR USE OF
1992-12-14
HISTORICAL
AS567H
This standard covers devices whose primary function is the retention of fasteners, except for such devices that are integral with the item being retained.
Standard
STARTER, MOUNTING PADS AND DRIVES - TYPES I, II, III & IV
2013-01-04
CURRENT
AS44B
Standard
STARTER, MOUNTING PADS AND DRIVES - TYPES I, II, III & IV
1942-07-01
HISTORICAL
AS44
Standard
STARTER, MOUNTING PADS AND DRIVES - TYPES I, II, III & IV
2006-05-11
HISTORICAL
AS44A
Standard
Safety Cable, Safety Wire, Key Washers, and Cotter Pins for Propulsion Systems, General Practices for Use of
2021-09-10
CURRENT
AS567L
This SAE Aerospace Standard (AS) covers devices whose primary function is the retention of fasteners, except for such devices that are integral with the item being retained.
Standard
Safety Cable, Safety Wire, Key Washers, and Cotter Pins for Propulsion Systems, General Practices for Use of
2015-04-28
HISTORICAL
AS567K
This SAE Aerospace Standard (AS) covers devices whose primary function is the retention of fasteners, except for such devices that are integral with the item being retained.
