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Standard

Aircraft Cargo Door Opening/Sill Details for Ground Support Equipment Interface
2020-11-23
CURRENT
AIR1673B
Manufacturers/designers of all aircraft equipped with a pallet/container capability have provided a means of linking the ground loaders/elevators with the aircraft sill for the smoother transfer of pallets and containers into or out of the aircraft holds. Use of the aircraft attachment points may be used as a means of averting damage to the aircraft door frames and other important parts. Latch-on guarantees fore and aft and vertical alignment of the loader bed with the aircraft doorway, when used in conjunction with the appropriate ground equipment. This SAE Aerospace Information Report (AIR) has been prepared by SAE Subcommittee AGE-2A to present a review of the current range of aircraft attachment points on wide body aircraft and those narrow body aircraft with a ULD cargo capability. Airline operators, who utilized these facilities, have been faced with a growing number of adaptor bars necessary to suit each type of aircraft and door position.
Standard

AIRCRAFT CARGO DOOR OPENING/SILL DETAILS FOR GROUND SUPPORT EQUIPMENT INTERFACE
1992-12-01
HISTORICAL
AIR1673
Manufacturers/designers of all aircraft equipped with a pallet/container capability have provided a means of linking the ground loaders/elevators with the aircraft sill for the smoother transfer of pallets and containers into or out of the aircraft holds. Use of the aircraft attachment points may be used as a means of averting damage to the aircraft door frames and other important parts. Latch-on guarantees fore and aft and vertical alignment of the loader bed with the aircraft doorway, when used in conjunction with the appropriate ground equipment. This Aerospace Information Report has been prepared by SAE Subcommittee AGE-2A to present a review of the current range of aircraft attachment points on wide body aircraft and those narrow body aircraft with a ULD cargo capability. Airline operators, who utilized these facilities, have been faced with a growing number of adaptor bars necessary to suit each type of aircraft and door position.
Standard

Aircraft Cargo Door Opening/Sill Details for Ground Support Equipment Interface
2013-08-12
HISTORICAL
AIR1673A
Manufacturers/designers of all aircraft equipped with a pallet/container capability have provided a means of linking the ground loaders/elevators with the aircraft sill for the smoother transfer of pallets and containers into or out of the aircraft holds. Use of the aircraft attachment points may be used as a means of averting damage to the aircraft door frames and other important parts. Latch-on guarantees fore and aft and vertical alignment of the loader bed with the aircraft doorway, when used in conjunction with the appropriate ground equipment. This SAE Aerospace Information Report (AIR) has been prepared by SAE Subcommittee AGE-2A to present a review of the current range of aircraft attachment points on wide body aircraft and those narrow body aircraft with a ULD cargo capability. Airline operators, who utilized these facilities, have been faced with a growing number of adaptor bars necessary to suit each type of aircraft and door position.
Standard

Tube Fittings, Aerospace Fluid Systems, Separable, for 24 Degree Cone, General Specification, Metric (ISO 7169)
2021-06-10
CURRENT
MA2005C
This document specifies performance and quality requirements for the qualification and manufacture of 24 degree cone fittings to ensure reliable performance in aircraft hydraulic systems. This document specifies baseline criteria for the design and manufacture of system fittings that are qualification tested on engines. This document covers fittings of temperature types and pressure classes specified in MA2001.
Standard

Tube Fittings, Aerospace Fluid Systems, Separable, For 24° Cone, General Specification, Metric (ISO 7169)
2015-08-21
HISTORICAL
MA2005B
This document specifies performance and quality requirements for the qualification and manufacture of 24° cone fittings to ensure reliable performance in aircraft hydraulic systems. This document specifies baseline criteria for the design and manufacture of system fittings that are qualification tested on engines. This document covers fittings of temperature types and pressure classes specified in MA2001.
Standard

TUBE FITTINGS, METRIC, AEROSPACE FLUID SYSTEMS, SEPARABLE – GENERAL SPECIFICATION FOR
1983-09-01
HISTORICAL
MA2005A
This standard establishes the basic performance and quality criteria for screw-together tube fitting assemblies and port connectors. It was prepared to standardize on the qualification test and procurement requirements for ISO standard tube fittings. The test requirements are intended to satisfy the most strenuous demands encountered in a high performance aircraft hydraulic system. The procurement requirements are intended to assure that fittings which are bought to this specification are of the same quality as the fittings used during the original qualification testing. Compliance with these test and procurement requirements is necessary for fittings which are used in control systems where a malfunction could affect the safety of flight.
Standard

Fittings, Welded, Hydraulic, Titanium and Corrosion Resistant Steel, 21 000 kPa, Metric
2015-08-21
CURRENT
MA2060A
This aerospace specification defines the requirements for metric weld fittings and machine weldments using an orbiting welding head suitable for use on cold worked 3A1-2.5V titanium and 21Cr-6Ni-9Mn CRES tubing and associated fittings. This specification is equivalent to AS1576 except for metric dimensions and standards.
Standard

Fittings, Cargo Tiedown, Aircraft
2006-04-27
HISTORICAL
AS7092A
This specification covers the requirements for one type of tiedown fitting for installation in the floors of aircraft.
Standard

Fittings, Cargo Tiedown, Aircraft
2012-10-15
CURRENT
AS7092B
This specification covers the requirements for one type of tiedown fitting for installation in the floors of aircraft.
Standard

Fittings, Cargo Tiedown, Aircraft
1999-07-01
HISTORICAL
AS7092
This specification covers the requirements for one type of tiedown fitting for installation in the floors of aircraft.
Standard

Impulse Testing of Hydraulic Tubing and Fittings, S-N Curve
2013-01-07
CURRENT
AS4265
This aerospace test standard establishes the requirements and procedures for evaluating and comparing the impulse fatigue performance of high pressure hydraulic fittings and tubing. This test method may be used to test similar fluid system components, if desired.
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