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.
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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
Fittings and Cargo Rings, Tie-Down, Aircraft Floor
2012-12-03
CURRENT
AS8905A
This specification establishes requirements for two types of aircraft floor fittings for tiedown of cargo and seats, and two types of cargo tiedown rings.
Standard
Fittings and Cargo Rings, Tie-Down, Aircraft Floor
2006-07-25
HISTORICAL
AS8905
This specification establishes requirements for two types of aircraft floor fittings for tiedown of cargo and seats, and two types of cargo tiedown rings.
Standard
Tie Downs, Cargo, Aircraft
2000-11-01
HISTORICAL
AS25959
This specification covers four types of aircraft cargo tie downs.
Standard
Tie Down, Cargo, Aircraft, CGU-1/B
2000-11-01
HISTORICAL
AS27260
This specification covers one type of 5,000-pound capacity aircraft cargo tie down. The tie down is designated CGU-1/B and is furnished in a minimum length of 240 inches.
Standard
Net, Cargo Tiedown, Pallets, HCU-7/E, HCU-15/C, HCU-11/C, and HCU-16/C
2000-11-01
HISTORICAL
AS27444
This specification covers pallet cargo tiedown nets, designated HCU-7/E, HCU-15/C, HCU-11/C and HCU-16/C.
Standard
Tie Down, Cargo, Aircraft, Nylon Web Net
2000-11-01
HISTORICAL
AS26780
This specification covers two types of aircraft cargo tie downs, each having a capacity of 10,000 pounds.
Standard
Environmental Degradation of Composite Materials
2018-10-18
CURRENT
ARP6287
In accordance with § 4.11 of AS36100, materials used in the construction of pallets, nets, and containers shall take into account the effects of environmental conditions, such as temperature, humidity, and UV degradation, expected in service. In accordance with (E)TSO-C90, the applicant shall consider environmental degradation due to aging, ultra-violet (UV) exposure, weathering, etc., for any materials used in the construction of pallets, nets, and containers. The purpose of this Aerospace Recommended Practice (ARP) is to provide guidelines for the basic requirements to be considered regarding environmental degradation effects when qualifying composite materials in the design to fulfill the (E)TSO-C90 Minimum Performance Standard. Material qualification is the verifying of a materials attributes and characterizations, which are typically determined through testing.
Standard
RING, CARGO TIEDOWN (10 000 LB), TYPE III
2011-11-23
CURRENT
AS21236A
Standard
RING, CARGO TIEDOWN (10,000 LB), TYPE III
2005-08-09
HISTORICAL
AS21236
Standard
FITTING, TIEDOWN, CARGO RING (10 000 LB) AND SEAT STUD, TYPE II
2011-11-23
CURRENT
AS21235A
Standard
FITTING, TIEDOWN, CARGO RING (5,000 LB) AND SEAT STUD, TYPE I
2005-08-09
HISTORICAL
AS21234
Standard
FITTING, TIEDOWN, CARGO RING (10,000 LB) AND SEAT STUD, TYPE II
2005-08-09
HISTORICAL
AS21235
Standard
FITTING, TIEDOWN, CARGO RING (5000 LB) AND SEAT STUD, TYPE I
2011-11-23
CURRENT
AS21234A
Standard
GENERAL REQUIREMENTS FOR POWERED DRIVE UNITS IN AIRCRAFT CARGO SYSTEMS
2008-06-22
HISTORICAL
AIR4165
This Aerospace Information Report (AIR) serves a dual purpose. It enables the user (aircraft manufacturer/airline) to do the following: a To make a positive decision for the installation of a powered drive system in the cargo loading system during the definition of the aircraft on-board cargo loading system to be developed/procured. b To provide the user with general requirements to be taken into consideration during the preparation of component specifications for powered drive units (PDUs) to be used in aircraft cargo systems. This is to provide the author of such a component specification with a selection of criteria in order to obtain an optimum component suitable for the users’ applications.
Standard
General Requirements for Powered Drive Units (PDUs) in Aircraft Cargo Systems
2012-11-01
HISTORICAL
AIR4165A
This SAE Aerospace Information Report (AIR) is intended to assist the user (aircraft manufacturer/airline) in the following areas: a In the decision of whether or not to plan for the installation of a powered drive system in the cargo loading system (CLS) during the definition of the aircraft on-board cargo loading system. b If a powered drive system is decided upon, to provide general requirements to be considered during the preparation of component specifications for the powered drive units (PDUs) to be used. This provides a selection of criteria in order to obtain an optimum PDU for the application considered.
Standard
General Requirements for Powered Drive Units (PDUs) in Aircraft Cargo Systems
2019-10-02
CURRENT
AIR4165B
This SAE Aerospace Information Report (AIR) is intended to assist the user (aircraft manufacturer/airline) in the following areas: a In the decision of whether or not to plan for the installation of a powered drive system in the cargo loading system (CLS) during the definition of the aircraft on-board cargo loading system. b If a powered drive system is decided upon, to provide general requirements to be considered during the preparation of component specifications for the powered drive units (PDUs) to be used. This provides a selection of criteria in order to obtain an optimum PDU for the application considered.
Standard
Stand, Shipboard, Helicopter Maintenance
2017-11-06
CURRENT
AS85376
This specification covers a helicopter maintenance stand used by personnel aboard aviation capable ships.
