Standard
FITTING, TIEDOWN, CARGO RING (10,000 LB) AND SEAT STUD, TYPE II
2005-08-09
HISTORICAL
AS21235
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Standard
FITTING, TIEDOWN, CARGO RING (5000 LB) AND SEAT STUD, TYPE I
2011-11-23
CURRENT
AS21234A
Standard
Temperature Controlled Container - Performance Requirements and Test Parameters
2015-12-19
CURRENT
AS6163
This SAE Aerospace Standard (AS) defines the minimum performance standard to demonstrate compliance with the regulatory design, test and operational requirements for a Temperature Controlled Container (TCC).
Standard
Tie Down, Cargo, Aircraft, Type C-2
2013-03-15
CURRENT
AS6480B
This specification covers one type of aircraft cargo tie down, designated Type C-2.
Standard
Certified Containers for Lower Deck Compartments
2018-10-18
CURRENT
AS5896
This SAE Aerospace Standard (AS) covers the design, fabrication, performance, and testing requirements for general-purpose, base-restrained, containers requiring airworthiness approval for installation/use in aircraft lower deck compartments. See 10.1 and 10.2.
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
Interline Air Cargo Pallets
2023-01-13
CURRENT
AS1491B
This SAE Aerospace Standard specifies the dimensional, design criteria, fabrication, performance, operational, environmental, and testing requirements for interline pallets requiring airworthiness approval for loading onto civil transport aircraft equipped with NAS3610/AS36100 restraint systems and using pallet nets meeting the requirements of AS1492. Type II/2 covers NAS3610/AS36100 code sizes. Type III pallets have been removed from this SAE Aerospace Standard revision.
Standard
Universal Leak Detector
2005-10-28
CURRENT
ARP726A
This recommended practice covers a self-contained detection system which is capable of pressurizing a closed system up to 70 psig with halogen (tracer) gas and up to 3500 psig with nitrogen.
Standard
Standardization of Drive End of Hydraulic or Geared Torque Wrenches for Use to an Upper Limit of 500,000 inch pounds
2012-12-05
CURRENT
ARP1135B
This SAE Aerospace Recommended Practice (ARP) covers the dimensions of an inside splined driver-wrench adapter, envelope of the housing-wrench reaction, the mechanical method of adapting the driver-wrench adapter to the wrench adapter driven end, and the housing-wrench reaction to the holder-counter torque.
Standard
LIFTING EYE - PROPELLER SHAFT
2012-12-05
CURRENT
AS161A
Standard
WRENCH - PROPELLER SHAFT (SHAFT SIZES NO. 10-20-30)
2012-12-05
CURRENT
AS352B
Standard
HANDLE - PROPELLER SHAFT WRENCH
2012-12-05
CURRENT
AS353A
Standard
PIN - PROPELLER SHAFT WRENCH
2012-12-05
CURRENT
AS354B
Standard
WRENCH - PROPELLER SHAFT (SHAFT SIZES NO. 40-50-60)
2012-12-05
CURRENT
AS351B
Standard
Drum, Metal-Shipping and Storage
2017-11-03
CURRENT
AS6054
This specification covers new cylindrical drums to be used as exterior shipping containers (see 6.1).
Standard
Air Cargo Pallet Extensions
2023-10-06
CURRENT
AS1988B
This SAE Aerospace Standard (AS) establishes the dimensional and operational requirements for pallet extension devices. It provides support for items of cargo beyond either the short or the long sides of a pallet, allowing increased volume to be achieved in conjunction with pallets meeting the requirements of AS1491 plus additional pallet sizes usable with extensions.
Standard
Air Cargo Unit Load Devices - Load Distribution Model
2004-01-14
HISTORICAL
AS36101
This SAE Aerospace Standard (AS) defines an industry agreed reference model for load distribution on air cargo unit load device (ULD) bases, to reflect maximum allowable center of gravity (CG) eccentricity and ensure the maximum allowable area load is not exceeded.
Standard
Air Cargo Unit Load Devices – Load Distribution Model
2011-09-07
CURRENT
AS36101A
This SAE Aerospace Standard (AS) defines an industry agreed reference model for load distribution on air cargo unit load device (ULD) bases, to reflect maximum allowable center of gravity (CG) eccentricity and ensure the maximum allowable area load is not exceeded.
