Standard
WRENCH - PROPELLER SHAFT (SHAFT SIZES NO. 40-50-60)
2012-12-05
CURRENT
AS351B
Search Results
Standard
WRENCH - PROPELLER SHAFT (SHAFT SIZES NO. 10-20-30)
2012-12-05
CURRENT
AS352B
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
ULD for Aircraft Transportation of Horses
2017-09-11
CURRENT
ARP1621C
This SAE Aerospace Recommended Practice (ARP) defines minimum requirements for an aircraft transport ULD to transport horses properly and safely by air, to protect the horse(s) from injuries, and to protect the aircraft from corrosion created by waste spill. The ULD is designed to accommodate one horse or several. There are two types of ULDs for aircraft transportation of horses:
Standard
Tie Down Assembly, Helicopter Blade, General Specification For
2017-11-03
CURRENT
AS85075
This specification covers the tie down assemblies for use on helicopter blades.
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 ASSEMBLY, HELICOPTER BLADE CH-53 HELICOPTER
2017-11-05
CURRENT
AS85075/2
Standard
TIE DOWN ASSEMBLY, HELICOPTER BLADE CH-46 HELICOPTER
2017-11-05
CURRENT
AS85075/1
Standard
RING, CARGO TIEDOWN (25,000 LB), TYPE IV
2005-08-09
HISTORICAL
AS21237
Standard
RING, CARGO TIEDOWN (25 000 LB), TYPE IV
2011-11-23
CURRENT
AS21237A
Standard
RING, CARGO TIEDOWN (10,000 LB), TYPE III
2005-08-09
HISTORICAL
AS21236
Standard
RING, CARGO TIEDOWN (10 000 LB), TYPE III
2011-11-23
CURRENT
AS21236A
Standard
REQUIREMENTS FOR AIRCRAFT ON BOARD WEIGHT AND BALANCE SYSTEM
1995-06-01
HISTORICAL
ARP1409B
This SAE Aerospace Recommended Practice (ARP) establishes requirements for the function, characteristics, and installation of an aircraft On Board Weight and Balance System (OBWBS) for use on civil transport aircraft. This document is not intended to specify design methods, mechanisms, or material to accomplish the requirements set forth.
Standard
REQUIREMENTS FOR AIRCRAFT ON BOARD WEIGHT AND BALANCE SYSTEM
1992-12-01
HISTORICAL
ARP1409A
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
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
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
Fire Containment Cover - Design, Performance, and Testing Requirements
2021-12-13
CURRENT
AS6453A
This SAE Aerospace Standard (AS) specifies the minimum design and performance criteria and testing methods of fire containment covers (FCCs) used either: a In those cargo compartments of civil transport aircraft where they constitute one means of complying with applicable airworthiness regulations, or b On a voluntary basis, when deemed appropriate by operators to improve fire protection in aircraft cargo compartments where airworthiness regulations do not mandate their use.
