Search Results

Standard

Vehicle Transport Unit Load Device (ULD)

2020-11-30

CURRENT

ARP1554D

The tests are static in nature to minimize complexity and cost of required testing facilities. As far as practical, applied static loads should take into account the combined static and dynamic loads anticipated in service. It is intended that tests shall be non-destructive in nature and not result in damage unless ultimate load conditions are employed. Test equipment and methods of testing described are not meant to be restrictive. Alternate equivalent methods to accomplish the desired results may be employed. In selected cases, tests may be repeated under ultimate load conditions when required for substantiation of analytical data. If this becomes necessary, the parts deformed may be removed and replaced prior to the retest.

Standard

Universal Turnover Build-Up Stand for Small Propulsion Units Requiring Vertical Assembly

2012-12-05

CURRENT

ARP863B

This recommended practice covers a stand that may be used for assembly, disassembly, and maintenance. The stand incorporates the following design criteria: complete interchangeability of any and all components, collapsible frame construction, envelope dimensions (marked with an asterisk on the attached drawings), attachment pad configuration, and gearbox and caster specifications.

Standard

Universal Turnover Build-Up Stand Series for Propulsion Units and/or Components

2005-10-28

CURRENT

ARP680C

This recommended practice covers a series of stands that may be used for assembly, disassembly and maintenance; incorporating the following design criteria: a collapsible frame construction, envelope dimensions, attachment shear pad configuration and gear box and caster specifications.

Standard

Universal Maintenance & Overhaul Stand for Turbo-Jet (10,000 Lbs. Thrust Class) and Turbo-Prop Engines

2002-12-16

CURRENT

ARP458

Standard

ULD for Aircraft Transportation of Horses

2012-11-26

HISTORICAL

ARP1621B

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: a Type 1: The ULD is an airworthiness certified structural container, satisfying the requirements of NAS 3610 for the appropriate base size. b Type 2: The ULD consists of a self-contained stall which is positioned on a standard aircraft pallet and restrained to the pallet by means of a cargo pallet net or by straps. WARNING: It is the carrier’s responsibility to obtain airworthiness approval for a Type 2 unit using strap-restraint. Refer to 7.1 b (Documentation).

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

ULD FOR AIRCRAFT TRANSPORTATION OF HORSES

1980-03-01

HISTORICAL

ARP1621

This ARP defines minimum requirements for horse stalls necessary to maintain a structurally safe operation and protect aircraft from corrosion created by waste spills.

Standard

ULD FOR AIRCRAFT TRANSPORTATION OF HORSES

1990-08-01

HISTORICAL

ARP1621A

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: a Type 1: The ULD is an airworthiness certified structural container, satisfying the requirements of NAS 3610 for the appropriate base size. b Type 2: The ULD consists of a self-contained stall which is positioned on a standard aircraft pallet and restrained to the pallet by means of a cargo pallet net or by straps.

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, Type C-2

1997-08-01

HISTORICAL

AS6480

This specification covers one type of aircraft cargo tie down, designated Type C-2.

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

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

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

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

Symbology for Standardization of Cargo Handling Systems

2013-03-01

CURRENT

ARP1757B

The symbols specified in this SAE Aerospace Recommended Practice (ARP) are applicable to all aircraft cargo handling systems for lower deck as well as for upper deck systems. Utilizing the symbols the conveyance, guidance, restraint, power drive unit and the degree of automation for the total cargo handling system can be depicted.

Standard

Symbology for Standardization of Cargo Handling Systems

2007-12-07

HISTORICAL

ARP1757A

The symbols specified in this SAE Aerospace Recommended Practice (ARP) are applicable to all aircraft cargo handling systems for lower deck as well as for upper deck systems. Utilizing the symbols the conveyance, guidance, restraint, power drive unit and the degree of automation for the total cargo handling system can be depicted.

Standard

Stand, Shipboard, Helicopter Maintenance

2017-11-06

CURRENT

AS85376

This specification covers a helicopter maintenance stand used by personnel aboard aviation capable ships.

Standard

Slings, Aircraft, General Specification For

2017-11-03

CURRENT

AS5944

This specification covers the general requirements for aircraft slings used to lift and transport aircraft or aircraft components which may be bulky or fragile.