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

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

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

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

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

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

REQUIREMENTS FOR AIRCRAFT ON BOARD WEIGHT AND BALANCE SYSTEM

1978-01-01

HISTORICAL

ARP1409

Standard

Interline Air Cargo Pallets

2012-09-05

HISTORICAL

AS1491A

This document establishes dimensional, structural and environmental requirements for two types of interline pallets. Type II covers NAS 3610 code sizes and Type III covers other sizes not currently included in NAS 3610.

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

Interline Air Cargo Pallet Nets

2023-01-13

CURRENT

AS1492C

This document establishes dimensional, structural, and environmental requirements for Type II/2 interline pallet nets. Type II/2 covers NAS3610/AS36100 code sizes.

Standard

General Requirements for Noncertified Cargo/Baggage Containers

2018-10-18

CURRENT

AS1677D

This SAE Aerospace Standard (AS) covers the design, fabrication, performance and operational testing requirements for lower deck containers for use in main line aircraft which do not require airworthiness certification when loaded under the conditions of compartment restraint and in accordance with the aircraft's Weight and Balance Manual and/or, where applicable according to the aircraft type's approved Weight and Balance Manual, AS36100A or NAS 3610 equivalent base plate restraint for these containers. Most sizes of containers covered by this document (base sizes K, L, P, and Q) cannot physically be loaded and latched on aircraft main deck cargo systems. Base size A and M containers can, but are not allowed on aircraft main decks, which do not accept non-certified units. Accordingly, all containers covered by this document are to be used/installed exclusively in aircraft lower deck compartments.

Standard

General Requirements for Noncertified Cargo/Baggage Containers

2008-06-22

HISTORICAL

AS1677C

This SAE Aerospace Standard (AS) covers the requirements for lower deck containers in wide body and standard body aircraft which do not require airworthiness certification under the condition of compartment restraint and/or, where applicable according to aircraft type, NAS3610 equivalent baseplate-restraint for these containers. NOTE: IATA 50/0, “Requirements for interlining of ULDs”, should also be taken into account when designing and making equipment.

Standard

GENERAL REQUIREMENTS FOR NONCERTIFIED LD-2, LD-4, AND LD-8 CARGO/BAGGAGE CONTAINERS

1995-06-01

HISTORICAL

AS1677B

This SAE Aerospace Standard (AS) covers the requirements for three sizes of compartment restrained lower deck containers (unit load devices) for the 767 airplane and which do not require airworthiness certification. NOTE: IATA Specification 50/0, General Technical Requirements and Serviceability limits, should also be taken into account when designing and making equipment according to this specification as certain provisions contained therein will also be applicable.

Standard

GENERAL REQUIREMENTS FOR NON-CERTIFIED LD-2, LD-4 & LD-8 CARGO/BAGGAGE CONTAINERS

1985-03-15

HISTORICAL

AS1677

This AS covers the requirements for three sizes of compartment restrained lower deck containers (Unit Load Devices) for the 767 airplane and which do not require airworthiness certification.

Standard

GENERAL REQUIREMENTS FOR NON-CERTIFIED LD-2, LD-4 & LD-8 CARGO/BAGGAGE CONTAINERS

1988-11-01

HISTORICAL

AS1677A

This AS covers the requirements for three sizes of compartment restrained lower deck containers (Unit Load Devices) for the 767 airplane and which do not require airworthiness certification. NOTE: IATA Specificaton 50/0, General Technical Requirements and Serviceability limits, should also be taken into account when designing and making equipment according to this Specification as certain provisions contained therein will also be applicable.

Standard

Fire Containment Cover - Operation and Use

2020-04-23

CURRENT

ARP6905

This SAE Aerospace Recommended Practice (ARP) provides guidelines for the effective operation and use of fire containment covers (FCCs). Technical Standard Orders (TSOs) C203 and C90e (and later revisions) incorporate AS6453, and provide the Minimum Performance Standards (MPS) for an FCC design. The net and pallet used with the FCC must be approved using the updated net and flammability requirements in TSO C90e and later revisions. However, fire containment performance also requires this equipment is properly used. Fire safety is compromised when FCCs are used in an inadequate manner.