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Standard

Wide-Body and Standard-Body Aircraft Lower Deck Cargo Compartment ULD Capacities
2022-05-04
CURRENT
AIR1869D
This SAE Aerospace Information Report (AIR) covers information relative to ULDs (Unit Load Devices) container and pallet configurations, maximum usable container, pallet and bulk compartment volumes and tare weights for the lower deck of various wide-body aircraft. Bulk compartment volumes are also included for standard-body aircraft.
Standard

Wide-Body and Standard-Body Aircraft Lower Deck Cargo Compartment ULD Capacities
2009-11-20
HISTORICAL
AIR1869C
This SAE Aerospace Information Report (AIR) covers information relative to ULDs (Unit Load Devices) container and pallet configurations, maximum usable container, pallet and bulk compartment volumes and tare weights for the lower deck of various wide-body aircraft. Bulk compartment volumes are also included for standard-body aircraft.
Standard

Wide-Body and Standard-Body Aircraft Lower Deck Cargo Compartment ULD Capacities
2008-06-22
HISTORICAL
AIR1869B
This SAE Aerospace Information Report (AIR) covers information relative to ULDs (Unit Load Devices) container and pallet configurations, maximum usable container, pallet and bulk compartment volumes and tare weights for the lower deck of various wide-body aircraft. Bulk compartment volumes are also included for standard-body aircraft.
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 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

Universal Horizontal Field Maintenance Stand for 10,000 pound Weight Class Propulsion Units (48 inch and 30 inch Rail Gage)
2012-12-05
CURRENT
ARP581B
This recommended practice covers a rail concept stand that may be used for horizontal disassembly and reassembly, and maintenance, incorporating certain design features which are defined herein. These features include the rail dimensions and width, length and height of stand to insure compatibility with rail concept type transport and positioning trailers.
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

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.
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