Search Results

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

Wide-Body and Standard-Body Aircraft Lower Deck Cargo Compartment ULD Capacities

1991-01-18

HISTORICAL

AIR1869A

This AIR covers information relative to container and pallet configurations (ULDs), 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

WRENCH - PROPELLER SHAFT (SHAFT SIZES NO. 40-50-60)

2012-12-05

CURRENT

AS351B

Standard

WRENCH - PROPELLER SHAFT (SHAFT SIZES NO. 10-20-30)

2012-12-05

CURRENT

AS352B

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 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 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

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

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

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.