Refine Your Search

Date

Date

Topic

Topic

AGE-2 Air Cargo Safety Identification Materials properties

Search Results

Viewing 1 to 20 of 112
123Next >Last >>
Sort by title
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

ULD for Aircraft Transportation of Horses
2023-05-26
WIP
ARP1621D
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.
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 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

Stands, Shipping and Storage, Aircraft Engines, Reusable
2017-10-25
WIP
ARP4898A
This SAE Aerospace Recommended Practice (ARP) recommends design and test criteria for reusable shipping and storage stands for aircraft engines. An optional hard cover (enclosure) is also specified.
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.
Standard

Methodology of Calculating Aircraft Cargo Volumes
2014-03-25
CURRENT
AS1825C
The scope of this SAE Aerospace Standard (AS) shall cover the methodology of defining and determining the "internal volumes" of both the main deck and lower deck aircraft cargo compartments. The minimum required clearance between the compartment envelope and the unit load devices (ULDs) shall also be stated in order to provide the maximum ULD external contour and the methodology to define the ULD internal volumes.
Standard

Methodology of Calculating Aircraft Cargo Volumes
2008-06-22
HISTORICAL
AS1825B
The scope of this SAE Aerospace Standard (AS) shall cover the methodology of defining and determining the "internal volumes" of both the main deck and lower deck aircraft cargo compartments. The minimum required clearance between the compartment envelope and the unit load devices (ULDs) shall also be stated in order to provide the maximum ULD external contour and the methodology to define the ULD internal volumes.
Standard

METHODOLOGY OF CALCULATING AIRCRAFT CARGO VOLUMES
1983-07-01
HISTORICAL
AS1825
The scope of this Aerospace Standard shall cover the methodology of defining and determining the "Internal Volumes" of both the main deck and lower deck aircraft cargo compartments. The minimum required clearance between the compartment envelope and the unit load devices (ULD's) shall also be stated in order to provide the maximum OLD external contour and the methodology to define the OLD internal volumes. The methodology of defining and determining "maximum package sizes charts" for the cargo compartments shall also be included.
Standard

METHODOLOGY OF CALCULATING AIRCRAFT CARGO VOLUMES
1995-03-01
HISTORICAL
AS1825A
The scope of this SAE Aerospace Standard (AS) shall cover the methodology of defining and determining the "internal volumes" of both the main deck and lower deck aircraft cargo compartments. The minimum required clearance between the compartment envelope and the unit load devices (ULDs) shall also be stated in order to provide the maximum ULD external contour and the methodology to define the ULD internal volumes.
123Next >Last >>
X