Standard
Fittings, Cargo Tiedown, Aircraft
2006-04-27
HISTORICAL
AS7092A
This specification covers the requirements for one type of tiedown fitting for installation in the floors of aircraft.
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Standard
Fittings, Cargo Tiedown, Aircraft
2012-10-15
CURRENT
AS7092B
This specification covers the requirements for one type of tiedown fitting for installation in the floors of aircraft.
Standard
Fittings, Cargo Tiedown, Aircraft
1999-07-01
HISTORICAL
AS7092
This specification covers the requirements for one type of tiedown fitting for installation in the floors of aircraft.
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
Net, Cargo Tiedown, Pallets, HCU-7/E, HCU-15/C, HCU-11/C, and HCU-16/C
2000-11-01
HISTORICAL
AS27444
This specification covers pallet cargo tiedown nets, designated HCU-7/E, HCU-15/C, HCU-11/C and HCU-16/C.
Standard
Cargo Compartments Maximum Package Size Calculation Methodology
2008-06-22
HISTORICAL
AIR4899
The methodology for maximum package size loading is based on a mathematical method allowing the calculation of maximum package size tables. This method does not in principal differentiate between bulk loading and cargo system loading. However, some restrictions have to be considered: Some cargo systems generate pre-determined pallet trajectories. Envelope curves depending on the pallet size and the possible trajectories have to be determined first. Door geometric limitations (with or without cargo loading system) Turning limitations due to weight, load geometry and conveyance capability Securing requirements This document is not intended for airline operational use. It should be used by engineers performing calculations or developing computer programs to produce Maximum Package Size tables specified in AS1825.
Standard
Cargo Compartments Maximum Package Size Calculation Methodology
2014-03-25
CURRENT
AIR4899A
The methodology for maximum package size loading is based on a mathematical method allowing the calculation of maximum package size tables. This method does not in principal differentiate between bulk loading and cargo system loading. However, some restrictions have to be considered: Some cargo systems generate pre-determined pallet trajectories. Envelope curves depending on the pallet size and the possible trajectories have to be determined first. Door geometric limitations (with or without cargo loading system) Turning limitations due to weight, load geometry and conveyance capability Securing requirements This document is not intended for airline operational use. It should be used by engineers performing calculations or developing computer programs to produce Maximum Package Size tables specified in AS1825.
Standard
RING, CARGO TIEDOWN (10 000 LB), TYPE III
2011-11-23
CURRENT
AS21236A
Standard
RING, CARGO TIEDOWN (10,000 LB), TYPE III
2005-08-09
HISTORICAL
AS21236
Standard
FITTING, TIEDOWN, CARGO RING (10 000 LB) AND SEAT STUD, TYPE II
2011-11-23
CURRENT
AS21235A
Standard
FITTING, TIEDOWN, CARGO RING (5,000 LB) AND SEAT STUD, TYPE I
2005-08-09
HISTORICAL
AS21234
Standard
FITTING, TIEDOWN, CARGO RING (10,000 LB) AND SEAT STUD, TYPE II
2005-08-09
HISTORICAL
AS21235
Standard
FITTING, TIEDOWN, CARGO RING (5000 LB) AND SEAT STUD, TYPE I
2011-11-23
CURRENT
AS21234A
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
INTERLINE AIR CARGO PALLET NETS
1982-03-01
HISTORICAL
AS1492
This specification establishes dimensional, structural and environmental requirements for interline pallet nets.
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.
Standard
LIFTING EYE - PROPELLER SHAFT
2012-12-05
CURRENT
AS161A
Standard
WRENCH - PROPELLER SHAFT (SHAFT SIZES NO. 10-20-30)
2012-12-05
CURRENT
AS352B
Standard
HANDLE - PROPELLER SHAFT WRENCH
2012-12-05
CURRENT
AS353A
