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NPFC - MIL-STD-1791

DESIGNING FOR INTERNAL AERIAL DELIVERY IN FIXED WING AIRCRAFT

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Organization: NPFC
Publication Date: 31 October 1985
Status: inactive
Page Count: 359
scope:

This standard covers general design and performance requirements of military equipment for internal air transport in military prime mission cargo aircraft and the long range international segment of the Civil Reserve Air Fleet (CRAF). This standard also contains general design and performance requirements for military equipment to be airdropped from Air Force cargo aircraft. The complete air transportability and airdrop requirements for an item of equipment not specified herein shall be specified in the individual equipment specification.

The requirements and tests contained in this standard apply to the internal air transportability and airdrop aspects of all items intended for aerial delivery in CRAF or USAF aircraft. They represent the minimum acceptable transportability and airdrop features. When it is known that the equipment will require features that are more restrictive than those stated herein, the more stringent features will be specified in the individual equipment specification.

Any projected design that will improve performance, safety, or reliability or reduce life cycle and end item cost through deviations from this standard, or where the requirements of this standard result in a compromise of the item for the sake of air transportability or airdrop, shall be brought to the attention of the procuring activity for consideration.

Document History

June 22, 2021
DESIGNING FOR INTERNAL AERIAL DELIVERY IN FIXED WING AIRCRAFT
The information in this standard covers everything necessary to adequately design or modify a cargo item to be safely and successfully transported aboard USAF cargo aircraft. The air transport...
March 31, 2021
DESIGNING FOR INTERNAL AERIAL DELIVERY IN FIXED WING AIRCRAFT AMSC
The information in this standard covers everything necessary to adequately design or modify a cargo item to be safely and successfully transported aboard USAF cargo aircraft. The air transport...
December 29, 2017
DESIGNING FOR INTERNAL AERIAL DELIVERY IN FIXED WING AIRCRAFT
Purpose. This standard provides design and performance requirements to assure the airworthiness of USAF fixed wing aircraft during safe and effective cargo transportation missions. It presents...
October 23, 2017
DESIGNING FOR INTERNAL AERIAL DELIVERY IN FIXED WING AIRCRAFT
A description is not available for this item.
December 2, 2014
DESIGNING FOR INTERNAL AERIAL DELIVERY IN FIXED WING AIRCRAFT
Purpose. This standard provides design and performance requirements to assure the airworthiness of USAF fixed wing aircraft during safe and effective cargo transportation missions. It presents...
June 11, 2014
DESIGNING FOR INTERNAL AERIAL DELIVERY IN FIXED WING AIRCRAFT
A description is not available for this item.
November 19, 2012
Designing for Internal Aerial Delivery in Fixed Wing Aircraft
This standard provides design and performance requirements to assure the airworthiness of USAF fixed wing aircraft whose missions involve the safe and effective transport of cargo. It presents design...
February 14, 1997
DESIGNING FOR INTERNAL AERIAL DELIVERY IN FIXED WING AIRCRAFT
A description is not available for this item.
March 23, 1995
DESIGNING FOR INTERNAL AERIAL DELIVERY IN FIXED WING AIRCRAFT
A description is not available for this item.
April 15, 1986
DESIGNING FOR INTERNAL AERIAL DELIVERY IN FIXED WING AIRCRAFT
A description is not available for this item.
MIL-STD-1791
October 31, 1985
DESIGNING FOR INTERNAL AERIAL DELIVERY IN FIXED WING AIRCRAFT
This standard covers general design and performance requirements of military equipment for internal air transport in military prime mission cargo aircraft and the long range international segment of...

References

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