1998589

MIL MIL-STD-1791C

Designing for Internal Aerial Delivery in Fixed Wing Aircraft

standard by Military Specifications and Standards , 10/23/2017

📝 Amendments Available

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Full Description

MIL-STD-1791C provides design and performance requirements to assure the airworthiness of USAF fixed wing aircraft during safe and effective cargo transportation missions. It presents design requirements and operating limits from the basic aircraft loading manuals and technical publications and is supplemented by additional useful air transport data. The process for approval or certification of cargo for air transport in USAF fixed wing aircraft is described in 6.4. This section presents the format for submitting a request for certification and provides examples of the type of data to submit. The reinstatement of this document as a Department of Defense Standard (subsequent to its previous conversion to a MIL-HDBK) allows it to be cited in procurement packages.
 

Product Details

Published:
10/23/2017
Number of Pages:
397
File Size:
1 file , 34 MB
Note:
This product is unavailable in Ukraine, Russia, Belarus
 

Document History

  1. MIL MIL-STD-1791C

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    Designing for Internal Aerial Delivery in Fixed Wing Aircraft

    • Most Recent

  2. MIL MIL-STD-1791B


    Designing for Internal Aerial Delivery in Fixed Wing Aircraft

    • Historical Version

  3. MIL MIL-STD-1791A


    Designing for Internal Aerial Delivery in Fixed Wing Aircraft

    • Historical Version
 

Amendments, rulings, supplements, and errata

  1. MIL MIL-STD-1791C Change 1


    Designing for Internal Aerial Delivery in Fixed Wing Aircraft