UNLIMITED FREE ACCESS TO THE WORLD'S BEST IDEAS

close
Already an Engineering360 user? Log in.

This is embarrasing...

An error occurred while processing the form. Please try again in a few minutes.

Customize Your Engineering360 Experience

close
Privacy Policy

This is embarrasing...

An error occurred while processing the form. Please try again in a few minutes.

ARMY - DI-SESS-82291

AIR VEHICLE TECHNICAL DESCRIPTION REPORT FOR ROTORCRAFT AND PROPELLER-DRIVEN FIXED-WING AIRCRAFT

active, Most Current
Organization: ARMY
Publication Date: 18 September 2019
Status: active
Page Count: 48
scope:

Use/relationship:

This Data Item Description (DID) specifies the technical data and supplementary technical data necessary for Government assessments of the flight performance, stability and control, handling qualities, rotor dynamics, airframe dynamics, engine/drive system response characteristics, and transportability characteristics of new design or derivative rotary-wing and propeller-driven fixed-wing aircraft. These evaluations and analyses are used to support the substantiation of aircraft airworthiness in accordance with (IAW) Army Regulation (AR) 70-62, and to support Government technical analyses IAW Federal Acquisition Regulation (FAR) 15.404-1(e).

Document History

DI-SESS-82291
September 18, 2019
AIR VEHICLE TECHNICAL DESCRIPTION REPORT FOR ROTORCRAFT AND PROPELLER-DRIVEN FIXED-WING AIRCRAFT
Use/relationship: This Data Item Description (DID) specifies the technical data and supplementary technical data necessary for Government assessments of the flight performance, stability and...

References

Advertisement