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SAE AIR1850 Rev A

Twin Engine Helicopter Power Requirements
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SAE AIR1850 Rev A

Twin Engine Helicopter Power Requirements

PUBLISH DATE 1997
PAGES 8
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This SAE Aerospace Information Report (AIR) defines the power spectrum during normal and emergency operations of a twin engine helicopter and thereby postulates suitable power plant rating structures. This document does not address the power requirements for single engine helicopters or those with more than two engines.
SDO SAE: SAE International
Document Number AIR1850
Publication Date June 1, 1997
Language en - English
Page Count 8
Revision Level A
Supercedes
Committee
Publish Date Document Id Type View
June 1, 1997 AIR1850A Revision
March 13, 1989 AIR1850 Revision