SAE AIR1850

Twin Engine Helicopter Power Requirements.

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Standard:
  • AIR1850
Revised:
  • 1989-03-13
Revision:
  • Historical. Access the latest revision: AIR1850A
Issuing:
  • S-12 Helicopter Powerplant Committee
Scope:

The purpose of this document is to define the power spectrum during normal and emergency operations of a twin engine helicopter and thereby to postulate suitable power plant rating structures. The document does not address the power requirements for single engine helicopters or those with more than two engines.

History:
StandardPublishedRevisionStatus
AIR1850A1997-06-01LatestRevised
AIR18501989-03-13HistoricalIssued
AKA:
  • SAE AIR 1850
Sector:
  • Aerospace
Topic:
  • Hybrid engines
  • Turboprop engines
  • Rotary-wing aircraft

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