AIR1850A Twin Engine Helicopter Power Requirements
Revised
06/01/1997
- Features
- Issuing Committee
- Content
- 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.
- Pages
- 8
- Citation
- SAE International Information Report, Twin Engine Helicopter Power Requirements, SAE Standard AIR1850A, Revised June 1997, Issued March 1989, https://doi.org/10.4271/AIR1850A.