AIR1850: TWIN ENGINE HELICOPTER POWER REQUIREMENTS - Information Report

Features

Issuing Committee: S-12 Powered Lift Propulsion Committee

Scope

Content: No Scope available

Meta Tags

Topics: Aircraft
Helicopters
Entry, descent and landing
Fuel consumption
Hazards and emergency operations

Details

DOI: https://doi.org/10.4271/AIR1850

Pages: 1

Citation: SAE International Information Report, TWIN ENGINE HELICOPTER POWER REQUIREMENTS, SAE Standard AIR1850, Issued March 1989, https://doi.org/10.4271/AIR1850.

Additional Details

Publisher: SAE International

Published: Mar 13, 1989

Product Code: AIR1850

Content Type: Information Report

Status: Issued

Language: English

Historical