ARP748A: Gas Turbine Engine Power Take-Off Pad Requirements - Recommended Practice

Features

Issuing Committee: E-25 General Standards for Aerospace and Propulsion Systems

Scope

Content: This document summarizes the need for power take-off pads on gas turbine engines intended for helicopter power plant installations.

Meta Tags

Topics: Aircraft propulsion systems
Gas turbines
Aircraft
Helicopters
Gases

Details

DOI: https://doi.org/10.4271/ARP748A

Citation: SAE International Recommended Practice, Gas Turbine Engine Power Take-Off Pad Requirements, SAE Standard ARP748A, Stabilized February 2014, Revised February 2004, Reaffirmed May 1995, https://doi.org/10.4271/ARP748A.

Additional Details

Publisher: SAE International

Published: 2/23/2004

Product Code: ARP748A

Content Type: Recommended Practice

Status: Revised

Language: English

Historical