ARP748B: 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.

Rationale

Content: This document has been determined to contain basic and stable technology which is not dynamic in nature. This standard has been stabilized.

Meta Tags

Topics: Aircraft
Helicopters
Documentation
Gases

Details

DOI: https://doi.org/10.4271/ARP748B

Pages: 2

Citation: SAE International Recommended Practice, Gas Turbine Engine Power Take-Off Pad Requirements, SAE Standard ARP748B, Stabilized February 2014, Revised February 2004, Issued December 1961, https://doi.org/10.4271/ARP748B.

Additional Details

Publisher: SAE International

Published: Feb 6, 2014

Product Code: ARP748B

Content Type: Recommended Practice

Status: Stabilized

Language: English

Historical