Gas Turbine Engine Power Take-Off Pad Requirements(STABILIZED Feb 2014)

Standard:
Stabilized:
  • 2014-02-06
 
  • CURRENT
Publisher:
  • SAE International
Pages:
2
Scope:

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

Rationale:

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

History:
Standard Published Revision Status
ARP748B 2014-02-06 Latest Stabilized
2004-02-23 Historical Revised
1995-05-01 Historical Reaffirmed
AKA:
  • SAE ARP 748
Sector:
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