SAE AS838A

Aircraft Hydraulic Starter/Pumps(STABILIZED Oct 2013)

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Standard:
  • AS838
  • Revision: A
Revised:
  • 2013-10-28
Issuing:
  • A-6c6 Power Sources Committee
Scope:

This specification established (1) the common requirements for hydraulic units capable of functioning as starters and as pumps suitable for use in aircraft and missiles and (2) the methods to be used for demonstrating compliance with these requirements.

History:
StandardPublishedRevisionStatus
AS838A2013-10-28LatestStabilized
AS8381968-01-31HistoricalReaffirmed
AKA:
  • SAE AS 838
Sector:
  • Aerospace
Topic:
  • Electrical, Electronics and Avionics
  • Fly-by-wire control systems
  • Electrical Systems
  • Electromagnetic compatibility
  • Sensors and Actuators
  • Hybrid power
  • Electric hybrid power
  • Fluid power systems
  • Hydraulic systems
  • Electrohydraulics
  • Hydraulic motors
  • Fuel pumps
  • Safety
  • Tests and Testing
  • Missiles
  • Unmanned aerial vehicles

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