Aircraft Hydraulic Starter/Pumps(STABILIZED Oct 2013)
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.
Rationale: This document has been determined to contain basic and stable technology which is not dynamic in nature.
Electrical, Electronics, and AvionicsFly-by-wire control systemsElectrical systemsElectromagnetic compatibilitySensors and actuatorsHybrid powerElectric hybrid powerPumpsFluid power systemsHydraulic systemsElectrohydraulicsHydraulic motorsFuel pumpsSafetyTests and TestingMissilesUnmanned aerial vehicles
Also known as: SAE AS 838
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