SAE AS44 Starter, Mounting Pads and Drives - Types I, II, III & IV (NONCURRENT Aug 1973)
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Product Code:SAE AS44
Title:Starter, Mounting Pads and Drives - Types I, II, III & IV (NONCURRENT Aug 1973)
Issuing Committee:E-25 General Standards For Aerospace And Propulsion Systems
Scope:To establish essential minimum safe performance standards for Automatic Pilots primarily for use with turbine powered subsonic transport aircraft, the operation of which may subject the instrument to the environmental conditions specified in Section 3.3. This Aerospace Standard covers Automatic Pilots intended for use on aircraft to automatically operate the primary and trim aerodynamic controls to maintain stable flight and/or to provide maneuvering about any of the three axes through servo control. Automatic control functions essential for primary or augmented flight control are excluded.
MIL-DTL-83420L, DETAIL SPECIFICATION: WIRE ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL, GENERAL SPECIFICATION FOR (20 NOV 2002) [SUPERSEDING MIL-W-83420]., This specification covers the requirements for carbon steel and corrosion resistant steel aircraft control flexible wire rope. Type I wire rope will be capable of operation within a -65 degrees F to +250 degrees F (-54 degrees C to +121 degrees C) temperature range in wind, dust, fuel, and oil spills, in wash-down and other environmental stresses and aircraft experiences. Type II wire rope will be capable of operation within a -65 degrees F to +200 degrees F (-54 degrees C to +94 degrees C) temperature range in wind, dust, fuel, and oil spills, n wash-down and other environmental stresses and aircraft experiences.MIL-PRF-12934J (SUPPLEMENT 1), PERFORMANCE SPECIFICATION: RESISTORS, VARIABLE, WIRE WOUND, PRECISION, GENERAL SPECIFICATION FOR (1 FEB 1999) [SUPERSEDING MIL-R-12934H]., This supplement forms a part of MIL-PRF-12934J, dated 1 February 1999.