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solid propellent cartridge, af type MXU-4/a, w/provisions for air turbine starting, 50.0 psi air inlet pressure, 95.0 lb per min flow, max elec data, 32 v, 3 amp, dc, ccw drive rotation viewing output shaft, drive spline data, 24 teeth, 20/30 pitch, 1.200 in. pitch dia, 1.090 in. min dia, 1.2645 in. max dia, 0.700 in. lg, mtg data, std mtg, an, AND10266, type xvi&a, w/quick detachable mtg
starter, engine, gas turbine
1EA
Schedule B number: 8411997050
nmfc 114215
Parts of gas turbine aircraft engines, other than for use in civil aircraft
FSC 2995 ⁓ Miscellaneous engine accessories, aircraft
Note-items classified in this class must be specifically designed for use with aircraft or quided missile primemovers only.
Excluding exhaust system; (fsc 1560); jet engine hydraulic reservoirs (fsc 2840); jet engine oil tanks (fsc 2840); electrical starters (fsc 2925); cockpit mounted control quadrants (fsc 1680); aircraft engine covers (fsc 1730).
Nothing similar to this part number was found in our inventory
An item designed to accelerate a gas turbine engine from rest to starter cutoff speed by means of a combustion gas driven turbine and reduction gear assembly constructed to be mounted on the engine starter drive. the combustion gas is generated from ignited liquid fuel and air in the combustion chamber or from a solid propellant cartridge attached to the combustion chamber of the starter. may have provision for energizing the turbine by low pressure air from engine bleed or ground equipment air supply.