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F100-PW-200/-220 (F-16A/b/c/d, F-15C/d/e) aircraft engines
no. of teeth 3; diametral pitch 2.5; pressure angle 30 deg.; helix angle 45 deg. ref.; lead 3.7699; pitch dia. 1.2000 ref.; this part mates with p/n 2668807 (nsl) ; material 2668466 cres investment casting rh "c" 32-38; similar to p/n 2668806, nsn 2915012489006, rotor; item converts air preesure to rotorational energy used on engine
1EA
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).
Used on f100-pw-200/-220 (f-16a/b/c/d, f-15c/d/e) aircraft engines.