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J-57 aircraft engine
steel, ams 5610; rockwell c 26-32; length 0.970 in; dia 1.170 in; clevis end; outside clevis width 0.540 in to 0.550 in; inside clevis width 0.280 in to 0.290 in; clevis length 0.450 in; clevis end has 2 pin holes 0.1560 to 0.1564 in; inside dia 1.0236 TO1.0246 in chamfered 30 deg to dia 1.050 to 1.070 in
body group, speed set fscm 11599, p/n 6A12354A, 6A12981A, 6A12758A, 6A12715A for control, compressor bleed p/n A12110Ahg, A12140Ky, A12702Ahf, A12715Rr, A12902Ajc, A12902Ajj, A17101Rr
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 j-57 aircraft engine.