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J-57 aircraft engine
length 1.130 to 1.160 in; height 2.270 to 2.290 in; width 1.060 to 1.070 in; hole for outer governor shaft 0.5905 to 0.6000 in; wall thickness 0.039 to 0.057 in; lip of shaft hole 0.110 to 0.120 in from shroud body, matl steel ams 5040/5042
control, compressor bleed A12110Aag, 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.