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aneroid body group 6A12355A, J57 compressor bleed control
two holes 1.122 in to 1.128 in between centers; leg located at one end; 0.260 in at end of leg is annealed to rockwell C26-32; lever finish induction anneal to rockwell c 20-36; chrome plated
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 aneroid body group 6a12355a,j57 compressor bleed control.