Serving our customers with quality and safety first.
T-53 mfr 2915-01-216-9779
aluminum alloy, AMS4120, anodized finish, AMS2470, 63 microinch aa surface finish grooves, 125 microinch aa surface finish od, 250 microinch aa finish remaining surfaces, 2.455 in. min, 2.465 in. max o/a lg, stepped od, 0.306 in. min, 0.308 in. max od 1st step 1st end, 0.160 in. min, 0.166 in. max lg 1st step 1st end, 0.250 in. nom dia 2nd step 1st end, 1.643 in. min, 1.669 in. max lg 2nd step 1st end, 0.306 in. min, 0.308 in. max dia 1st step 2nd end, 0.609 in. min, 0.619 in. max lg 1st step 2nd end, 1 ext groove max lg 1st step 2nd end, 1 ext groove 1st step 1st end, 0.099 in. min, 0.109in. max w by 0.207 in. min, 0.211in. max dia groove, 0.048 in. min, 0.064 in. max distance from 1st end to groove, 2 ext grooves 1st step 2nd end, 0.099 in. min, 0.109 in. max w by 0.207 in. min, 0.211 in. max dia grooves, 0.071 in. min, 0.081 in. max distance from 2nd end to 1st groove, 0.480 in. nom distance from 2nd end to 2nd groove, chamfered od both ends, 0.020 in. min, 0.030 in. max lg by 45 deg chamfer 1st end, 0.040 in.
1EA
FSC 2915 ⁓ Engine fuel system components, aircraft and missile prime movers
Note-fuel components specially designed for propulsion fuel systems, aircraft and missiles are to be placed in this fsc.
Excluding aircraft fuel tanks (fsc 1560); in-flight refueling system fuel components (fsc 1680). fuel system components not specifically designed for use with aircraft engines or missile prime-movers.
Used on t-53 mfr 2915-01-216-9779.