Updated National Stock Numbers

u s army tank automotive command. the component document origin is government

u s army tank automotive command. the end item source is 19207

lockheed martin corporation nose tube assembly nsn 1560000152542.

lockheed martin corporation canopy latch shim nsn 1560000152541.

lockheed martin corporation fusel tube assembly nsn 1560000152540.

nonmetallic hose assembly nsn 4720000152539. the sectional shape style cross is round

lockheed martin corporation fusel tube assembly nsn 1560000152538.

lockheed martin corporation fusel tube assembly nsn 1560000152537.

lockheed martin corporation fusel tube assembly nsn 1560000152536.

e and b discount marine. the mounting method is unthreaded holes

lockheed martin corporation. the overall width is 5.420 inches

check valve s shim nsn 2915000152515. the end item identification is 29158931551

triumph engine control systems llc. the 29158931551 is the end item identification

triumph engine control systems llc. the 29156755376 is the end item identification

triumph engine control systems llc. the material is steel comp 302

triumph engine control systems llc. the aperture diameter is 0.095 inches minimum and 0.097 inches maximum

shutoff lever and bearing nsn 2915000152503. the end item identification is tf33 aircraft engine

adjusting lever nsn 2915000152502. the tf33 aircraft engine is the end item identification

hamilton sundstrand corporation. the main fuel control 572100 for tf33 aircraft engine is the end item identification

idler plate nsn 2915000152499. the end item identification is tf33 aircraft engine

hamilton sundstrand corporation. 2915-954-9585 is the end item identification

spring holder nsn 5340000152497. the material is steel corrosion resisting

spring holder nsn 5340000152496. the usage design is for holding torsion spring p/n 581519.

speed set leve stop nsn 2915000152495. the end item identification is the main fuel control p/n 572100 for tf33 aircraft engine

hamilton sundstrand corporation sleeve bushing nsn 3120000152494. the overall length is 0.2750 inches

idle reset lever nsn 2915000152493. the end item identification is tf33 aircraft engine

hamilton sundstrand corporation. the general characteristics item description is d3.695 in. lg o/a; hole both ends 0.311 - 0.312 in. dia; hole top center0.250-20unc-3b thddistance hole cen to bracket base 0.92 in; part of idle reset assy 581516 for

lockheed martin corporation. the general characteristics item description is matl spec 992finish c-19-24type iii alheat treat 180000-200000 psi

lockheed martin corporation. the general characteristics item description is steelmil-s-5000

lockheed martin corporation. steelmil-s-6758condition d-43.380 in. lg1.562 in. id2.330 in. od is the general characteristics item description