Updated National Stock Numbers

nwl transformers. the body length is 7.750 inches

m. t. davidson company. the keyway width 0.187 inches

valve op gage glass nsn 4470000152559. the criticality code justification is zzzy

u s army tank automotive command. the thickness is 0.020 inches.

trim vane catch nsn 2540000152556. the general characteristics item description is 7steelsheetfed qq-s-698composition 1008 to 1020hr or crcommercial qualityolive drab finish0.120 in. thk material4-1/2 in. o/a lg by 2-3/32 in. o/a wone 1-1/8 in. d

u s army tank automotive command. the basic shape style is rectangular

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