Updated National Stock Numbers

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

lockheed martin corporation ball bearing unit nsn 3130000152482. the alignment type is rigid

lockheed martin corporation. the general characteristics item description consists of 1 chain assembly 98.630 in. lgwith 1/4 pitch chain1 cable assembly 73.000 in. lgwith 0.062 in. dia wire rope and 1 rod assembly 3.770 in. lg

chain and cable assembly nsn 1560000152480. the end item identification is aircraft model c-141

chain and cable assembly nsn 1560000152479. the end item identification is aircraft model c-141

aircraft trailing edge nsn 1560000152471. the aircraft mission design series is c-141a

emergency ex panel nsn 1560000152474. aluminum alloyqq-a-250/13 is the general characteristics item description

aircraft structural panel nsn 1560000152470.

aircraft structural panel nsn 1560000152469. the material document and classification is qq-a-250 fed spec single material response

overall length 46.6in. ⁓46-39/64

aluminum material

aluminum material

material thickness 0.375 inches

material thickness 0.375 inches