6675-99-285-4054

Documents 6650-99-605-8619 5+ Documents ( More... ) https//www.nsnlookup.com /fsg-66/fsc-6675/uk 6675-99-285-4054
Case Surveying Inst 6675992854054 992854054 More... ) https//www.nsnlookup.com /cage Leica Geosystems

4 19 Jul 1995 6650-99-605-8619 Stereo Module 10445295RNCC: 3 | RNVC: 2 | DAC: 4 22 Nov 2001 6675-99-285-4054

2840-01-182-0430 2840011820430 011820430 is a component of a vane assembly, compressor, aircraft gas turbine engine. it is designed to receive air from the preceding compressor blades and deliver it to the succeeding row of compressor blades, diffuser, or combustion area at correct pressure, velocity and direction.

2840-00-138-9358 2840001389358 001389358 is inc 61701 reinstated on 112113~inc 61701 cancelled/replaced by ,inc 50614, fiig a10700, app-key a ,inc 50613, fiig a10700, app-key a ,inc 50612, fiig a10700, app-key a ,inc 50611, fiig a10700, app-key a ,on 100112 ~(all except usa) for usa inc 61701 canceled replaced by vane, turbine engine: inc 40963, fiig a107, appl key a. an item spaced radially in a nozzle, turbine, turbine engine, located between the inner and outer shroud of the nozzle unit, designed for the function of directing hot gases to the turbine at a proper velocity and angle.

2840-01-180-4229 2840011804229 011804229 is a component of a vane assembly, compressor, aircraft gas turbine engine. it is designed to receive air from the preceding compressor blades and deliver it to the succeeding row of compressor blades, diffuser, or combustion area at correct pressure, velocity and direction.