01-193-1858
Turbine Nonaircraft Gas Tu Rotor
Turbine rotor is 8.189 min to 8.193 max high
01-193-8104
Combustion Nonaircraft G Chamber
Used on auxiliary power unit,b1b acft. 5.400" overall length zholes 180 at 0.043 in. dia, 300 at 0.061 in. dia, 120 at 0.072 in. dia, 180 at 0.075 in. dia, 120 at 0.088 in. dia, 180 at 0.095 in. dia, 54 at 0.156 in. dia, 54 at 0.184 in. dia, 54 at 0.197 in. dia, 54 at 0.244 in. dia & 54 at 0.293 in. dia
01-194-4952
Turbine Rotor Nonaircraft Blade
01-194-4953
Turbine Rotor Nonaircraft Blade
01-194-4954
Turbine Rotor Nonaircraft Blade
01-194-4955
Turbine Rotor Nonaircraft Blade
01-194-4956
Turbine Rotor Nonaircraft Blade
01-194-4957
Turbine Rotor Nonaircraft Blade
01-196-2733
Axial Com Case And Vane Assembly
01-197-1939
Gearbox Turbine Engine Housing
01-197-8325
Accessory Drive Turbine Gearbox
Used on 2350-01-061-2445 tank,cmbt.
01-198-3766
Planetary Reduction Gear Carrier
Used on t62t eng.
01-199-4843
Combustion Chamber Turbine Case
Steel ams 5548; 2.410 in. w; 24.150 in. dia.
01-199-7842
Turbine Rotor Nonaircraft Blade
01-199-7848
Axial Compressor Turbine En Disk
01-200-3106
Planetary Reduction Gear Carrier
Check dwg 12321766 for more detail
01-200-9649
Gas Turbine Nonaircraft Engine
Engine, gas turbine
01-201-7366
Gearbox Parts Kit
01-202-5320
Lubricating Nonaircraft G Nozzle
Used on 2g-gtcp165 rn381380-2,-3,-4. 3.890" overall length body o.d. 0.195 in. min
01-202-5321
Lubricating Nonaircraft G Nozzle
Used on 2g-gtcp165 rn381380-2,-3,-4. 3.407" overall length
01-202-5322
Lubricating Nonaircraft G Nozzle
Used on 2g-gtcp165 rn381380-2,-3,-4. cadmium pl encl area per qq-p-416TY1 CL2 silver braze per mil-b-7883 7.077 in. min
01-202-5323
Lubricating Nonaircraft G Nozzle
Used on 2g-gtcp165 rn318380-2,-3,-4. cadmium pl encl area per qq-p-416TY1 CL2 silver braze per mil-b-7883 2.622 in. nom long, 0.200 in. nom dia; first shoulder 0.309 in. nom dia, groove 0.210 in. nom dia; second shoulder 0.369 in. nom dia, groove 0.274 in. nom dia; one mounting tab 1.250 in. nom long, 0.620 in. nom widemounting hole 0.222 in. nom dia; bore 0.102 in. nom dia, 0.252 in. nom depthcounterbore 0.1574 in. nom dia, 0.620 in. nom depth
01-202-5324
Lubricating Nonaircraft G Nozzle
Used on 2g-gtcp165 rn381380-2,-3,-4. cadmium pl encl area per qq-p-416TY1 CL2, silver braze per mil-b-7883. 3.502 in. nom long, 0.200 in. nom dia; first shoulder 0.308 in. nom dia, groove 0.211 in. nom dia; second shoulder 0.369 in. nom dia, groove 0.274 in. nom dia; one hole mounting tab 1.250 in.nom long, 0.620 in. nom wide, mountinghole 0.222 in. nom dia; bore 0.102 in.nom dia, 3.400 in. nom depth; counterbore 0.1574 in. nom dia, 0.140 in. nom depth
01-202-5325
Lubricating Nonaircraft G Nozzle
Used on 2g-gtcp165 rn381380-2,-3,-4. cadmium pl encl area per qq-p-416TY1, CL2, silver braze per mil-b-7883; 2.562 in. nom long, 0.200 in. nom dia, first shoulder 0.209 in. nom dia, groove 0.210 in. nom dia; second shoulder 0.369 in. nom dia, groove 0.274 in. nom dia; one mounting hole tab 1.250 in.nom long, 0.620 in. nom wide, mountinghole 0.222 in. nom dia; bore 0.102 in.nom dia, 2.450 in. nom depth, COUNTERBORE0.1574 in. nom dia, 0.140 in. nom deep
01-202-5326
Lubricating Nonaircraft G Nozzle
Used on 2g-gtcp165 rn381380-2,-3,-4. 1.497" overall length
01-203-0169
Compressor Nonaircraft Gas Vane
Used on 2350-01-087-1095. 0.770" overall length vane, turbine engine
01-203-0170
Compressor Nonaircraft Gas Vane
Used on 2350-01-087-1095. 0.750" overall length vane, turbine engine
01-204-2431
Turbine Rotor Nonaircraft Blade
01-204-3733
Lubricating Nonaircraft G Nozzle
Used on t62t-40lc apu b1b. 1.972" overall length silver braze per mil-b-7883; firstshoulder 0.308 in. nom dia, groove 0.2105 in. nom dia; second shoulder 0.369in. nom dia, groove 0.274 in. nom dia; one hole mounting tab 1.250 in. nom lg, 0.625 in. nom wide, mount hole 0.222in. nom dia; bore 0.102 in. nom dia, 1.865 in. nom deep; bore 0.1574 in. nom dia, 0.140 in. nom deep cadmium surface treated
01-205-0759
Fan Nonaircraft Ga Vane Assembly
Items are being coded as critical to insure source inspection will be performed at the point of manufacture, prior to material receipt by the us navy or other dod components. these items are piece parts or end items in support of vital military hardware necessary to sustain the successful mission of the ships, submarines,
01-205-0796
Compressor Nonaircraft Gas Rotor
Used on gas turbines and jet engines,except aircraft. rotor, compressor, gas turbine engine
01-205-1310
Lubricating Nonaircraft G Nozzle
Used on t62t-40lc apu b1b. 1.650 in. nom lg, 0.200 in. nom dia; one hole mounting tab 0.090 in. long, 0.560 in. wide; mpunting hole 0.222 in nom dia; connecting end 0.3525 in. nom dia, groove 0.2465 in. nom dia, 0.103 in. long; partial bore 1.555 in.nom depth, 0.0925 in. nom dia; side bore one wall thru 0.125 in. nom dia
01-205-1311
Lubricating Nonaircraft G Nozzle
Used on t62t-40lc apu b1b. 1.745 in. lg; one mounting hole tab w/ 0.221 in. dia. hole; connecting end groove 0.103 in. wide; partial bore 0.095 in. dia, 1.535 in. deep; side wall bore thru one wall 0.032 in. dia
01-205-1312
Lubricating Nonaircraft G Nozzle
Used on t62t-40lc apu b1b. 1.245 in. 1st end nom od; 0.380 in. connecting end nom od, groove 0.215in. nom dia; 0.103 in. nom wide; one hole mounting tab, 0.450 in. nom wide, mounting hole 0.222 in. dia; partial bore 1.115 in. nom deep; side wall borethru one wall 0.032 in. nom, center bore 0.120 in. dia
01-205-1313
Lubricating Nonaircraft G Nozzle
Used on t62t-40cl apu b1b. matl cres 300 series cond. a per qq-s-763; 1.040 in. lng, 1st end threads 0.3125-24 unf-2a, 1st end groove 0.2525 in. nom dis, 0.100 in. wide; flange 0.180 in lng; 2nd end 0.500 in. od; hex head 0.3725 in. across; bore 0.540in. nom dia, cbore 0.145 in. nom dia, 0.800 in. nom deep
01-205-1314
Lubricating Nonaircraft G Nozzle
Used on t62t-40cl apu b1b. 2.425" overall length 0.190" overall width first shoulder 0.288 in. nom dia; groove 0.103 in. lng, 0.183 in. dia; 2nd shoulder 0.3525 in. lng; groove 0.247 in. nom dia, 0.103 in. nom wide; one hole mounting tab 0.065 in. lng w/ hole 0.222 in. dia; partial bore 2.230in. lng, 0.0925 in. nom dia; cbore 0.1574 in. dia, 0.140 in. deep; side borewall thru 0.032 in. nom dia
01-205-1315
Lubricating Nonaircraft G Nozzle
Used on t62t-40cl apu b1b. 2.195" overall length 1stshoul 0.319 in. nom dia, groove 0.215 in. nom dia, 0.103 in. lng; 2nd shoulder 0.378 in. nom dia, groove 0.213 in. nom dia, 0, 146 in. nom lng; one mounting hole tab 0.130 in. lng, 0.500 in. wide, mounting hole 0.282 in. dia, bore 0.032 in. dia; cbore 0.1257 in. nom dia, 1.950 in. nom deep
01-205-1316
Lubricating Nonaircraft G Nozzle
Used on t62t-40cl apu b1b. 2.240" overall length one mounting hole tab 0.095 in. nom lng, 0.440 in. wide, mounting hole 0.222 in. nom dia; connecting end 0.319 in. nom dia; groove 0.215 in. nom dia, o.103 in. lng; partial bore 0.094 in. nom dia, 2.240 in. nom deep; side bore one wall thru 0.032 in. nom dia, cbore 0.125 in. dia
01-205-3976
Accessory Drive Turbine Gearbox
01-205-8176
Axial Compressor Turbine En Case
01-206-0085
Gearbox Turbine Engine Housing
01-207-1798
Dirt And Liquid Deflector
0.7565" inside diameter 1.060" outside diameter 0.050" material thickness welded on cres tube, 0.8125 in. od; 0.028 in. wall thk; end cut at angle; 4.075 in. lg at ctr; mounting hole on tab of flange; fluorescent penetrant inspected round, flanged
01-208-0169
Accessory Drive Turbine Gearbox
01-208-0809
Combustion Nonaircraft G Chamber
01-208-3670
Accessory Drive Turbine Gearbox
Used on aviation ground power system (includes: electrical-dc +28 v at 700 amo maximum; ac =115-230 v, 30 kv at 400 hz maximum, ac = 110, 60 hz at 500 w maximum; hydraulic--3,300 lb at 15 gpm maximum; pneudraulic--60 lb pm at 40 psi maximum) other aircraft categories.
01-208-4430
Gearbox Turbine Engine Housing
01-208-4431
Lubricating Nonaircraft G Nozzle
Used on apu p/n381380-2-2 b1b. 2.095" overall length one hole mounting tab 0.430 wide, mounting hole 0.208 in. nom dia; mounting end 1st shoulder 0.4195 in. dia, groove 0.3095 in. nom dia; 2nd SHOULDER0.2195 in. dia, groove 0.185 in. nom dia; partial bore 0.800 in. dia, 1.970 in. deep; sidebore thru one wall 0.0155 in. dia
01-208-4433
Lubricating Nonaircraft G Nozzle
Used on apu p/n381380-2-2 b1b. 1.745" overall length one mounting hole tab 0.430 in. nom wide w/mounting hole 0.208 in. nom dia; mounting end 1st shoulder 0.4195 in. dia, groove 0.3095 in. nom dia; 2nd shoulder 0.291 in. dia, groove 0.185in. nom dia; bore 0.024 in dia, cbore 0.080 in. dia by 1.630 in. deep
01-209-0103
Thermal Nonai Insulation Blanket
Used on part of apu p/n 381380-2-2 b1-b acft,gtcp165-7 eng. cres foil 0.002 stock per mil-s-6721; 5.30 in. nom lg; first end 9.80 in. om od, second end 10.69 in. nom od; insulation per TMS0814 0.38-0.50 thk
01-209-3122
Fan Nonaircraft Gas Vane Segment
Used on aircraft engine model j52-p-8a.
