01-185-1864
Afterburner Turbine Fuel Control
Used on tf30-p-3 aircraft engine.
01-185-4018
Pump Centrifugal Impeller
Used on main fuel pump,708000,for f100 aircraft engine. chrome plate .002 - .004 in. thk bottom inside dia passivate surface treated
01-186-2444
Fuel Component Engine Adjustor
Used on main fuel pump,708000,for f100 aircraft engine.
01-186-7870
Float Aircraft Fuel Tank Valve
Used on aircraft model f-18.
01-187-0579
Fuel Jet Engine Pump
01-187-4259
Main Turbine Engine Fuel Control
Used on u/o apu t62t40lc-2; e/i kc135r acft.
01-187-6627
Actuator Valve Special Diaphragm
01-188-2647
Fluid Filter Element
0.13 in. thk mounting w/0.437-20unf-3a thd, 0.187 in. internal hex; 0.008 in. nom screen hole size, 0.090 in.nom open screen area
01-188-3774
Fluid Filter Element
Wash filter assy used on unified control fj-A3/5 for F100 acft engine
01-188-5202
Fuel Injection Nozzle
Used on general electric cf700 engines on rockwell international sabreliner 80 aircraft.
01-189-0276
Submerged Aircraft Pump Assembly
01-189-4223
Fuel Pump Cover
Used on fuel pump,704300-4,for f108 engine. cover assembly, pump, fuel cage 58825 p/n 301-776-104-0
01-190-9221
Aircraft Engine Tube Assembly
Used on acft eng tf33. 36.340" overall length
01-190-9242
Fuel Injection Nozzle
Used on f108-ge aircraft,turbo fan engine,main. t.o.2j-F108-4, figure 51
01-191-1886
Fuel Jet Engine Pump
Used on f110-ge-100 acft engine.
01-191-5702
Main Turbine Engine Fuel Control
Used on turbo prop engine model t-58.
01-191-8596
Fluid Filter
Rdischarge port seal area 1.685 in. id, 2.375 in. od; inlet port seal area 1.181 in. id, 2.745 in. min od; threaded cover 4.000-12unj-3a, 3.70 in. dist inlet port cen to end of hex wrenching facility 1.50 in. across flats
01-192-0846
Fuel Jet Engine Pump
Used on f110-ge-100 acft engine. fscap
01-192-0847
Fuel Metering And Distribut Pump
Used on f110-ge-100 aircraft engine. pump, fuel boost fscap
01-192-5419
Main Turbine Engine Fuel Control
Used on f108 acft engine for kc135r acft.
01-192-6826
Fuel Injector Assembly
Used on 2j-f100-24. sleeve
01-193-4771
Valve Body
Synthetic rubber mil-r-6855, class 1, grade 60 (precision composition number 7186) ; 1.000 in. wide; 1.060 in. long
01-195-9537
Fuel Jet Engine Pump
Used on targets, surface to air missiles.
01-196-4362
Submerged Aircraft Pump
Used on c130 acft fuel system.
01-196-8281
Electro-mechanical Line Actuator
01-197-6485
Fuel Cam Actuated Pump
01-197-6558
Fuel Injection Nozzle
Used on oh-58d turbine engine (t703-ad-700). 2.5mm overall length 1.1mm overall width flight safety critical aircraft part
01-197-8176
Electro-mechanical Rota Actuator
01-198-0148
Main Turbine Engine Fuel Control
Used on jet engine model f-104.
01-198-0149
Fuel Pressurizing And Drai Valve
Used on jet engine model f-104.
01-198-2003
Fuel Control Housing
Used on f108-ge aircraft engine. vbv case assembly match assembly with p/n 5255-267
01-198-3710
Fuel Control Housing
Used on main fuel control,p/n 8062-469,for f108 acft eng. housing assy. throttle & shutoff part of shaft assy 5355-254 for hsg assy 6016-657. anodize surface treated
01-198-9678
Fuel Jet Engine Pump
01-199-5255
Fuel Jet Engine Pump
Used on f101-ge-102 engine,b-1b acft.
01-199-7449
Main Turbine Engine Fuel Control
Used on j85-ge-21/21a/21b aircraft eng.
01-199-9759
Valve Piston
Used on main fuel control,p/n 8062-469,for f108 acft eng. 2.200" overall length part of valve assy 5252-009; alum alloy per ams 4117; 1.311 in. od o/a; groove 0.105 in. w x 1.18 in. dia; 0.937 in. max id
01-200-0119
Afterburner Turbine Fuel Control
Used on f110-ge-100 acft engine. fscap
01-200-0120
Main Turbine Engine Fuel Control
Used on f110-ge-100 acft engine.
01-200-3495
Valve Piston
Used on main fuel control,p/n 8062-469,for f108 acft eng. part of v.b. valve assy 5255-141
01-200-9564
Main Turbine Engine Fuel Control
01-201-6783
Main Turbine Engine Fuel Control
Used on f100-pw-200 acft engine.
01-201-7765
Pump Centrifugal Impeller
Used on u/o fuel pump.
01-201-7766
Pump Centrifugal Impeller
Used on u/o pump element assy pn 395600; 395800; 396400. 5.344" overall width anodize surface treated
01-201-7767
Pump Centrifugal Impeller
Used on u/o pump element assy pn 396100; 396300; 396600. 2.807" overall width anodize surface treated
01-201-7804
Valve Disk
Used on u/o valve,dual shut pn 2750045-101 nsn 2915011783442. 0.603" inside diameter
01-201-7806
Actuator Valve Special Diaphragm
Used on u/o valve dual shut pn 270045-101 nsn 2915011783442. 0.190" hole diameter 0.014" material thickness 0.605" center hole diameter 4 bolt hole quantity special shaped
01-202-3228
Valve Cap
Used on pilot valve,2710738m3,b-1b aircraft fuel system. alum alloy 6061-T651 per qq-a-225/8, anodize; 0.46 in. h, 0.70 in. od w/0.838 in. dia flange 0.060 in. thk, 0.625 in. id; hole thru top cen 0.135 in. dia, 4 holes thru wall eq sp 0.12 in. dia
01-202-6393
Valve Disk
Used on pump unloading valve assembly;to.6j3-4-113-4,f.2-14-203. c/o rotor 3396-076, rotor 3396-068, sleeve 3515-110, sleeve 3515-042 poppet
01-202-6432
Fuel Injection Nozzle
Used on f108-ge aircraft,turbo fan engine,main. t.o.2j-F108-4, figure 51
01-203-4644
Valve Disk
Used on main fuel control,p/n 8062-469,for f108 acft eng. second step disc end 0.328 - 0.333 in. dia, 0.063 in. h w/center bore 0.105 in. dia, 0.350 - 0.400 in. dp; hole 0.312 in. cen-to-disk end 0.072 in. dia poppet
