01-195-9627
Aircraft Engine Maintenan Heater
Circular configuration with insulated handles; company item name-heater
01-195-9628
Test Adapter
Used on f-4 acft age. c/o front panel; case
01-195-9629
Stores Management Syste Test Set
Used on f-16 acft age..
01-196-0029
Test Program Set
Used on b-1b acft age.. c/o i/o interface; ita
01-196-0031
Test Program Set
Used on b-1b acft age.. c/o i/o interface; ita
01-196-0327
Machining Aircraft Engin Fixture
Used on f100-pw-100/200/220/220e aircraft engine. company item name-fixture machine, 2nd stage compressor vane recontour vane foot repair
01-196-0328
Engine Maintenance Aircr Fixture
Used on f100-pw-100/200 engine. aluminum; company item name-fixture mold, 1st stage fan case rear seal partial rubber repair
01-196-0329
Engine Maintenance Aircr Fixture
Used on f100-pw-100/200 engine. aluminum; company item name-fixture mold, 2nd stage fan case rear seal, partial rubber repair
01-196-0330
Engine Maintenance Aircr Fixture
Used on f100-pw-100/200 aircraft age.. steel
01-196-3037
Indicator Test Set
01-196-3459
Plasma Spray Mask
Used on f100-pw-100/200 aircraft engine. 9.200" overall length steel; company item name-plasma spray fixture
01-196-3465
Engine Maintenance Aircr Fixture
Used on f100-pw220/220e engines. fixture c/o dual steel ring with center post used with PWA55380
01-196-3466
Engine Maintenance Aircr Fixture
Used on f100-pw-100/200n aircraft engine. steel; company item name-adapter
01-196-3472
Aircraft Maintenance Fixture
Used on f101-ge-102 engine. material: steel, sae 1010-1020
01-196-3473
Aircraft Maintenance Fixture
Used on c-5a acft age./odru.
01-196-3580
Maintenance Aircraft Engin Stand
3.500 feet overall length 3.333 feet overall width
01-196-3709
Aircraft Maintenance Fixture
Used on b-1b acft. c/o eoisting ring 1; adjustable strap 1; spreader bar 1; steel pin 2; material: steel
01-196-4043
Special Purpose E Cable Assembly
Used on f-18 acft.
01-196-4083
Aircraft Maintenance Fixture
Company item name-holding fixture, valve
01-196-4239
Aircraft Maintenance Fixture
Used on kc-135r acft age.. c/o mechanical assembly 12.000 in. dia, 5.000 in. lg, p/n 93951-01; mechanical assembly, 12.000 in. dia, 7.000 in. lg, p/n 93951-02; y-bar assembly, 20.000 in. lg, 10.000 in w, 1.000 in h, p/n 93951-03; dwg title restraining fixture, load compressor wheel
01-196-4240
Aircraft Maintenance Fixture
Used on kc-135r acft age.. c/o distribution block w/hydraulic fittings; company item---name, test fixture
01-196-4241
Engine Maintenance Aircr Fixture
Used on f100-pw-100/200 aircraft engine. drill fixture on mobile cart with casters, floor locks, toggle clamps, oiler, filter regulator, hose, special right angle drill with air driver
01-196-4242
Engine Maintenance Aircr Fixture
Used on f100-pw-100/200 engine. steel; company item name-fixture
01-196-4255
Engine Maintenance Aircr Fixture
Used on f100-pw-100/200/220/220e engine support equipment. company item name-fixture, drill/ream, gearbox housing
01-196-4256
Engine Maintenance Aircr Fixture
Used on f100-pw-100/200/220/220e engine support equipment. steel; c/o drill guide plate, diamond pin, stud
01-196-4258
Engine Maintenance Aircr Fixture
Used on f100-pw-100/200 engine age.. steel
01-196-4267
Aircraft Maintenance Fixture
Used on b-1b aircraft age..
01-196-4273
Test Adapter
Used on b-1b acft age. adapter kit-constant speed drive
01-196-4274
Aircraft Maintenance Fixture
Used on b-1b acft. bc/o an actuator-holding mount
01-196-4285
Aircraft Maintenance Fixture
Used on b-1b acft. c/o base plate with eight removable planet gear alignment rods
01-196-4287
Pressure Test Adapter
Used on f100-pw-200/229 engine. 12.000" overall length c/o an l shaped quick disconnect adapter 1 in. dia, which attachs test cart to the quick access rear compressor variable vane test fittings
01-196-4290
Aircraft Maintenance Fixture
Used on 4920011273247,f-16 aircraft age.. 7c/o:cover (p/n 16U1908-45) 1, plenum assy (p/n 16U1908-59) 1, plate assy (p/n 16U19080-77) 1, plate assy (p/n 16U1908-78) 1, fixture assy (p/n 16U1908-85) 1, board assy (p/n 16U1910-801) , connector 10; fsc application data:adapter, central interface unit;
01-196-4296
Stores Management Syste Test Set
Used on f-16 acft.
01-196-4297
Stores Management Syste Test Set
Used on f-16 acft.
01-196-4298
Stores Management Syste Test Set
Used on f-16 acft.
01-196-4303
Stores Management Syste Test Set
Used on f-16a/b acft age..
01-196-4325
Aircraft Maintenance Fixture
Used on b-1b acft. c/o open box-shaped structure with oversize hole in bearing end which allows for ejection of the bearing during removal
01-196-4326
Interface Devic Adapter Assembly
Used on b-1b acft.
01-196-4327
Aircraft Maintenance Fixture
Used on b-1b acft. c/o a skid with fixed
01-196-4488
Frequency Multiplier
Used on f-16 acft age.. 7.000" overall length 1.500" overall width
01-196-5973
Aircraft Maintenance Fixture
Used on f110-ge-100 engine support equipment. c/o 3 steel plates; 1 steel tube, 1 steel cap plug; 1 drain tube cap plug
01-196-5974
Aircraft Maintenance Fixture
Used on f110-ge-100 engine. c/o external retaining ring; expanding arbor; arbor protector; molded devices, spider
01-196-5975
Aircraft Maintenance Fixture
Used on f110-ge-100 acft eng age. c/o 2 brackets w/partial bolt circle for connection to the front frame aft flange
01-196-5988
Aircraft Maintenance Fixture
Used on b-1b acft age.. steel; there are 4 holes 0.500 in. dia, and 3 holes 0.250 in. dia.
01-196-5989
Interface Devic Adapter Assembly
Used on f100-pw-200/229 engine. c/o an l shaped quick disconnect adapter, 1 in. dia which attaches the test cart to the quick acess rear compressor varible vane test fittings
01-196-5990
Engine Maintenance Aircr Fixture
Used on f100-pw-100/200/220/220e aircraft engine. stainless steel; c/o structure with combination chill bar/expanding mechanical arbor; company item name-fixture
01-196-5991
Hydraulic System Compone Fixture
Used on f110-ge-100 engine support equipment. company name-locating fixture, actuator; steel
01-196-5996
Interface Devic Adapter Assembly
Used on f-109-ga-100 turbofan engine.
01-196-6010
Aircraft Maintenance Fixture
Used on b-1b acft support. hmaterial aluminum
01-196-6012
Engine Maintenance Aircr Fixture
Used on tf-41 eng age.. matl:sae 01, rockwell c 55-60 hardness, black oxide ams 2485 surfact treatment; 4.651 in min 4.655 in. max dia; 0.500 in h; contains 8 holes equally spaced on 2.750 in. dia, 0.880 in. dia thru; countersunk 90 deg to 1.000 in. dia on both sides; contains one hole centrally located 1000 in. dia thru; countersunk 90 deg to 1.120 in dia on both sides; dwg title, plug-alignment runout, inner stage turbine seal (help)
