01-106-9393
Push-pull Control Assembly
Used on mh/sh/uh-60 aircraft.
01-106-9396
Push-pull Control Assembly
Used on uh-60a/sh-60b/hh-60h; helicopter,carrier based asw, sh-60f; helicopter, electronic countermeasures, eh-60a; aircraft black hawk (mh-60k special operations aircraft); helicopter, uh-60a/uh-60d; helicopter, seahawk, h-60; hh-60l medivac.
01-107-2645
Aircraft Pod
Used on multi acft. 130.000" overall length
01-107-2666
Mechanical Aircraft Actuator
Used on c-130j acft. actuator assy, trim tab
01-107-3346
Electro-mechanical Rota Actuator
01-107-3349
Aircraft Seat
01-107-3350
Aircraft Seat
01-107-3351
Aircraft Seat
01-107-3485
Fault-function Indicator A Panel
01-107-5986
Wiring Harness
F-16 aircraft
01-107-8563
Aircraft Seat
Used on c-130 aircraft. 27.000" overall length 21.188" overall width headrest material - naugahyde
01-108-0384
Aircraft Safety Belt
01-108-0558
Aircraft Seat
Used on uh-60, rotary wing aircraft.
01-108-0612
Fault-function Indicator A Panel
01-108-2895
Aircraft Safety Belt
01-108-3136
Branched Wiring Harness
Used on f-16 aircraft. sc/O2 connectors; 2 wafers; tape as required; contacts as referenced; plugs as required; 2 receptacles; 9 endbells; sleeving as required; 25 terminals; 3 splices; exact wire length to be determined on first installation; braid per 16PR106
01-108-3661
Electro-mechanical Rota Actuator
01-108-3682
Shoulder Harness Inertia Lo Reel
01-108-6542
Aircraft Control Wheel
Material aluminum alloy, mounting 90.0 deg internal straight 48 tooth serration 1.000 in. major dia, copilot wheel
01-108-7183
Aircraft Glareshield
Used on f-16 aircraft. 11.750 in.wide; metal removal per fps-3017; mark x-ray serial no per fps-3008, class 1a; other inspection markings to be fps-3008 class 2a; class a inspection in accordance with fps-100/; all dimensions to be taken from planes established by tooling check points; straighten within 0.050 in.; location of parting planes optional; mismatch 0.010 max; all web
01-108-7422
Branched Wiring Harness
01-108-7993
Mechanical Aircraft Actuator
Dactuator, rotary, front wheel; altered part per drawing 58313-40147, bottom ports to be plugged by vendor, markings
01-108-8034
Aircraft Glareshield
Used on f-16 aircraft. fsc application data:aircraft accessories equipment;
01-108-8035
Aircraft Glareshield
Used on f-16a aircraft. gc/o:nuts p/n NAS1068RA06, MS32075L3; rivet p/n MS20426AD4, MS20426AD3, MS20426AD2; spacer p/n 16F0128-9; support p/n 16F0128-7; glareshield p/n 16F0128-41; fsc application data:glareshield, thermal radiation;
01-108-9659
Aircraft Pod
Used on multiple fighter/trainer acft. 130.000" overall length
01-108-9660
Aircraft Pod
Used on multiple fighter/trainer acft. 130.000" overall length
01-108-9681
Branched Wiring Harness
Used on f-16b aircraft, tail effectivity 62 0003 0003; 62 0005 0005; 62 0025 0051. forward station flight instruments
01-108-9682
Branched Wiring Harness
Used on f-16b aircraft, tail effectivity 62 0003 0003; 62 0005 0005; 62 0025 0051. communications right crew compartment; used on 16D21824-1; components: cap 2; connector 2; waffer 8; contact, plug, tape as required; exact length to be determined on first installation; braid harness per 16PR106; dead end W575-040-20 at 2739P311b
01-108-9689
Branched Wiring Harness
Used on f-16 aircraft. c/owafers as referenced; tape as required; contacts as referenced; plugs as referenced; 3 splices; 1 endbell; sleeving as required; 6 washers; 3 nuts; 3 screws; 4 terminals; exact length to be determined on first installation; solder per mil-std-454d requirement 5; braid harness per 16PR106
01-109-4808
Aircraft Glareshield
Used on f-16b acft. c/o:4 nuts; rivets as required; 1 spacer; 1 support; glareshield; 11.750 in.wd; fsc application data:glareshield, aircraft;
01-109-4830
Wiring Harness
01-109-4844
Branched Wiring Harness
Used on f-16a acft. c/O6 wafers; 1 connector; tape as required; contacts as referenced; plugs as required; 7 splice; 5 bus; 6 endbells; sleeving as required; 4 washers; 2 nuts; 2 screws; 14 terminals; 1 receptacles; 2 caps; exact length to be determined on first installation; braid harness per 16PR106
01-109-4845
Branched Wiring Harness
Used on f-16a aircraft. aoa tone gen aoa indicator; components: wafer p/n 16VE049011-12, -11; tape p/n P5372-1-1; plug p/n M83723/75R1624n, /28-20; splice p/n C4812-33, NAS1744-3; endbell p/n C8822-1-16; sleeving p/n C8844-2; washer p/n AN960PD61; nut p/n MS21042L06; screw p/n NAS1101-06-6; terminal p/n M7928/1-13; solder per mil-std-454d, requirement 5; braid harness per 16PR106
01-109-4858
Branched Wiring Harness
Used on f-16a/b acft. c/O4 connectors; 5 wafers; actuatorreferenced; tape as required; 7 contacts; plugs as required; switches as referenced; 1 endbell; 3 tubing; sleeving as required; 1 terminal; exact wire length to be determined on first installation; braid per 16PR106
01-109-4860
Branched Wiring Harness
Used on f-16a/b acft. jc/O3 wafers; 1 connector; tape as required; contacts as referenced; plugs as required; 10 endbells; sleeving as required; 1 receptacle; 4 terminals; exact length to be determined on first installation; braid per 16PR106
01-109-4862
Branched Wiring Harness
Used on f-16a aircraft, tail effectivity 61 0262 9999. components: connector 3; endbell 2; terminal 5; waffer 5; contact, plug, sleeving, tape as required; battery as referenced; braid harness per 16PR106, exact length to be determined on first installation
01-109-4873
Branched Wiring Harness
Used on f-16a acft. c/O6 connectors; 12 wafers; light, rnav, light, l nav as referenced; 2 receptacles; tape as required; contacts as referenced; plugs as required; 1 splice; 3 bus; 9 endbells; sleeving as required; 20 terminals; braid harness per 16PR106; exact length to be determined on first installation
01-109-5273
Wiring Harness
01-109-6214
Aircraft Safety Lap Bel Actuator
01-110-1811
Aircraft Seat
Used on uh-60a helicopter.
01-110-5331
Aircraft Load Balancing Computer
01-110-5879
Aircraft Seat
01-111-4392
Push-pull Control Assembly
01-111-4393
Push-pull Control Assembly
01-111-9586
Gearbox Parts Kit
Used on 1680-00-867-1479.
01-112-2653
Aircraft Glareshield
Used on f-16a/b aircraft. functional description:pilot aft rh; used on 16F1291-803; height 10.120; type/model designation:f-16 air combat fighter; tail effectivity 61 0262 9999; fsc application data:aicraft accessory equipment;
01-112-3591
Aircraft Safety Belt
01-113-0173
Seat Back Aircraft Cushion
01-113-1857
Quadrant Control Assembly
Used on f16a,f16b. aft station; grip w/improved ant elev thumbwheel to quadrant
01-113-1858
Quadrant Control Assembly
Used on f-16a/b aircraft. 1 light; 1 liner; 1 grip assy; 1 disc; 1 sleeve assy; 1 wheel assy; 1 shaft; 1 trigger assy; 1 lever assy; wiring harness; misc hardware; functional description:throttle, engine control
