01-184-5261
Access Aircraft Door
Used on aircraft model f-18.
01-184-6723
Structural Component Air Fitting
Ext emer canopy jtsn hdl assy
01-184-6724
Structural Component Air Fitting
Ext emer canopy jtsn hdl assy
01-184-8225
Intake Muffler
01-184-8675
Structural Component Air Support
Opp -503; nha 458-51247
01-184-8676
Structural Component Air Support
Used on acft model c/kc-135. c/o 1 fitting, 1 bushing; opposite p/n -503; nha 458-51247
01-184-8677
Structural Component Air Support
Used on acft model c/kc-135. c/o 1 aft drag fitting, 2 bushings; opposite p/n -502
01-184-8678
Structural Component Air Support
Used on acft model c/kc-135. c/o 2 overwing supports, 1 marker 4 bushings; opposite p/n -502; nha 458-51214
01-184-8679
Structural Component Air Support
Used on acft model c/kc-135. c/o 1 aft drag fitting, 2 bushings; opposite p/n -2; nha 458-51214
01-184-8680
Structural Component Air Support
C/o 1 drag fitting, 2 bushing; opp -504; nha 458-51236
01-184-8681
Structural Component Air Support
Used on acft model c/kc-135. c/o 1 drag fitting, 2 bushings; opposite p/n -504; nha 458-51247
01-184-8682
Structural Component Air Support
Used on acft model c/kc-135. c/o 1 fitting, 1 bushing; opposite p/n -504; nha 458-51247
01-184-8873
Access Aircraft Door
Used on acft model a-10a.
01-184-8990
Structural Aircraft Plate
01-184-8991
Structural Aircraft Plate
01-184-8992
Aircraft Fairing
Used on F-111.
01-184-8996
Structural Component Air Support
01-184-8998
Structural Aircraft Panel
Used on acft model f-111-a-d-e-fb.
01-184-9001
Fuselage Section
Used on aircraft model a-10a. rework of existing 160D211001-26
01-184-9119
Radome
Used on an/ale40-4. 8.300" overall length 7.540" overall width
01-184-9389
Access Aircraft Door
Used on f-14 aircraft.
01-184-9390
Access Aircraft Door
Used on f-14 aircraft.
01-184-9661
Aircraft Fairing
Used on uh-1 helicopter.... fiberglass cloth, type 7a, resin reinforcement, polyster
01-184-9662
Aircraft Fairing
01-184-9793
Structural Aircraft Plate
Used on acft model av-8. aluminum alloy; 1.630 in. lg; 0.770 in. w; 0.104 in. thk
01-184-9794
Structural Aircraft Plate
Used on acft model av-8. aluminum alloy; 1.630 in. lg; 0.770 in. w; 0.104 in. thk
01-184-9795
Structural Aircraft Plate
Used on acft model av-8. aluminum alloy; 1.630 in. lg; 0.770 in. w; 0.104 in. thk
01-184-9796
Structural Aircraft Plate
Used on acft model av-8. aluminum alloy; 1.630 in. lg; 0.770 in. w; 0.104 in. thk
01-184-9834
Thermal Insulation Pipe Covering
Used on reaction control system, av-8 harrier aircraft; 8.900 in. lg; 4.000 in. id
01-185-0641
Access Aircraft Door
01-185-0813
Airframe Aircraft Rail
Used on acft model c/kc-135. used as track assy on elevator balance panel support mechanism installation; located station 70.38; opposite p/n -24; nha 65-5650-3
01-185-0819
Structural Component Air Support
Opposite -21; nha L1800000
01-185-0829
Structural Aircraft Plate
Used on c-5b aircraft. matl-al alloy, comp 2024-T3 per qq-a-250/5; location-used on lighting strip, navigator aft circuit breaker panel; 22.670 in. lg, 1.066 in. w
01-185-0830
Structural Aircraft Plate
Used on acft model c/kc-135.
01-185-0831
Structural Aircraft Plate
Used on acft model b-1b. al clad sheet 2024-T3 per qq-a-250/5; 7.500 in. lg, 4.570 in. w, 0.050 in. thk; 4 0.257 in. dia holes in corners; nha L5416750
01-185-0832
Structural Aircraft Plate
Used on acft model c/kc-135. commercialy pure titanium sheet 70 per mil-t-9046, type i, comp. b, annealed; finish f-10.10; 5.500 in. lg, 2.000 in. w, 0.050 in. thk
01-185-0840
Structural Component Air Support
Used on f-4 aircraft. used on -30 structural assy, center section fwd, torque box; material-al aly 7075-to per qq-a-250/12; heat treated to T6, anodized
01-185-0841
Structural Component Air Support
Used on f-4 aircraft. part of-door assembly, nose landing gear forward; used on -1, -301, -79, -303; stock size-.025 x 3.20 x 16.70 in; material-alclad 7075-T6 per qq-a-250/13
01-185-0842
Structural Component Air Support
Used on acft model b-1b.
01-185-0845
Structural Component Air Support
Used on acft model c/kc-135. al alloy clad sheet 2024 per qq-A250/5; finish f-2.115; c/o 1 support, 2 brackets, 4 rivnuts; opposite p/n -1; nha 65-41778
01-185-0846
Structural Component Air Support
Used on acft model c/kc-135. c/o 2 overwing supports, 1 marker, 4 bushings; opposite p/n -502; nha 458-51201
01-185-0847
Structural Component Air Support
Used on acft model c/kc-135. c/o 1 forward drag fitting, 2 bushings; opposite p/n -504; nha 458-51234
01-185-0848
Structural Component Air Support
Used on acft model b-1b. fitting, actuator-cont attach, strl mode cont fin; opposite -002;
01-185-0849
Structural Component Air Support
Used on acft model c/kc-135. al alloy clad sheet 2024-T3 per qq-a-250/5; finish f-2.59; 13.100 in. lg, 7.400 in. w, 0.063 in. thk; c/o 1 pan, 8 nutplates; nha 458-54845
01-185-0850
Structural Component Air Support
Used on acft model c/kc-135. al alloy plate 7075-T7351 per qq-a-250/12; finish f-2.47 except bushing holes; 1.871 in. lg, 1.625 in. w, 1.440 in. h; 0.190 in. matl thk; 4 0.190 in. dia mouting holes in. base; 2 in-line 0.437 in. dia holes in clevis; c/o 1 clevis fitting, 1 bushing; opposite p/n -2; nha 458-52275
01-185-0851
Structural Component Air Support
Used on acft model c/kc-135. al alloy plate 7075-T7351 per qq-a-250/12; finish f-2.47 except bushing holes; 1.871 in. lg, 1.625 in. w, 1.440 in. h; 0.190 in. matl thk; 4 0.190 in. dia mounting holes in base; 2 in-line 0.437 in. dia holes in clevis; c/o 1 clevis fitting, 1 bushing; opposite p/n -1; nha 458-52275
01-185-0863
Aircraft Former
19.500" overall length 4.900" overall width 0.050" material thickness
01-185-0864
Aircraft Former
12.900" overall length 2.000" overall width 0.050" material thickness
01-185-0865
Aircraft Former
8.400" overall length 1.600" overall width 0.050" material thickness
