01-183-1991
Structural Aircraft Plate
Used on c-5b aircraft. matl-al alloy, comp 7075-T651 per qq-a-250/12; location-hinge, bridge rail, ramp extension assy; 2.650 in. lg, 2.250 in. w
01-183-1993
Structural Aircraft Plate
Used on f-4 aircraft. 1location-outboard flap mechanism overcenter; dimensions-1.82 l x .88 w x .650 thk; material-al aly per qq-a-288 cond T6; has 2 holes on long centerline, .44 in. centered from ea end, csink for NAS583, mate with 32-15523; holes .191 dia; nha 32-19750
01-183-1994
Structural Component Air Support
Used on c-5a aircraft. matl-al alloy, comp 6061-T6511 per qq-a-225/8; finish-chromate per mil-c-5541, cl 3
01-183-1995
Structural Component Air Support
Used on c-5b aircraft. matl-cres, 17-4ph per ams 5643; finish-paint, color white, no 17875 per fed std 595; 4.680 in. w, 2.670 in. h, irregular shape; location-tube support, nose landing gear door, BL61.70, FS584
01-183-1996
Structural Component Air Support
Used on c-5b aircraft. matl-cres, 17-4ph per ams 5643; finish-paint, color white, no 17875 to fed. std 595; location-tube support, nose landing gear door, BL61.70, FS584; 4.940 in. lg, 2.670 in. h, irregular shape
01-183-1997
Structural Component Air Support
Used on c-5b aircraft. location-hinge fitting, floor access panel, forward ramp extension; 2.720 in. lg, 2.300 in. w
01-183-2000
Structural Component Air Support
Used on f-4 aircraft. stock size-.032 x 3.80 x 30.25 in; material-titanium per mil-t-9046, type iii, comp a annealed; part of frame assy, f.s. 421.05; part of -1
01-183-2001
Structural Component Air Support
Used on f-4 aircraft. stock size-.071 x 2.60 x 8.60 in; material-alum 7075-0 per qq-a-250/13; part of -66
01-183-2002
Structural Component Air Support
Used on f-4 aircraft. for bulkhead repair, fs 303.62
01-183-2003
Structural Component Air Support
Used on f-4 aircraft. stock size-.050 x 2.30 x 8.20 in; material-al aly 7075-0 per qq-a-250/13; part of -65
01-183-2004
Structural Component Air Support
Used on f-4 aircraft. part of--1 seal assy, engine compartment; stock size-.032 x 1.10 x 6.88 in; material T1 unalloyed per mil-t-9046 type 1, comp b, annealed
01-183-2005
Structural Component Air Support
Used on f-4 aircraft. t.o.1f-4c-3-2-2s-42; part of-rib assy, m.l.g. actuator; stock size-.071 x 2.20 x 7.10 in; part of -1, -301
01-183-2006
Structural Component Air Support
Used on acft model a-10a. aluminum alloy forging per qq-a-367 7075-T73
01-183-2022
Structural Aircraft Panel
Used on c-5b aircraft. used on floor assy, flight station
01-183-2023
Structural Aircraft Panel
Used on c-5b aircraft. used on floor assy, flight station
01-183-2024
Structural Aircraft Panel
Used on c-5b aircraft. used on floor assy, flight station
01-183-2025
Structural Aircraft Panel
Used on c-5b aircraft. used on floor assy, flight station
01-183-2026
Structural Aircraft Panel
Used on c-5b aircraft. used on floor assy, flight station
01-183-2027
Structural Aircraft Panel
Used on c-5b aircraft. used on floor assy, flight station
01-183-2028
Structural Aircraft Panel
Used on F-111.
01-183-2031
Wing Landing Flap
C/o: stringers, intercostals, closeouts, ribs, spars, trailing edge assys, skin, gussets, doublers, splices, & hardware; opp -001
01-183-2032
Aircraft Former
Used on f-4 aircraft. t.o. 1f-4c-3-2s-42
01-183-2035
Aircraft Skin
Used on F-4. 37.000" overall length 31.400" overall width
01-183-2371
Aircraft Door
C/o latch mechanism, door, misc hardware
01-183-2774
Airframe Modification Kit
Used on ah-1 series helicopters.
01-183-4235
Aircraft Frame
01-183-4256
Structural Aircraft Plate
Used on c-5b aircraft. dmatl-acrylic per mil-p-5425; location-navigators forward circuit breaker panel; 16.600 in. lg, 0.750 in. w
01-183-4257
Structural Aircraft Plate
Used on c-5b aircraft. matl-acrylic per mil-p-5425; paint black, no. 37038, fed. std 595; location-navigators aft circuit breaker panel; 22.670 in. lg, 0.750 in. w
01-183-4258
Structural Aircraft Plate
Used on acft model b-1b.
01-183-4259
Structural Aircraft Plate
Used on acft model c/kc-135. aluminum alloy clad sheet 2219-T81 BMS7-110, 6.200 in. lg, 4.400 in. w, 0.063 in. thk, fin f-2.20
01-183-4260
Structural Aircraft Plate
Used on acft model c/kc-135. aluminum alloy clad sheet per qq-a-250/30 2219, ht tr T62, 8.200 in. lg, 4.300 in. w, 0.063 in. thk, fin f-2.20
01-183-4262
Aircraft Fairing
01-183-4263
Structural Component Air Support
Used on c-5a acft. matl-al alloy, comp 6061-T651 per qq-a-250/11; finish-chromate per mil-c-5541, cl 3
01-183-4264
Structural Component Air Fitting
Irregular shape
01-183-4265
Structural Component Air Support
Used on acft model c/kc-135.
01-183-4266
Structural Component Air Support
Used on acft model b-1b. al shape alloy per qq-a-200/11, 7075-T73511, shape LS043-0421, 3.51 lg; nha-L6310021 on 76-174 & subq (a/c 4 only) , nha-L6310113 on 77-0325 & subq (a/c 5 & subq) ; location-target mount-full open position indicator, weapons bay door
01-183-4268
Structural Component Air Support
Used on acft model b-1b. mfitting, amd 62 cf steel bar, alloy 9-4-20, 6.46 LGX4 thkx 5 wd; material meets class a ultrasonic quality per mil-i-8950; heat treated 9ni-4co-.20c steel per ST0111LA0002 to 190-210 ksi; nha-L8800003; eff on-74-0158 on
01-183-4269
Structural Component Air Support
Used on acft model b-1b.
01-183-4270
Structural Component Air Support
Used on acft model b-1b.
01-183-4271
Structural Component Air Support
Used on acft model b-1b. bracket, target mount-full open position indicator, weapons bay door; nha L6311023; matl 7075-T73511 al shape alloy per qq-a-200/11; shape LS043-0421, 4.57 lg
01-183-4280
Structural Aircraft Panel
Used on c-5b aircraft.
01-183-4281
Structural Aircraft Panel
01-183-4282
Structural Aircraft Panel
01-183-4289
Aircraft Former
5.500" overall length 5.500" overall width 0.063" material thickness
01-183-4290
Aircraft Former
4.800" overall length
01-183-5149
Structural Component Air Bracket
PH13-8mo per ST0160LB0005; opp -005; nha L1201050
01-183-5150
Aircraft Door
C/o skins, cores, closeout, hinge, strikers, doubler, splice, fittings; nha L3011695
01-183-5184
Structural Aircraft Plate
Used on acft model c/kc-135. aluminum alloy clad sheet per qq-a-250/30 2219-0, ht tr T62, 20.000 in. lg, 3.500 in. w, 0.071 in. thk, fin f-2.20and apply desoto hi-temperature polyurethane primer per BAC5710
01-183-5185
Structural Aircraft Plate
Used on acft model c/kc-135.
01-183-5186
Structural Aircraft Plate
Used on acft model c/kc-135. aluminum alloy clad sheet per qq-a-250/30 2219-0, 4.800 in. lg, 2.000 in. w, 0.125 in. thk, fin f-2-20
