01-212-3444
Aircraft Stringer
Used on refueling/ tanker aircraft.
01-212-4038
Structural Aircraft Plate
Used on c-5 aircraft. crew compt, floor, fs 524.00 to 624.00; matl 2024-T3 alclad per qq-a-250/5; size 0.016X6.0X20.0in
01-212-4039
Structural Aircraft Plate
Used on c-5 aircraft. c/o: bracket (2) , fwd panel (1) ; part of -102d door assembly-slat actuator track 5a; opposite -109c
01-212-4040
Aircraft Fairing
C/o -120b cover; -126a fairing assembly; opposite -129b
01-212-4041
Structural Component Air Support
Used on acft model f-111. aluminum alloy per 356-T6 ams 4260
01-212-4045
Structural Aircraft Panel
Used on c-5a aircraft. trim panel assembly-floating ceiling, flight sta; c/o: -105b panel assembly (1) , -117a panel assembly (2) , -123a door assembly (1) , spacer (23) , hinge assembly (1) , sleeve (30) , retainer (1) , stud (1) , receptacle (1) , nut (1) ; part of -101a trim panel instl
01-212-4073
Aircraft Former
01-212-4074
Longeron
Used on T-37. opposite -3
01-212-4075
Aircraft Pylon
Alt fuel pylon
01-212-4077
Aircraft Skin
01-212-4909
Structural Component Air Support
01-212-4910
Structural Component Air Support
01-212-4911
Structural Component Air Support
01-212-6214
Aircraft Skin
Skin section, similar to part number 216-40454-1; end item TA7c aircraft; material al alloy 7075-0, clad one side; 0.190 in. thick; 9.600 in. wide; 16.100 in. long
01-212-6215
Aircraft Skin
Skin section, similar to part number 218-40003-41; end item TA7c aircraft material al alloy 7075-0 clad one side 0.080 in. thick
01-212-6216
Aircraft Skin
Skin section similar to part number 218-40033-43; end item TA7c aircraft; material al alloy qq-a-250/18; 0.080 in. thick; 29.000 in. wide; 75.700 in. long
01-212-8780
Aircraft Ramp Assembly
Aft ramp assembly complete
01-212-8945
Structural Aircraft Plate
Used on acft model av-8b. matl, copper alloy, mil-s-22499 cl 2, ty ii, surf, anodize per PS13201, ty ii, cl 1; rectangular wth one side cut to tri angular shape, lgth 1.760 in, 1st wdth from angle point 1.560 in., 2nd wth 1.080 in., thk 0.094 in., thre holes 0.190 in. dia. located in thre corners, c to c 1.000 lgth; c to c 0.750 in. along wth
01-212-8946
Structural Aircraft Plate
Used on acft model av-8. spacer plate, rect shape, one aperture located c to end edge 0.250 in., alum 7075 per qq-a-250/24 cond t 76; lg 1.270 in., wth 0.640 in.; cross section, convex; thk 0.125 at center to 0.030 at edge; aperture dia 0.255 in.
01-212-8947
Structural Aircraft Plate
01-212-8949
Structural Component Air Support
Used on t-38 aircraft. located nose ldg gear, sta 126.10; c/o: lub fitting (1) , bearing (1) , machined fitting (1)
01-212-8950
Structural Component Air Support
Used on acft model fb-111a. aluminum alloy per 2024-T851 fms-1010, 3.000 in. lg, 4.000 in. w, 1.500 in. thk
01-212-8951
Structural Component Air Support
Used on acft model fb-111a. aluminum alloy per 2024-T851 fms-1010, 3.000 in. lg, 4.000 in. w, 1.500 in. thk
01-212-8952
Structural Component Air Support
Used on acft model fb-111-a. aluminum alloy per 2024-T851 FMS1010, 3.000 in. lg, 6.000 in. w, 2.000 in. thk
01-212-8953
Structural Component Air Support
Used on acft model fb-111-a. aluminum alloy per 2024-T851 FMS1010, 3.000 in. lg, 6.000 in. w, 2.000 in. thk
01-212-8955
Structural Component Air Fitting
3.760" overall length
01-212-8956
Structural Component Air Support
Used on c-130 aircraft. matl size LS5095-2X27; opposite -1; stiffener-flap track rib, rear beam, o.w. sta 18.00; nha 3325534
01-212-8960
Bleed Air Duct Assembly
Used on acft model f-111. c/o 49 components
01-212-8996
Aircraft Former
31.000" overall length 2.000" overall width 0.020" material thickness matl sheet hastelloy x per AMS5536; part of former installation
01-212-8997
Aircraft Former
18.300" overall length 14.300" overall width 0.020" material thickness
01-212-9350
Structural Component Air Support
60.000" overall length 2.850" overall width 1.820" material thickness repair member
01-212-9360
Structural Component Air Support
Used on f-15 aircraft. size 3.00X9.50X22.00; matl 7075-T7351 per mms-159, cond T7351; opposite -2017
01-212-9361
Structural Component Air Support
Used on f-15 aircraft. size 3.00X9.50X22.00; matl 7075-T7351 per mms-159, cond T7351; opposite -2018
01-212-9745
Access Aircraft Cover
Used on t-37b aircraft. door-c/o: -2 skin (1) , -3 pan (1) , -4 doubler (1) ; part of -9 door assembly, tunnel center
01-212-9856
Aircraft Skin
Used on T-38. 58.000" overall length 14.000" overall width part of -5 skin bottom; T1-6al-4v; this item has been determined to be a critical application item. in-flight failure of this item would create a hazardous condition
01-213-1102
Structural Aircraft Plate
01-213-1107
Structural Component Air Support
Used on c-5 aircraft. part of -101a fitting assembly-hinge, slot door, mlg fairing; opposite -104a
01-213-1109
Structural Component Air Support
Used on acft model c-130. ls 5197 by 82; opposite p/n -l; nha 352763
01-213-1110
Structural Component Air Support
01-213-1121
Aircraft Skin
Used on f-4 aircraft. skin-bottom, outer wing repair; left hand; material-al aly sht 7075-T6 per qq-a-250/12 (alternate-al aly 7178-T76 per qq-a-250/21) ; max l-74.90, max h-39.06
01-213-1124
Aircraft Skin
Used on f-4 aircraft. skin, top-outer wing repair; material-al aly sht 7075-T6 per qq-a-250/12 (alternate-al aly sht 7178-T76 per qq-a-250/21) ; max w-74.90, max h-39.06; right hand
01-213-1910
Access Aircraft Door
01-213-1911
Access Aircraft Door
01-213-1912
Access Aircraft Door
01-213-2201
Aircraft Fairing
Used on e-2 aircraft.
01-213-2202
Aircraft Elevator
Used on aircraft model c2-a.
01-213-2203
Aircraft Elevator
Used on aircraft model c-2a.
01-213-2231
Aircraft Tip
47.000 in. o/a l; 14.000 in. o/a w; 6.000 in. o/a h
01-213-2548
Structural Aircraft Panel
Used on c-2a aircraft.
