01-222-7629
Structural Component Air Support
Type/model designation:f-4e/gy/ nickel chromium alloy mil-n-7786, matl 0.050 in. thk by 7.000 in. w by 3.047 in. lg
01-222-7630
Structural Component Air Support
Type/model designation:f-4e/gy/ nickel chromium alloy mil-n-7786; matl 0.050 in. thk by 7.000 in. w by 3.062 in. lg
01-222-7631
Structural Component Air Support
Type/model designation:f-4e/gy/ nickel chromium alloy mil-n-7786, matl 0.050 in. thk by 7.000 in. w by 3.062 in. lg
01-222-7632
Structural Component Air Support
Type/model designation:GRMK5 comp qty 3; support p/n 75A6136032005 alloy steel uns J22090 mil-a-21180 class 10 T61; 2 inserts p/n MS21209F5-10
01-222-7633
Structural Component Air Support
Type/model designation:f-4e/gy/ nickel chromium alloy mil-n-7786, matl 0.040 in. thk by 2.391 in. w by 18.797 in. lg
01-222-7634
Structural Component Air Support
Used on aircraft model av8b. radius 1.290 in min
01-222-7778
Bell Crank
0.257" bore diameter
01-222-8351
Structural Component Air Support
Used on h46 acft. 16.48 in. lg; 13.85 in. w; 1.86 in. h min
01-222-8352
Structural Component Air Support
01-222-8353
Structural Component Air Support
01-222-8354
Structural Component Air Support
Used on ch46 acft. 6.70 in. lg; 2.00 in. w; -3 forged
01-222-8355
Structural Component Air Support
01-222-9264
Structural Aircraft Plate
01-222-9265
Structural Aircraft Plate
01-222-9266
Structural Aircraft Plate
01-222-9267
Structural Aircraft Plate
01-222-9268
Structural Aircraft Plate
01-222-9271
Structural Aircraft Panel
01-222-9519
Structural Aircraft Plate
1.380" overall length 0.620" overall width 0.063" material thickness
01-222-9520
Structural Aircraft Plate
5.700" overall length 4.500" overall width 0.050" material thickness
01-222-9523
Structural Component Air Support
Used on c-5b aircraft. mlg fairing, fus sta 1303.19 & fus sta 1603.13; matl 7075-01 al alloy per qq-a-367; size 7.0X9.0X13.0; opposite -104a
01-222-9524
Structural Component Air Support
Used on c-5b aircraft. mlg fairing, fus sta 1303.19 & fus sta 1603.13; matl 7075-01 al alloy per qq-a-367; size 7.0X9.0X13.0; opposite -103a
01-222-9525
Structural Component Air Support
Used on acft model f-4c,d,e. 7075-T6 al aly plate per qq-a-250/12; opposite p/n -01; nha 7127390-10
01-222-9526
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 type 3 composition c anl, 12.100 in. lg, 2.500 in. w, 0.063 in. thk
01-222-9527
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 type 3 composition c anl, 15.450 in. lg, 1.150 in. w, 0.036 in. thk
01-222-9528
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 type 3 composition c anl, 19.000 in. lg, 3.800 in. w, 0.050 in. w
01-222-9529
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 type 3 composition c anl, 19.300 in. lg, 3.600 in. w, 0.050 in. thk
01-222-9530
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 type 3 composition c anl, 19.300 in. lg, 3.600 in. w, 0.050 in. thk
01-222-9531
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 type 3 composition c anl, 7.500 in. lg, 3.400 in. w, 0.050 in. thk
01-222-9532
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 type 3 composition c anl, 12.100 in. lg, 2.500 in. w, 0.063 in. thk
01-222-9533
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 type 3 composition c anl, 10.500 in. lg, 2.900 in. w, 0.016 in. thk
01-222-9534
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition c anl, 26.800 in. lg, 1.900 in. w, 0.036 in. thk
01-222-9535
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition c anl, 25.500 in. lg, 1.900 in. w, 0.036 in. thk
01-222-9536
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition c anl, 15.950 in. lg, 1.150 in. w, 0.036 in. thk
01-222-9537
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition c anl, 15.450 in. lg, 1.150 in. w, 0.036 in. thk
01-222-9538
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition c anl, 15.450 in. lg, 1.150 in. w, 0.036 in. thk
01-222-9539
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition c anl, 6.800 in. lg, 1.800 in. w, 0.036 in. thk
01-222-9540
Structural Component Air Support
Used on f-15 acft. titanium per mil-t-9046 type 3 composition c anl, 6.500 in. lg, 3.700 in. w, 0.050 in. thk
01-222-9543
Structural Aircraft Panel
Used on acft model e-3a. c/o 1 panel, 2 rubber supports, dacron cloth, velcro tape, rigid vinyl, 3 inserts, 1 bronze staple
01-222-9545
Structural Aircraft Panel
Used on acft model e-3a. c/o 1 panel, 3 rubber supports, 1 gap filler, dacron cloth, velcro tape, 4 bollards, rigid vinyl, 2 insert, 1 bronze staples
01-222-9546
Structural Aircraft Panel
Used on acft model e-3a. c/o 1 panel, 3 rubber supports, 1 gap cover, dacron cloth, velcro tape, rigid vinyl, 1 bronze staple
01-222-9547
Structural Aircraft Panel
Used on acft model e-3a. c/o 1 panel, 3 rubber supports, dacron cloth, velcro tape, 2 stiffeners, 3 bollard, rigid vinyl, 24 inserts, 1 bronze staple
01-222-9548
Structural Aircraft Panel
Used on acft model e-3a. c/o 1 panel, 1 spacer, 1 rubber seal, dacron cloth, 2 spacer, rigid vinyl, 3 spacer insert, 1 bronze staple
01-222-9549
Aircraft Former
9.300" overall length 8.800" overall width 0.045" material thickness
01-222-9550
Aircraft Former
25.700" overall length 8.000" overall width 0.063" material thickness
01-222-9551
Aircraft Former
25.300" overall length 9.200" overall width 0.071" material thickness material per mms 1203 6al-6v-2sn
01-222-9552
Aircraft Former
9.000" overall length 9.000" overall width 0.050" material thickness
01-222-9553
Aircraft Skin
Used on f-5 aircraft.
01-222-9556
Aircraft Door
Used on F-15.
01-223-0633
Structural Component Air Support
