01-295-9600
Aircraft Former
21.000" overall length 18.000" overall width 2.250" material thickness former-nacelle; nha 6-11450; eff 63-8450 & subq
01-295-9768
Structural Aircraft Plate
Torque tube bearing; T3
01-295-9769
Structural Component Air Support
Used on f-16a aircraft.
01-295-9770
Aircraft Channel
P/o: door, mlg, outer
01-295-9776
Aircraft Skin
Used on F-16. part of skin instl, upper-outbd
01-295-9777
Aircraft Skin
Used on F-16. 26.000" overall length 22.000" overall width matl fms 3002-T851; nha 16B415-1
01-296-0659
Access Aircraft Door
Used on aircraft model f-18.
01-296-0660
Access Aircraft Door
Used on target drone bqm-34s.
01-296-0747
Structural Aircraft Plate
Used on aircraft model s-3.
01-296-0748
Structural Aircraft Plate
Used on aircraft model s-3.
01-296-0756
Movable Canopy
Used on aircraft model f-14.
01-296-0758
Aircraft Skin
Used on aircraft model s-3.
01-296-0759
Aircraft Skin
Used on aircraft model s-3.
01-296-0760
Aircraft Skin
Used on aircraft model s-3.
01-296-0761
Aircraft Skin
Used on aircraft model s-3.
01-296-0762
Aircraft Skin
Used on s-3 acft. 57.100 in. l; 15.300 in. w; 0.020 in. thk; aluminum alloy qq-a-250/5
01-296-0763
Aircraft Skin
Used on s-3 acft. aluminum alloy qq-a-250/5; 57.100 in. l; 15.300 in. w; 0.020 in. thk
01-296-0764
Aircraft Skin
Used on s-3 acft. aluminum alloy qq-a-250/5; 57.100 in. l; 10.700 in. w; 0.025 in. thk
01-296-0765
Aircraft Skin
Used on s-3 acft. 57.100 in. l; 10.700 in. w; 0.025 in. thk; aluminum alloy qq-a-250/5 material
01-296-0766
Aircraft Skin
Used on aircraft model s-3.
01-296-0767
Aircraft Skin
Used on aircraft model s-3.
01-296-0769
Aircraft Tip
Used on aircraft model s3.
01-296-0770
Aircraft Tip
Used on aircraft model s3.
01-296-0773
Aircraft Windshield Panel
Used on fighter aircraft f-14.
01-296-0774
Aircraft Windshield Panel
01-296-0881
Fluid Aircraft Manifold
5.292" overall length 4.908" overall width
01-296-1386
Structural Component Air Support
Used on c-141 acft. al alloy 7075-T6511; cap-center wing, front beam upper, outboard seg
01-296-1390
Structural Component Air Support
Bracket-support; matl:al aly t-3 clad
01-296-1391
Structural Component Air Support
Temper T3
01-296-1408
Aircraft Spar
52.000" overall length 8.000" overall width 0.032" material thickness
01-296-2476
Structural Aircraft Plate
9.000" overall length 2.000" overall width 0.125" material thickness NHA3W11000
01-296-2477
Structural Aircraft Plate
10.000" overall length 2.000" overall width 0.312" material thickness NHA3W11008; ctr wing
01-296-2478
Structural Aircraft Plate
10.000" overall length 2.000" overall width 0.312" material thickness ctr wing; nha 3W11008
01-296-2479
Aircraft Fairing
01-296-2481
Structural Component Air Support
Used on acft model c-141a/c. LS30057-1 by 38.0 in; heat treat lac 0521; finish f-19-24 type iii aluminized; nha 3W11001
01-296-2482
Structural Component Air Support
Used on acft model f-15. 7075-T7351 per qq-a-225/9 cond T7351; 10.65 in lg, 5.00 in wd, 3.00 in thk; nha 68A310012
01-296-2483
Structural Component Air Support
Used on acft model f-15. 7075-T7351 rolled per qq-a-225/9, cond T7351; 12.00 in lg, 5.00 in wd, 3.00 in thk; nha 68A310002
01-296-2484
Structural Component Air Support
Used on acft model c-141a/c. LS30056-1 by 38.0 in; heat treat LAC0521; finish f-19.24 type ii aluminized; nha 3W11002
01-296-2490
Structural Aircraft Panel
Used on acft model b-1b. consist of 1 panel, 2 angle, 1 clevis; located XFP595.056 to XFP604.656
01-296-2500
Aircraft Skin
Used on C-141. make from 3W22178-103; nha 3W00011
01-296-2506
Aircraft Spar
L53389 by 3.0 in
01-296-3270
Aircraft Former
0.880" overall length 0.680" overall width 0.063" material thickness nha -1003
01-296-3271
Airfoil Rib
14.000" overall length 5.000" overall width 2.000" material thickness nha 68A118002
01-296-3272
Airfoil Rib
14.000" overall length 5.000" overall width 2.000" material thickness nha 68A118002
01-296-3273
Airfoil Rib
14.000" overall length 5.000" overall width 2.000" material thickness nha 68A118002
01-296-3274
Airfoil Rib
14.000" overall length 5.000" overall width 2.000" material thickness nha 68A118002
01-296-3275
Airfoil Rib
14.000" overall length 5.000" overall width 2.000" material thickness nha 68A118002
01-296-3276
Airfoil Rib
14.000" overall length 5.000" overall width 2.000" material thickness nha 68A118002
01-296-3405
Aircraft Frame
