01-213-3863
Aircraft Fairing
Used on aircraft model av-8.
01-213-3864
Aircraft Fairing
Used on aircraft model av-8.
01-213-3866
Structural Component Air Support
Used on t-38 aircraft. 7075-T73 aluminum alloy forging attaches to aft fuselage section
01-213-3867
Structural Component Air Support
Used on t-38 aircraft. 7075-T6 aluminum alloy; fitting for attaching nose landing gear drag brace
01-213-3871
Wing Landing Flap
01-213-3872
Wing Landing Flap
01-213-3873
Wing Landing Flap
01-213-3880
Aircraft Skin
Skin section, similar to part number 218-40033-39; end item TA7c aircraft; material al alloy 7075-0, clad one side; 0.080 in. thk; 29.0 in. wide; 84.0 in. long
01-213-3881
Aircraft Skin
Used on aircraft model av-8. aluminum alloy
01-213-3882
Aircraft Windshield Panel
01-213-3883
Aircraft Windshield Panel
01-213-4535
Structural Component Air Support
Used on c-141a/b aircraft. emer exit, fus sta 566.44; matl 7075-T6 bare per qq-a-283, temper-T6; matl size .190X3.0X4.0; opposite -104; nha 3F10241
01-213-4950
Structural Component Air Support
1.100" overall length 0.800" overall width 0.250" material thickness
01-213-4951
Structural Component Air Support
1.500" overall length
01-213-5593
Structural Component Air Support
3.250" overall length 2.190" overall width
01-213-5594
Structural Component Air Support
3.250" overall length 2.190" overall width
01-213-6444
Access Aircraft Door
Used on acft model f-111.
01-213-7783
Structural Component Air Support
01-213-7784
Structural Component Air Support
4.320" overall length 3.440" overall width 0.125" material thickness
01-213-8435
Access Aircraft Cover
Used on f-16c/d usaf aircraft. engine bay access, fs 410.06; c/o- -7 door .100 x 10.1 x 10.6, grommet (10) ; eff on 5c 0178, 0180, 0182, 0188, 0190, 0192, 0194, 0204, 0206, 0208, 0212, 0214, 0216, 0218, 0220; nha-16B6591-1
01-213-8612
Structural Aircraft Plate
01-213-8613
Structural Aircraft Plate
Xtitanium alloy ams 4911, alloy R56400; l-shaped strip; width 1.460 in. min
01-213-8619
Structural Component Air Support
0.063" material thickness
01-213-8621
Structural Component Air Support
0.105" material thickness
01-213-8622
Structural Component Air Support
01-213-8623
Structural Component Air Support
01-213-8625
Structural Component Air Support
01-213-8626
Structural Component Air Support
0.063" material thickness
01-213-8627
Structural Component Air Support
0.063" material thickness
01-213-8628
Structural Component Air Support
0.063" material thickness
01-213-8629
Structural Component Air Support
01-213-8977
Structural Component Air Support
01-213-8978
Structural Component Air Support
0.063" material thickness
01-213-9091
Access Aircraft Door
Used on F-16. lh lower strake access
01-213-9211
Access Aircraft Door
Used on acft model a-10a.
01-213-9235
Structural Aircraft Plate
53.000" overall length 15.000" overall width 0.875" material thickness
01-213-9236
Structural Component Air Support
01-213-9406
Aircraft Windshield Panel
01-213-9407
Aircraft Windshield Panel
01-213-9408
Aircraft Windshield Panel
01-213-9409
Aircraft Windshield Panel
01-213-9410
Aircraft Windshield Panel
01-213-9411
Aircraft Windshield Panel
01-214-0013
Access Aircraft Door
Torpedo, door assembly peripheral shape style - rectangle, no holes; width - 110.00" ; length - 93.00" ; securing device type - elbow catch
01-214-0192
Horizontal Stabilizer
01-214-1305
Structural Component Air Support
Used on eh-60a,uh-60a aircrafts.
01-214-2448
Structural Component Air Support
01-214-2452
Wing Landing Flap
