01-108-4053
Aircraft Fairing
30.500" overall length 24.000" overall width 0.080" material thickness finish srf-2.30
01-108-4054
Aircraft Fairing
30.500" overall length 24.000" overall width 0.080" material thickness finish srf-2.30
01-108-4055
Aircraft Fairing
30.500" overall length 24.000" overall width 0.080" material thickness finish srf-2.30
01-108-4685
Access Aircraft Door
Used on A-10. c/o 1 skin, 1 ramp, 1 former, attaching hardware
01-108-8635
Access Aircraft Door
Used on e-3a aircraft. nuclear hardness critical item; p/o: antenna pedestal
01-108-8636
Access Aircraft Door
Used on acft e3a. featgnuclear hardness critical item; p/o: antenna pedestal
01-108-8687
Structural Component Air Fitting
01-108-8723
Aircraft Rudder
01-108-8724
Aircraft Rudder
01-108-8736
Aircraft Former
Used on F-111. 38.000" overall length 2.000" overall width 0.071" material thickness
01-108-9662
Structural Component Air Support
01-108-9759
Structural Aircraft Panel
Used on A-10.
01-108-9760
Structural Aircraft Panel
Used on A-10.
01-108-9761
Structural Aircraft Panel
Used on a-10 aircraft.
01-108-9763
Structural Aircraft Plate
01-109-0762
Access Aircraft Door
Anodize surface treated
01-109-1565
Structural Aircraft Plate
17.000" overall length 8.000" overall width 0.071" material thickness
01-109-1566
Structural Aircraft Plate
17.000" overall length 8.000" overall width 0.071" material thickness
01-109-1567
Structural Aircraft Plate
19.000" overall length 8.000" overall width 0.071" material thickness
01-109-1569
Structural Aircraft Plate
50.000" overall length 3.000" overall width 0.100" material thickness
01-109-1576
Aircraft Skin
Used on F-111. 97.000" overall length 28.000" overall width
01-109-1577
Aircraft Skin
Used on F-111. 97.000" overall length 28.000" overall width
01-109-2375
Aircraft Beam
Strake fuel tank beam
01-109-3275
Structural Aircraft Plate
7.000" overall length 6.000" overall width 0.100" material thickness
01-109-3276
Structural Component Air Support
Used on acft model f111. steel casting per ams 5355
01-109-5580
Structural Aircraft Plate
Used on 1560-01-056-8385. aluminum alloy 356 T6 ams 4260, ANOD1zed mil-c-5541 class 1a, 1.000 in. o/a w, 2.156 in. o/a lg, 2 mtg holes 0.312 in. dia
01-109-6205
Aircraft Channel
Vertical tail; finish f-6.10; fabricate & inspect per BACD61099
01-109-6206
Structural Aircraft Plate
8.800" overall length 8.400" overall width 0.080" material thickness finish f-2.30; T6 temper
01-109-6242
Structural Aircraft Plate
01-109-6243
Structural Aircraft Plate
Finish f-6.10
01-109-6244
Aircraft Fairing
01-109-6245
Aircraft Fairing
01-109-6959
Aircraft Pylon
01-109-7711
Elevator Balance Weight
Used on a-37b acft. bronze; 32.400 in lg; located buttlock line 39.13 to 72.14
01-109-7739
Access Aircraft Door
Rh equipment bay
01-109-7772
Airfoil Rib
3.940" overall length
01-109-7773
Airfoil Rib
4.200" overall length 2.800" overall width 0.020" material thickness
01-109-7774
Airfoil Rib
8.520" overall length
01-109-7776
Airfoil Rib
13.590" overall length opposite pn 4034520-3; four holes, 0.218 in. dia.
01-109-7781
Airfoil Rib
5.360" overall length 0.128 in. dia.
01-109-7782
Thermal Special Purpo Insulation
End item identification:aircraft, model F4g
01-109-7783
Thermal Special Purpo Insulation
End item identification:aircraft, model F4g
01-109-8607
Aircraft Pylon
C/o apron assy, hydraulic system, drain system, cable pulley pylon support, panel assy, pylon structure assy, overheat
01-109-8608
Aircraft Pylon
Used on c-5 acft. c/o panel assy, 3; frame assy, 2; cable assy; miscellaneous hardware; used outboard;
