01-201-6155
Vertical Stabilizer
Used on acft model e-2c. cognizant service:navy;
01-201-6739
Structural Aircraft Plate
01-201-6744
Structural Component Air Support
C/o support assy, fitting assy, attaching hardware
01-201-6761
Aircraft Former
Used on c-130 acft.
01-201-6762
Aircraft Former
Used on c-130 acft.
01-201-6763
Aircraft Former
Used on c-130 acft.
01-201-6764
Aircraft Former
Used on c-130 acft.
01-201-6766
Aircraft Former
Used on c-130 acft.
01-201-6767
Aircraft Former
01-201-6768
Aircraft Former
33.210" overall length 2.000" overall width 1.150" material thickness cap-center section flap beam-lower
01-201-6774
Airfoil Rib
Used on C-130.
01-201-6775
Airfoil Rib
Used on C-130.
01-201-6777
Aircraft Skin
Used on C-130. 46.000" overall length 37.000" overall width
01-201-7681
Aircraft Fairing
Nha 35-35387, 35-35519, and 35-35552
01-201-7684
Structural Component Air Support
Used on acft model b-1b. made from LB0170-195 CL13 investment casting, alloy A356; c/o 1 hinge, 2 bearings, 4 nuts; nha L5342011
01-201-7685
Structural Component Air Support
Used on acft model b-1b.
01-201-7704
Aircraft Spar
78.000" overall length 4.000" overall width 3.000" material thickness
01-201-7843
Structural Component Air Support
Used on AH-64A.
01-201-9493
Access Aircraft Door
Used on aircraft model av-8.
01-202-0431
Structural Aircraft Plate
01-202-0432
Structural Component Air Support
14.000" overall length 7.000" overall width 0.100" material thickness finish f-2.30; nha 834-7657-10
01-202-0460
Airfoil Rib
Cond 0 clad
01-202-0462
Airfoil Rib
Used on C-130. cond 0 clad
01-202-0463
Aircraft Skin
Used on C-141.
01-202-0464
Aircraft Windshield Panel
01-202-3191
Structural Aircraft Plate
Used on kc-135 aircraft. stock BAC1524-3.8 in lg, 2.2 in wd, 0.30 in thk; finish f-2.21
01-202-3193
Structural Aircraft Plate
Used on acft model kc-135.
01-202-3194
Structural Aircraft Plate
Used on acft model kc-135.
01-202-3195
Structural Aircraft Plate
Used on acft model kc-135.
01-202-3196
Structural Aircraft Plate
Used on acft model kc-135.
01-202-3198
Structural Aircraft Plate
Used on acft model kc-135. 10.0 in lg, 10.0 in wd, 0.050 in thk; 7075-T6 sheet clad per qq-a-287; finish srf-2.30; nha 65-2516
01-202-3200
Structural Aircraft Plate
Used on acft model kc-135.
01-202-3201
Structural Aircraft Plate
Used on acft model kc-135. nha 65-31682
01-202-3202
Structural Aircraft Plate
Used on acft model kc-135. nha 65-31682
01-202-3203
Structural Aircraft Plate
4.000" overall length 3.000" overall width 0.050" material thickness
01-202-3204
Structural Aircraft Plate
3.000" overall length 2.000" overall width 0.050" material thickness
01-202-3206
Structural Component Air Support
Used on kc-135 aircraft.
01-202-3207
Structural Component Air Support
Used on kc-135 aircraft. 4340 steel per mil-s-5000, forge mil-f-7190 grade a; finish srf-12.206; nha 64-1068
01-202-3208
Structural Component Air Support
Used on kc-135 aircraft. located inbd strut, lwr spar nacelle sta 139.74
01-202-3209
Structural Component Air Support
Used on kc-135 aircraft. located inbd strut, lwr spar nacelle sta 139.74
01-202-3210
Structural Component Air Support
Used on kc-135 aircraft. located inbd strut, lwr spar nacelle sta 151.43
01-202-3211
Structural Component Air Support
Used on acft model kc-135.
01-202-3212
Structural Component Air Support
Used on acft model kc-135.
01-202-3213
Structural Component Air Support
Used on kc-135 aircraft. 5.0 in lg, 3.0 in wd, 0.040 in thk; finish srf 10.15; commercially pure titanium sheet per mil-t-9046 class 6 annelaed; nha 64-1061
01-202-3215
Structural Component Air Support
6.600" overall length 3.200" overall width 0.040" material thickness f-10.15; nha 64-1061
01-202-3216
Structural Component Air Support
Used on kc-135 aircraft. 2.5 in lg, 5.0 in wd, 0.040 in thk; commercially pure titanium sheet spec per mil-t-9046 class 6, cond annealed; finish srf-10.15; nha 64-1061
01-202-3217
Structural Component Air Support
Used on acft model kc-135. 2024-0 clad per qq-a-250/5; heat treat T4; finish SRF2.115; 2.4 in. long, 3.7 in. wide, 0.040 in. thick; nha 65-2494
01-202-3218
Structural Component Air Support
Used on acft model kc-135. titanium sheet per mil-t-9046 class 6, condition annealed; finish f-10.10; 8.80 in. long, 5.50 in. wide, 0.040 in. thick; opposite p/n -4; nha 65-2494
01-202-3219
Structural Component Air Support
Used on acft model kc-135. titanium sheet per mil-t-9046 class 6, condition annealed; finish f-10.10; 8.80 in. long, 5.50 in. wide, 0.040 in. thick; opposite p/n -3; nha 65-2494
01-202-3220
Structural Component Air Support
Used on acft model kc-135. 2024-T3 clad sheet per qq-a-250/5; heat treat T4; finish srf-2.115; 4.8 in. long, 1.6 in. wide, 0.040 in. thick; opposite p/n -16; nha 65-2494
