01-149-8788
Aircraft Former
49.000" overall length 3.200" overall width 0.045" material thickness
01-149-8789
Aircraft Former
Used on B-52. opposite p/n 25-2308-807
01-149-8790
Structural Component Air Bracket
01-149-8791
Aircraft Former
Used on B-52. opposite p/n 25-2308-811
01-149-8792
Aircraft Former
3.300" overall length 2.500" overall width 0.040" material thickness
01-149-8793
Aircraft Former
2.700" overall length 2.700" overall width 0.040" material thickness
01-149-8794
Aircraft Former
Used on B-52.
01-149-8797
Aircraft Former
6.600" overall length 1.500" overall width 0.032" material thickness temper to T0, heat treat to T4; agle; finish f-2.115
01-149-8798
Aircraft Former
Used on B-52. opposite pn 25-2308-815
01-149-8799
Aircraft Former
Used on B-52.
01-149-8800
Aircraft Former
Used on B-52. stock size alter bac 1512-432 by 2.700 in. lg
01-149-8801
Aircraft Former
Used on B-52. stock size alter bac 1512-432 by 2.700 in. long
01-149-8802
Aircraft Former
2.400" overall length 1.400" overall width 0.050" material thickness
01-149-8804
Aircraft Former
6.300" overall length 2.900" overall width 0.050" material thickness
01-149-8807
Aircraft Former
19.500" overall length 1.700" overall width 0.050" material thickness
01-149-8816
Access Aircraft Door
Fwd fuselage lh access
01-149-8817
Access Aircraft Door
Fwd fuselage lh access
01-149-8897
Radome
Used on f-5 acft.
01-149-9885
Access Aircraft Door
01-149-9886
Access Aircraft Door
01-150-0002
Aircraft Frame
34.000" overall length 2.000" overall width 0.040" material thickness used on -516, -522
01-150-0003
Structural Component Air Bracket
Used on -516, -522, & -545 firewall instl
01-150-0006
Wing Landing Flap
01-150-0044
Structural Aircraft Plate
Used on acft model c/kc-135. al clad sheet 2024-T3 per qq-a-250/5; finish f-2.59; 2.800 in. lg, 1.100 in. w, 0.040 in. thk; opposite p/n -14
01-150-0045
Structural Aircraft Plate
Used on acft model c/kc-135. al clad sheet 2024-T3 per qq-a-250/5; finish f-2.59; 2.800 in. lg, 1.100 in. w, 0.040 in. thk; opposite p/n -13
01-150-0046
Structural Aircraft Plate
Used on acft model c/kc-135. al clad sheet 2024-T3 per qq-a-250/5; finish f-2.59; 2.800 in. lg, 2.500 in. w, 0.050 in. thk; opposite p/n -4
01-150-0047
Structural Aircraft Plate
Used on acft model c/kc-135. al clad sheet 2024-T3 per qq-a-250/5; finish f-2.59; 2.800 in. lg, 2.500 in. w, 0.050 in. thk; opposite p/n -3
01-150-0049
Structural Aircraft Plate
Used on acft model b52. al clad 2024-0 per qq-a-250/5, 0.071 in.thk, 9.400 in.w, 16.100 in.lg, left hand, located at sta 271.65
01-150-0051
Aircraft Fairing
01-150-0052
Aircraft Fairing
01-150-0055
Structural Component Air Support
C/o: bracket (1 ea) 39-3908-3, nutplate (1 ea) MK1000-3; used on fire detector harn closure rib
01-150-0056
Structural Component Air Support
Bracket 1, 36-3902-1; do not use cadmium plated tools on this item, nutplate 1, p/n MK2000-3
01-150-0068
Aircraft Former
43.500" overall length 2.500" overall width 0.025" material thickness finish f-2.115; stiffener
01-150-0069
Aircraft Former
10.200" overall length 3.100" overall width 0.090" material thickness
01-150-0070
Aircraft Former
10.200" overall length 3.100" overall width 0.090" material thickness
01-150-0606
Structural Aircraft Plate
Used on acft model b52. steel per mil-s-5059
01-150-0607
Structural Aircraft Plate
11.500" overall length 3.000" overall width 0.036" material thickness steel aisi 17-7ph
01-150-0608
Structural Aircraft Plate
11.500" overall length 3.000" overall width 0.036" material thickness steel aisi 17-7ph
01-150-0609
Structural Aircraft Plate
14.000" overall length 3.000" overall width 0.036" material thickness steel aisi 17-7ph
01-150-0612
Structural Component Air Support
01-150-0613
Structural Component Air Support
5.000" overall length 2.300" overall width 0.050" material thickness gcp; class 6; do not use cadmium plated tools on this item
01-150-0614
Structural Component Air Support
5.000" overall length 2.300" overall width 0.050" material thickness gcp; class 6; do not use cadmium plted tools on this item
01-150-0615
Structural Component Air Support
9.300" overall length 3.100" overall width 0.050" material thickness gcp; do not use cadmium plated tools on this item; class 6
01-150-0616
Structural Component Air Support
9.300" overall length 3.100" overall width 0.050" material thickness class 6; do not use cadmium platedtools on this item
01-150-0617
Structural Component Air Support
8.800" overall length 1.300" overall width 0.063" material thickness bracket 1 ea p/n 36-3930-1, nutplate 2 ea p/n MK1000-3
01-150-0618
Structural Component Air Support
3.900" overall length 1.000" overall width 0.063" material thickness
01-150-0619
Structural Component Air Support
C/o washer 1 ea p/n 36-3993-1, o-ring 2 ea p/n AN6227-11
01-150-0620
Structural Component Air Support
Support 1 ea p/n 39-16034-501, nut plate 2 ea p/n NAS696A3
01-150-0621
Structural Component Air Support
5.200" overall length 3.600" overall width 0.032" material thickness annealed
01-150-0622
Structural Component Air Support
Angle 1 ea p/n 39-5612-1, nutplate 2 ea p/n MK2000-1032