01-156-9648
Structural Aircraft Plate
Used on acft model b52. al clad 7075-T6 per qq-a-287, 0.040 in.thk, 5.000 in.w, 5.000 in.lg, used on nose cowl, located at sta 68.90
01-156-9649
Structural Aircraft Plate
Used on acft model b52. cp titanium per ams 4901 annealed, 0.050 in.thk, 0.500 in.w, 23.800 in.lg, right hand, used on nose cowl, located at pp BL0
01-156-9651
Structural Component Air Support
Used on acft model b52. al alloy 2024-T4 per qq-a-267, stock BAC1514-293 by 14.200 in.lg, used on trailing edge fairing, outboard nacelle, wing, right hand, located at PPS286
01-156-9652
Structural Component Air Support
Used on acft model b52. al alloy 2024-T4 per qq-a-267, stock BAC1514-293 by 14.200 in.lg, used on trailing edge fairing, outboard nacelle, wing, left hand
01-156-9663
Aircraft Former
18.000" overall length 1.000" overall width 0.032" material thickness function-intercostal
01-156-9664
Aircraft Channel
10.200" overall length 1.500" overall width 0.040" material thickness matl: clad al aly; temp T3; fin: f-2.115; dimensions listed are stock size
01-156-9665
Structural Component Air Bracket
Manufacturer suggested name: bracket assembly; c/o: channel (-5:clad 2024-0)
01-156-9792
Access Aircraft Door
Used on aircraft model f-18.
01-157-0024
Aircraft Frame
01-157-0085
Structural Component Air Support
01-157-0086
Structural Component Air Bracket
01-157-0087
Aircraft Channel
01-157-0088
Aircraft Former
01-157-0089
Aircraft Channel
01-157-0092
Structural Component Air Bracket
01-157-0093
Structural Component Air Bracket
01-157-0094
Structural Component Air Bracket
01-157-0095
Structural Component Air Bracket
2.500" overall length 2.200" overall width
01-157-0096
Structural Component Air Bracket
01-157-0097
Structural Component Air Bracket
2.800" overall length 2.100" overall width
01-157-0099
Structural Aircraft Plate
01-157-0113
Structural Component Air Support
3.550" overall length 2.880" overall width next higher assy, 68A321000, u/o f-15c cum 270
01-157-0122
Structural Aircraft Plate
48.000" overall length 18.000" overall width 0.100" material thickness used on pn 16B5113-806
01-157-0123
Structural Aircraft Plate
4.000" overall length 3.300" overall width 0.050" material thickness used as doubler
01-157-0124
Structural Aircraft Plate
4.100" overall length 3.200" overall width 0.050" material thickness used as doubler
01-157-0125
Structural Aircraft Plate
Used on B-52. used as web assembly, fwd
01-157-0126
Structural Aircraft Plate
Used on B-52. used as web assembly, aft; opposiite pn 39-9919-509
01-157-0127
Structural Aircraft Plate
6.100" overall length 5.700" overall width 0.050" material thickness 0 temper; heat treat T4; finish f-2.115
01-157-0128
Structural Aircraft Plate
3.800" overall length 3.000" overall width 0.040" material thickness 0 temper; heat treat T4; finish f-2.130
01-157-0129
Structural Aircraft Plate
7.500" overall length 7.200" overall width 0.040" material thickness 0 temper; heat treat T4; finish f-2.115
01-157-0130
Structural Aircraft Plate
Used on B-52.
01-157-0131
Structural Aircraft Plate
Used on acft model b52. commercially pure titanium per ams 4901 annealed, 0.063 in.thk, 3.500 in.w, 3.900 in.lg, used on nose cowl
01-157-0139
Structural Component Air Support
Used as bracket
01-157-0140
Structural Component Air Support
3.800" overall length 2.500" overall width 0.050" material thickness used as tube support on nose cowl anti-icing (kit) ; matl aisi 17-7ph, surface cond 2d
01-157-0141
Structural Component Air Support
01-157-0147
Aircraft Former
0.040" material thickness 17-7ph annealed ht treated 180-200, 000 psi
01-157-0153
Aircraft Former
Used on B-52. used as channel
01-157-0154
Aircraft Former
Used on b52 strato fortess.
01-157-0158
Aircraft Former
18.000" overall length 1.000" overall width 0.032" material thickness
01-157-0159
Aircraft Former
18.000" overall length 1.000" overall width 0.032" material thickness
01-157-0160
Aircraft Former
19.000" overall length 1.000" overall width 0.032" material thickness
01-157-0161
Aircraft Former
19.000" overall length 1.000" overall width 0.032" material thickness
01-157-0162
Aircraft Former
46.000" overall length 2.000" overall width 0.050" material thickness outer
01-157-0163
Aircraft Former
18.000" overall length 1.000" overall width 0.032" material thickness
01-157-0164
Aircraft Former
18.000" overall length 1.000" overall width 0.032" material thickness
01-157-0165
Aircraft Former
18.000" overall length 1.000" overall width 0.032" material thickness
01-157-0166
Aircraft Former
Used on F-15.
01-157-0169
Aircraft Skin
Used on B-52. components skin-1
01-157-1574
Structural Aircraft Plate
Used on acft model b52. al clad 2024-T3 per qq-a-362, 0.050 in.thk, 0.500 in.w, 17.200 in.lg, used on nose cowl
01-157-1575
Structural Aircraft Plate
Used on acft model b52. cp titanium per ams 4901 annealed, 0.015 in.thk, 29.400 in.w, 30.200 in.lg, used on nose cowl
