01-148-2056
Structural Aircraft Plate
Function-web weldment assembly
01-148-2057
Structural Aircraft Plate
Function-web assembly
01-148-2058
Structural Aircraft Plate
Function-web assembly
01-148-2059
Structural Aircraft Plate
1.500" overall length 0.700" overall width 0.056" material thickness aisi 301, 1/2 hard, surface condition 2b; finfish f-8.05
01-148-2060
Structural Aircraft Plate
18.000" overall length 6.000" overall width 0.050" material thickness
01-148-2061
Structural Aircraft Plate
21.000" overall length 12.000" overall width 0.040" material thickness 6A1-4v annealed per bms 7-39; finish f-10.10
01-148-2062
Structural Aircraft Plate
20.000" overall length 8.000" overall width 0.020" material thickness 6A1-4v annealed per bms 7-39; finish f-10.10
01-148-2063
Structural Aircraft Plate
10.000" overall length 7.000" overall width 0.064" material thickness 6A1-4v annealed per bms 7-39; finish f-10.10
01-148-2064
Structural Aircraft Plate
6.000" overall length 1.500" overall width 0.020" material thickness 6A1-4v annealed per bms 7-39; finish f-10.10
01-148-2065
Structural Aircraft Plate
14.000" overall length 1.500" overall width 0.056" material thickness aisi 301, 1/2 hard, surface condition 2b; finish f-8.05
01-148-2066
Structural Aircraft Plate
26.000" overall length 11.000" overall width 0.056" material thickness 6A1-4v annealed per bms 7-39; finish f-10.10; opposite -4
01-148-2067
Structural Aircraft Plate
26.000" overall length 11.000" overall width 0.056" material thickness 6A1-4v annealed per bms 7-39; finish f-10.10; opposite p/n -3
01-148-2068
Structural Aircraft Plate
2.000" overall length 1.600" overall width 0.062" material thickness matl bac 1524-62
01-148-2069
Structural Component Air Support
Used on acft model f-16. al alloy per ams 4218-T61, 0.840 in.w, 1.790 in.h, 2.750 in.lg, located at bl 8.82, wl 80.44
01-148-2070
Structural Component Air Support
01-148-2071
Structural Component Air Support
01-148-2072
Structural Component Air Support
C/o 1 support pulley bracket, 1 nutplate
01-148-2073
Structural Component Air Support
01-148-2074
Structural Component Air Support
01-148-2075
Structural Component Air Support
01-148-2076
Structural Component Air Support
6.200" overall length 2.800" overall width 0.032" material thickness
01-148-2077
Structural Component Air Support
6.200" overall length 2.800" overall width 0.032" material thickness
01-148-2084
Aircraft Former
6.200" overall length 1.400" overall width 0.020" material thickness
01-148-2085
Aircraft Former
Used on B-52.
01-148-2086
Aircraft Former
Used on B-52. function-stiffener; extrusion
01-148-2087
Aircraft Former
Used on B-52. function-stiffener; extrusion
01-148-2089
Aircraft Former
Used on B-52. 6A1-4v; annealed; finish f-10.10
01-148-2090
Aircraft Former
Used on B-52. 6A1-4v, annealed, finish f-10.10
01-148-2091
Aircraft Former
1.500" overall length 0.500" overall width 0.030" material thickness
01-148-2092
Aircraft Former
1.500" overall length 0.500" overall width 0.030" material thickness
01-148-2093
Aircraft Former
21.900" overall length 2.600" overall width 0.025" material thickness
01-148-2094
Aircraft Former
26.400" overall length 3.300" overall width 0.040" material thickness 2nd matl/doc.
01-148-2097
Longeron
37.300" overall length 5.700" overall width 0.071" material thickness commercially pure; optional class 6
01-148-2098
Aircraft Skin
Used on B-52. 30.000" overall length 8.000" overall width surf cond 2d annealed
01-148-2099
Aircraft Skin
Used on B-52. 30.000" overall length 8.000" overall width surf cond 2d annealed
01-148-2100
Aircraft Skin
Used on B-52. 85.000" overall length 28.000" overall width finish f 2.130
01-148-2101
Aircraft Skin
Used on B-52. 85.000" overall length 18.000" overall width finish F2.130
01-148-2102
Aircraft Skin
Used on B-52. 120.000" overall length 8.000" overall width finish f 2.130
01-148-2103
Aircraft Skin
Used on B-52. 6A1-4v annealed, bms 7-39; finish f 10.10; opposite p/n -840
01-148-2104
Aircraft Skin
Used on B-52. 6A1-4v annealed, bms 7-39; finish f 10.10 ; opposite p/n -839
01-148-4083
Access Aircraft Cover
Used on b-52 aircraft. marked electrical receptacle access door; item attached with stud fasteners
01-148-4084
Access Aircraft Cover
Used on b-52 aircraft. marked electrical receptacle access door; door is attached with stud fasteners
01-148-4137
Structural Aircraft Plate
01-148-4183
Access Aircraft Cover
Used on b-52 acft.
01-148-4207
Structural Aircraft Plate
Function web assembly
01-148-4208
Structural Aircraft Plate
1.700" overall length 0.900" overall width 0.050" material thickness
01-148-4209
Structural Aircraft Plate
Temper T6; finish f-2.115
01-148-4210
Structural Aircraft Plate
1.250" overall length 1.250" overall width 0.016" material thickness
01-148-4211
Structural Aircraft Plate
10.000" overall length 5.500" overall width 0.040" material thickness
01-148-4212
Structural Aircraft Plate
1.000" overall length 0.500" overall width 0.062" material thickness matl bac 1524-6255
