01-152-2006
Aircraft Stiffener
01-152-2007
Structural Aircraft Plate
Used on B-52.
01-152-2008
Structural Aircraft Plate
Used on B-52.
01-152-2009
Structural Aircraft Plate
Used on B-52.
01-152-2107
Structural Aircraft Plate
8.500" overall length 5.500" overall width 0.063" material thickness
01-152-2108
Structural Aircraft Plate
6.500" overall length 2.500" overall width 0.063" material thickness
01-152-2109
Aircraft Former
3.000" overall length 2.000" overall width 0.063" material thickness
01-152-2110
Aircraft Former
12.500" overall length 1.500" overall width 0.063" material thickness
01-152-2112
Aircraft Fairing
C/o 1 skin, 1 bulkhead, 1 angle, 1 filler, 1 shim, 25 rivets
01-152-2113
Cowling
Used on b-52 aircraft.
01-152-2114
Cowling
Used on b-52 aircraft.
01-152-2115
Cowling
Used on b-52 aircraft.
01-152-2116
Structural Aircraft Plate
Used on B-52. application-kit, splitter web spray duct
01-152-2117
Structural Component Air Support
52.000" overall length 1.000" overall width 0.032" material thickness
01-152-2118
Aircraft Fairing
01-152-2121
Aircraft Former
Used on b-52 acft.
01-152-2122
Aircraft Former
Used on b-52 acft.
01-152-2135
Structural Aircraft Plate
9.700" overall length 0.750" overall width 0.068" material thickness
01-152-2136
Structural Aircraft Plate
10.500" overall length 0.750" overall width 0.068" material thickness
01-152-2137
Structural Aircraft Plate
11.300" overall length 0.750" overall width 0.068" material thickness
01-152-2138
Structural Aircraft Plate
Used on B-52. 2.260" overall length 0.700" overall width
01-152-2139
Structural Aircraft Plate
6.000" overall length 2.000" overall width ht tr to cond T4; finish f-2.115; opposite pn -31
01-152-2140
Structural Aircraft Plate
30.000" overall length 6.500" overall width 0.020" material thickness finish f-10.10; used on -516, -522
01-152-2141
Structural Component Air Support
2.600" overall length 1.800" overall width 0.040" material thickness tempered T3; finish f-2.115; used on -803
01-152-2142
Structural Component Air Support
3.000" overall length 2.500" overall width 0.025" material thickness used on -516, -522,
01-152-2143
Structural Component Air Support
2.700" overall length 0.700" overall width 0.032" material thickness used as bracket; finish f-2.115
01-152-2144
Structural Component Air Support
1.000" overall length 0.900" overall width 0.050" material thickness used on -516, -522, & -543; finish f-2.115
01-152-2146
Aircraft Former
12.800" overall length 1.800" overall width 0.032" material thickness opposite-8; used on -516, -522
01-152-2147
Aircraft Former
40.400" overall length 2.400" overall width 0.025" material thickness opposite -71; used on -516, -522
01-152-2148
Aircraft Former
17.500" overall length 1.500" overall width 0.025" material thickness used on -516, -522
01-152-2149
Aircraft Former
12.300" overall length 1.800" overall width 0.032" material thickness opposite -7; used on -516, -522
01-152-2150
Aircraft Former
3.700" overall length 3.000" overall width 0.040" material thickness used on -516, -522
01-152-2151
Aircraft Former
8.300" overall length 7.500" overall width 0.040" material thickness heat treat T4
01-152-2152
Aircraft Former
7.300" overall length 0.025" material thickness used on-516, -522
01-152-2153
Aircraft Former
3.900" overall length 1.600" overall width 0.025" material thickness used on -516, -522
01-152-2154
Aircraft Former
6.500" overall length 2.500" overall width 0.032" material thickness opposite -198; heat treat T4; finish f-2.115
01-152-2155
Aircraft Former
6.500" overall length 2.500" overall width 0.032" material thickness opposite -197; finish f-2.115; heat treat T4
01-152-2156
Aircraft Former
2.600" overall length 1.700" overall width 0.040" material thickness opposite -200; tempered T3; finish f-2.115
01-152-2157
Aircraft Former
2.600" overall length 1.700" overall width 0.040" material thickness opposite -39; tempered T3
01-152-2158
Aircraft Former
2.600" overall length 1.700" overall width 0.040" material thickness opposite of -202; tempered T3
01-152-2159
Aircraft Former
0.750" overall length 0.700" overall width 0.050" material thickness tempered T3; finish f-2.115
01-152-2160
Aircraft Former
2.500" overall length 1.500" overall width 0.025" material thickness opposite -815; tempered T3
01-152-2161
Aircraft Former
Used on acft model b-52. c/o 1 brackel, 1 channel, 6 nut pplate
01-152-2162
Longeron
Used on B-52.
01-152-2163
Longeron
Used on B-52.
01-152-2164
Longeron
45.000" overall length 3.500" overall width 0.040" material thickness opposite -80; finish f-10.10
01-152-2165
Longeron
45.000" overall length 3.500" overall width 0.040" material thickness opposite pn -79; finish f 10.10
01-152-2166
Aircraft Skin
Used on B-52. 21.000" overall length 15.000" overall width opt annealed
01-152-2169
Aircraft Skin
Used on B-52. 10.400" overall length 1.400" overall width
01-152-2170
Aircraft Skin
Used on B-52. 12.500" overall length 1.400" overall width
