01-159-9847
Aircraft Skin
01-160-1090
Access Aircraft Door
Used on acft model f-16c/d. located lower fs 110.4 to 124.0; c/o rivets, 20 grommet, 1 hinge, stiffener, cover, sealant; nha 16B1530-807; eff 5c 0001 9999; superseded p/n 16B1530-37 ow per ecn 1D461
01-160-1111
Elevator Balance Weight
01-160-1112
Elevator Balance Weight
01-160-1113
Elevator Balance Weight
01-160-1114
Elevator Balance Weight
01-160-1115
Elevator Balance Weight
01-160-1145
Aircraft Former
Used on acft model b-52.
01-160-1146
Structural Aircraft Plate
0.600" overall length 0.500" overall width 0.125" material thickness
01-160-1147
Structural Aircraft Plate
0.600" overall length 0.500" overall width 0.125" material thickness
01-160-1148
Aircraft Former
Opposite -3
01-160-1149
Structural Aircraft Plate
1.600" overall length 0.600" overall width 0.064" material thickness ht tr to 180, 000-200, 000
01-160-1159
Structural Aircraft Plate
Pre-impregnated glass fabric resin per mil-r-9299, type 11, class 2; includes 1 connector, 4 washers, 17 nuts, pan pn 3F21119-107
01-160-1160
Structural Component Air Support
Used on c-130 acft. location-qec kit; function-overheat detector mounting; matl-2024-T3 aluminum alloy per qq-a-362 cond T3; dim.-6.000 in. lg, 3.000 in. w, 0.040 in. thk
01-160-1170
Structural Aircraft Plate
4.900" overall length 2.150" overall width 0.020" material thickness
01-160-1171
Structural Aircraft Plate
Used on B-52. make from BAC540h-13-15
01-160-1172
Structural Aircraft Plate
Used on B-52. make from BAC540l-19-34
01-160-1173
Structural Aircraft Plate
Used on B-52. make from BAC540l-40-40
01-160-1174
Structural Aircraft Plate
Used on B-52. make from bac-540l-19-34
01-160-1175
Structural Aircraft Plate
Used on B-52. make from BAC1512-645 by 2.500
01-160-1176
Structural Aircraft Plate
Used on B-52.
01-160-1177
Structural Aircraft Plate
22.200" overall length 3.500" overall width 0.020" material thickness
01-160-1178
Structural Aircraft Plate
Used on B-52.
01-160-1179
Structural Aircraft Plate
Used on B-52. make from bac-540l-19-41
01-160-1180
Structural Aircraft Plate
11.600" overall length 1.050" overall width 0.020" material thickness
01-160-1181
Structural Aircraft Plate
19.200" overall length 1.100" overall width 0.020" material thickness
01-160-1182
Structural Aircraft Plate
9.900" overall length 1.000" overall width 0.020" material thickness
01-160-1183
Structural Aircraft Plate
23.950" overall length 1.300" overall width 0.040" material thickness
01-160-1184
Structural Aircraft Plate
13.700" overall length 1.050" overall width 0.040" material thickness
01-160-1185
Structural Aircraft Plate
12.200" overall length 1.000" overall width 0.040" material thickness
01-160-1186
Structural Aircraft Plate
9.700" overall length 1.500" overall width 0.020" material thickness
01-160-1187
Structural Aircraft Plate
Used on B-52.
01-160-1188
Structural Aircraft Plate
12.050" overall length 1.050" overall width 0.020" material thickness
01-160-1189
Structural Aircraft Plate
7.000" overall length 6.500" overall width 0.050" material thickness usd as end plate; opposite pn 25-2668-803
01-160-1191
Structural Aircraft Plate
Used on B-52. alter BAC143.30 lg
01-160-1192
Structural Aircraft Plate
Used on B-52. alter BAC143.30 lg.
01-160-1193
Structural Aircraft Plate
Used on B-52. stock size
01-160-1194
Structural Aircraft Plate
Used on B-52. stock size
01-160-1195
Structural Aircraft Plate
Used on B-52. stock size
01-160-1196
Structural Aircraft Plate
16.000" overall length 2.800" overall width 0.020" material thickness commercially pure
01-160-1197
Structural Aircraft Plate
13.300" overall length 5.700" overall width 0.063" material thickness 6al-4v
01-160-1198
Structural Aircraft Plate
33.100" overall length 10.600" overall width 0.100" material thickness
01-160-1199
Structural Aircraft Plate
21.000" overall length 1.250" overall width 0.250" material thickness
01-160-1200
Structural Aircraft Plate
5.500" overall length 0.750" overall width 0.100" material thickness
01-160-1201
Structural Aircraft Plate
2.120" overall length 1.880" overall width 0.063" material thickness used as adjusting plate; item is serrated; normalized
01-160-1204
Structural Component Air Support
Used on c-130 acft. location-qec kit; function-beam assembly support, fuselage station 448.20; matl-2024-T3 aluminum alloy clad per qq-a-362 cond T3
01-160-1205
Structural Component Air Support
Used on c-130 acft. location-qec kit; function-beam assembly support fuselage station 448.20; matl-2024-T3 aluminum alloy clad per qq-a-362 cond T3
01-160-1208
Structural Component Air Support
Used on c-130 acft. location-qec kit; function-beam assembly support fuselage station 461.40; matl-2024-T3 aluminum alloy clad per qq-a-362 cond T3; dim.-6.000 in. lg, 4.000 in. w, 0.050 in. thk
01-160-1220
Aircraft Former
7.800" overall length 1.600" overall width 0.020" material thickness
01-160-1221
Aircraft Former
7.800" overall length 1.600" overall width 0.020" material thickness
