01-148-6336
Structural Component Air Support
9.375" overall length 4.750" overall width 2.000" material thickness
01-148-6337
Structural Component Air Support
16.000" overall length 15.000" overall width 3.500" material thickness
01-148-6338
Structural Component Air Support
19.250" overall length 15.000" overall width 3.500" material thickness
01-148-6339
Structural Component Air Support
19.250" overall length 15.000" overall width 3.500" material thickness
01-148-6351
Aircraft Former
9.000" overall length 2.700" overall width 0.063" material thickness heat treated to condition T6; finish f-2.115
01-148-6352
Aircraft Former
1.500" overall length 0.750" overall width 0.120" material thickness finish f-2.30
01-148-6353
Aircraft Former
7.000" overall length 2.000" overall width 0.127" material thickness finish f-2.115
01-148-6354
Aircraft Former
17.500" overall length 1.600" overall width 0.050" material thickness
01-148-6489
Aircraft Pylon
Used on acft model f-18. cognizant service:navy;
01-148-7143
Stiffener Aircraft Rib
01-148-7157
Structural Aircraft Plate
7.000" overall length 2.500" overall width 0.080" material thickness opposite to p/n 25-2395-9; used asdoubler on rib number 4
01-148-7158
Structural Aircraft Plate
6.500" overall length 2.500" overall width 0.080" material thickness opposite to p/n 25-2395-8; used asdoubler on rib number 4
01-148-7159
Structural Aircraft Plate
6.500" overall length 2.500" overall width 0.080" material thickness opposite to p/n 25-2395-7; used asdoubler on rib number 4
01-148-7160
Structural Aircraft Plate
8.500" overall length 2.500" overall width 0.080" material thickness opposite to p/n 25-2395-808; used as doubler on rib number 4
01-148-7161
Structural Aircraft Plate
8.500" overall length 2.500" overall width 0.080" material thickness opposite to p/n 25-2395-808; used as doubler on rib number 4
01-148-7162
Structural Aircraft Plate
7.000" overall length 12.500" overall width 0.080" material thickness opposite to p/n 25-2395-10; used as doubler on rib number 4
01-148-7163
Structural Aircraft Plate
12.000" overall length 3.000" overall width 0.063" material thickness opposite to p/n 25-2396-814; used as doubler on rib number 5
01-148-7164
Structural Aircraft Plate
12.000" overall length 3.000" overall width 0.063" material thickness opposite to p/n 25-2396-813; used as doubler on rib number 5
01-148-7165
Structural Aircraft Plate
Function-web assembly
01-148-7166
Structural Aircraft Plate
Function-filler
01-148-7167
Structural Aircraft Plate
8.600" overall length 8.300" overall width 0.030" material thickness function-doubler; matl 6al-4v
01-148-7168
Structural Aircraft Plate
Function-web assembly
01-148-7169
Structural Aircraft Plate
Function-web assembly
01-148-7170
Structural Aircraft Plate
Used as sheer plate on firewall
01-148-7171
Structural Aircraft Plate
Used as filler on firewall installation forward nacelle; opposite p/n 25-2308-115
01-148-7172
Structural Aircraft Plate
2.500" overall length 1.000" overall width 0.125" material thickness
01-148-7173
Structural Aircraft Plate
01-148-7174
Structural Aircraft Plate
01-148-7175
Structural Aircraft Plate
01-148-7176
Structural Aircraft Plate
01-148-7177
Structural Aircraft Plate
01-148-7178
Structural Aircraft Plate
Used on acft model b-52. steel cres sheet AISI302 mil-s-5059 comp 302 surf cond 2d annealed, 31.000 in. lg, 13.000 in. w, 0.063 in. thk
01-148-7179
Structural Aircraft Plate
Used on acft model b-52. steel cres sheet per AISI302 mil-s-5059 comp 302 surf cond 2d annealed, 16.600 in. lg, 1.500 in. w, 0.040 in. thk, located fuselage station 236.25
01-148-7182
Structural Aircraft Plate
Used on b-52 aircraft. material-2024 clad aluminum-T3 per qq-a-250/5; location-pp station 236.25, tail fairing installation-outboard strut
01-148-7183
Structural Aircraft Plate
Used on b-52 aircraft. material-2024 aluminum clad per qq-a-250/5; location-270.00 pp station
01-148-7184
Structural Aircraft Plate
Material-aisi 301, 1/2 hard surface cond 2b
01-148-7187
Structural Aircraft Plate
Rib number 6 installation
01-148-7188
Structural Aircraft Plate
Opposite -6; rib number 6 installation
01-148-7189
Structural Aircraft Plate
Opposite -5; rib number 6 installation
01-148-7190
Structural Aircraft Plate
01-148-7191
Structural Aircraft Plate
01-148-7192
Structural Aircraft Plate
3.500" overall length 1.000" overall width 0.040" material thickness used as doubler on firewall installation
01-148-7193
Structural Aircraft Plate
1.750" overall length 1.000" overall width 0.040" material thickness used as doubler on firewall installation
01-148-7194
Structural Aircraft Plate
5.000" overall width 0.080" material thickness opp p/n 25-2600-14; used as splice plate on rib number 2 installation
01-148-7195
Structural Aircraft Plate
5.000" overall width 0.080" material thickness opp p/n 25-2600-13; used as splice plate on rib number 2 installation
01-148-7196
Structural Aircraft Plate
4.400" overall width 0.080" material thickness opp p/n 25-2600-15; used as splice plate on rib number 2 installation
01-148-7197
Structural Aircraft Plate
Make from BAC5408-13-131
01-148-7198
Structural Aircraft Plate
Make from bac 5408-13-26
01-148-7199
Structural Component Air Bracket
Clip make from BAC1606-100104 spec material
01-148-7200
Structural Component Air Support
