01-298-9026
Aircraft Skin
Used on acft model b-1b. 7075-0 al bare sheet per qq-a-250/12; 13.50 in lg, 12.00 in wd, 0.125 in thk; opposite -006
01-298-9028
Aircraft Skin
Used on acft model b-1b. 7075-0 al bare sheet per qq-a-250/12; 13.50 in lg, 12.00 in wd, 0.125 in thk; opposite -005
01-298-9033
Aircraft Stringer
01-298-9283
Control Surface Aircraft Fairing
01-299-0249
Structural Component Air Support
01-299-0326
Aircraft Skin
01-299-1152
Structural Aircraft Plate
Used on F-111.
01-299-1153
Structural Component Air Support
Used on acft model f-15. 2024-0 per qq-a-250/4 cond 0; 16.36 in lg, 8.00 in wd, 0.063 in thk
01-299-1158
Aircraft Former
3.960" overall length 2.150" overall width 0.050" material thickness finish f-1; nha 388085-1
01-299-1163
Airfoil Rib
7.500" overall length 4.810" overall width 0.063" material thickness opposite -006
01-299-1164
Stiffener Aircraft Rib
7.500" overall length 4.810" overall width 0.063" material thickness opposite -005
01-299-1165
Aircraft Skin
Used on acft model b-1b. 7075-T73 al clad sh per ST0170LB0030; 62.12 in lg, 34.50 in wd, 0.075 in thk; nha L1802005
01-299-1166
Aircraft Skin
Used on acft model b-1b. 7075-T73 al clad sht per ST0170LB0030; 63.62 in lg, 52.00 in wd, 0.075 in thk; nha L1804001
01-299-1167
Aircraft Skin
Used on acft model b-1b. 7075-T73 al clad sht per ST0170LB0030; 64.38 in lg, 47.50 in wd, 0.075 in thk; nha L1804001
01-299-1168
Aircraft Skin
Used on acft model b-1b. 7075-T73 al clad sht per ST0170LB0030; 66.12 in lg, 43.12 in wd, 0.075 in thk; nha L1804003
01-299-1169
Aircraft Skin
Used on acft model b-1b. 7075-T73 al clad sht per ST0170LB0030; 66.12 in lg, 43.12 in wd, 0.075 in thk; nha L1804003
01-299-1170
Aircraft Skin
Used on acft model b-1b. 7075-T73 al clad sht per ST0170LB0030; 66.12 in lg, 43.12 in wd, 0.075 in thk; nha L1804003
01-299-1171
Aircraft Trailing Edge
Consist of 1 spar, 2 skin, 3 closeout, 1 core, rivet a/r; nha L180400 1
01-299-1172
Aircraft Trailing Edge
Consist of 1 spar, 2 skin, 3 closeout, 1 core, rivet a/r; nha L180400 1
01-299-1173
Aircraft Trailing Edge
Consist of 1 spar, 2 skin, 3 closeout, 1 core, rivet a/r; nha L180400 2
01-299-1174
Aircraft Trailing Edge
Consist of 1 spar, 2 skin, 3 closeout, 1 core, rivet a/r; nha L180400 2
01-299-1175
Aircraft Trailing Edge
Consist of 1 spar, 2 skin, 3 closeout, 1 core, rivet a/r; nha L180400 3
01-299-1176
Aircraft Trailing Edge
C/o: 1 spar, 2 skin, 3 closeout, 1 core, rivet a/r; nha L1804003
01-299-1510
Pylon Aircraft Fairing
Used on f-14a acft.
01-299-1511
Wing Aircraft Fairing
Used on aircraft model p-3.
01-299-1512
Wing Aircraft Fairing
Used on aircraft model p-3.
01-299-1513
Structural Component Air Support
Used on aircraft model av-8. aluminum alloy
01-299-1712
Pylon Aircraft Fairing
Used on acft model av-8b.
01-299-2067
Structural Aircraft Plate
Used on acft model b-1b.
01-299-2068
Wing Aircraft Fairing
Used on aircraft model p-3.
01-299-2071
Structural Component Air Support
Used on acft model b-1b.
01-299-2072
Structural Component Air Support
Used on acft model b-1b.
01-299-2073
Structural Component Air Support
Used on acft model b-1b.
01-299-2074
Structural Component Air Support
Used on acft model b-1b.
01-299-2075
Structural Component Air Support
C/o 1 fitting, 2 bushing; nha L1800075
01-299-2096
Stiffener Aircraft Rib
C/o 1 seal, 1 stud, 3 bushing, 1 rib, 1 insert; nha L1804003
01-299-2097
Stiffener Aircraft Rib
C/o 1 rib, 1 seal, 3 bushings; nha L1804003
01-299-2098
Stiffener Aircraft Rib
C/o 1 seal, 1 stud, 3 bushing, 1 rib, 1 insert; nha L1804003
01-299-2099
Aircraft Skin
Used on aircraft model f-14.
01-299-2100
Aircraft Skin
Used on s-3 acft. 69.000 in. l; 22.600 in. w; 0.125 in. thk
01-299-2101
Aircraft Skin
Used on aircraft model s-3.
01-299-2538
Structural Component Air Support
Used on acft model c-141a/c. 7075-T6 alum; 3.0 in lg, 2.0 in wd, 2.0 in thk; used to connect inner wing to center wing
01-299-2547
Aircraft Former
13.500" overall length 7.900" overall width 0.050" material thickness nha -1001
01-299-2548
Aircraft Former
13.800" overall length 7.900" overall width 0.050" material thickness nha -1001
01-299-2549
Aircraft Former
13.500" overall length 7.900" overall width 0.050" material thickness nha -1001
01-299-2550
Aircraft Former
13.500" overall length 7.900" overall width 0.050" material thickness nha -1001
01-299-2618
Bell Crank
Used on acft model b-1b. consist of 2 support, 1 bellcrank, 2 nut, 2 cotter pin, 2 bolt; nha L5235401; located xrs 202; used on wing spoiler control bellcrank assembly
01-299-3511
Structural Aircraft Plate
Used on C-141. T3 clad
01-299-3518
Stiffener Aircraft Rib
C/o 1 rib, 1 seal, 3 bushing; nha L1804003
01-299-3519
Aircraft Skin
Consist of 1 tee, 4 covering; nha L3045519
