01-118-3591
Structural Aircraft Panel
Used on c-5 acft. matl metal plate, AMS5596, inconel 718; matl size 0.050 by 6.000 by 14.000 in. lg; part of pylon
01-118-3593
Airfoil Rib
8.600" overall length 5.000" overall width 0.040" material thickness
01-118-3595
Airfoil Rib
7.700" overall length 5.000" overall width 0.040" material thickness
01-118-3596
Airfoil Rib
7.700" overall length 5.000" overall width 0.040" material thickness
01-118-3597
Airfoil Rib
8.300" overall length 5.000" overall width 0.032" material thickness
01-118-3598
Airfoil Rib
8.600" overall length 5.800" overall width 0.040" material thickness
01-118-3599
Airfoil Rib
8.600" overall length 5.000" overall width 0.040" material thickness
01-118-3970
Aircraft Skin
20.000" overall length 15.000" overall width
01-118-3971
Aircraft Skin
35.000" overall length 25.000" overall width
01-118-3972
Aircraft Skin
40.000" overall length 40.000" overall width
01-118-3973
Aircraft Skin
20.000" overall length 15.000" overall width
01-118-4521
Structural Aircraft Panel
Used on c-5a acft. matl al alloy mil-a-8923 7079-T6, matl size .050 x 7 x 35; part of door, fixed leading edge, track 2b
01-118-4522
Structural Aircraft Panel
Used on c-5a acft. matl al alloy qq-a-250/12 7075-T6, matl size .040 by 2 by 24; part of panel, underwing tan fillet, fuselage station 1285.66 to 1353.66
01-118-4524
Structural Aircraft Plate
XW155.024
01-118-4525
Structural Aircraft Plate
Function-splice plate, surge tank
01-118-4529
Structural Component Air Support
Used on acft model f111. use on latch, aft side door, weapons bay, fuselage station 443.352
01-118-4530
Structural Component Air Support
Used on acft model f111. used on latch, aft side door, weapons bay, fuselage station 443.352
01-118-4541
Airfoil Rib
Used on A-7. 9.200" overall length 5.100" overall width 0.040" material thickness finish F27; ht tr
01-118-4542
Airfoil Rib
Used on A-7. 13.500" overall length 5.800" overall width 0.040" material thickness finish F27; ht tr
01-118-4543
Airfoil Rib
Used on A-7. 13.200" overall length 5.800" overall width 0.040" material thickness finish F27; ht tr
01-118-4544
Airfoil Rib
Used on A-7. 12.900" overall length 5.600" overall width 0.040" material thickness finish F27; ht tr
01-118-4545
Airfoil Rib
Used on A-7. 11.800" overall length 5.600" overall width 0.040" material thickness finish F27; ht tr
01-118-4546
Airfoil Rib
Used on A-7. 11.400" overall length 5.500" overall width 0.040" material thickness finish F27; ht tr
01-118-4547
Airfoil Rib
Used on A-7. 11.100" overall length 5.400" overall width 0.040" material thickness finish F27; ht tr
01-118-4548
Airfoil Rib
Used on A-7. 10.400" overall length 4.800" overall width 0.040" material thickness finish F27; ht tr
01-118-4550
Airfoil Rib
Used on A-7. 9.700" overall length 4.600" overall width 0.040" material thickness finish F27; ht tr
01-118-4551
Airfoil Rib
Used on A-7. 8.600" overall length 4.300" overall width 0.040" material thickness finish F27; ht tr
01-118-4552
Airfoil Rib
Used on A-7. 8.200" overall length 4.200" overall width 0.040" material thickness finish F27; ht tr
01-118-4553
Airfoil Rib
Used on A-7. 7.800" overall length 4.000" overall width 0.040" material thickness finish F27; ht tr
01-118-4554
Airfoil Rib
Used on A-7. 7.100" overall length 3.700" overall width 0.040" material thickness finish F27; ht tr
01-118-5198
Structural Aircraft Plate
20.500" overall length 1.700" overall width 0.060" material thickness
01-118-5204
Aircraft Fairing
01-118-5205
Aircraft Fairing
01-118-5206
Aircraft Fairing
01-118-5259
Structural Aircraft Panel
Used on F-111. c/o block assembly p/n C31B6806-1, doubler p/n C31B6815-15, doubler p/n C31B6815-17
01-118-5264
Structural Aircraft Panel
Cond 0, T42
01-118-5265
Structural Aircraft Panel
01-118-5266
Structural Aircraft Panel
01-118-5270
Structural Component Air Support
Used on acft model f111. aluminum per 2024-T851, 6.600 in. lg, 2.200 in. w, 2.000 in. thk
01-118-5271
Structural Component Air Support
Used on c141b acft. matl 2024-0 clad qq-a-250/5 T42; used on fuselage station 404.00
01-118-5281
Exhaust Pipe Flange
Used on acft model f-16a/b usaf. steel per mil-s-6721 type 321; eff 61-0009-9999; nha 16P1555-3
01-118-5282
Exhaust Pipe Flange
Used on acft model f-16a/b usaf. steel per mil-s-6721 type 321; eff 61-0009-9999; nha 16P1555-3
01-118-5283
Exhaust Pipe Flange
Used on acft model f-16a/b usaf. steel per mil-s-6721 type 321; eff 61-0200-9999; nha 16P1555-3
01-118-5290
Aircraft Skin
55.000" overall length 29.000" overall width superceded 16B4621-36 ni per ecn 2B958; nha 16B416-815; eff on 61-0262-9999
01-118-5291
Aircraft Skin
C/o skin p/n 16B4621-47
01-118-5296
Aircraft Skin
01-118-5297
Aircraft Skin
01-118-5298
Aircraft Skin
