01-236-3571
Structural Component Air Support
20.220" overall length 2.420" overall width 0.050" material thickness
01-236-3572
Structural Component Air Support
22.580" overall length 4.860" overall width 0.050" material thickness
01-236-3573
Structural Component Air Support
1.320" overall length
01-236-3574
Structural Component Air Support
Used on f-15 aircraft. 1.75 by 3.00 by 9.30 2024-T851 bar stock, specification qqa-225/6 cond T851; part of 1005 repair vertical stabilizer
01-236-3575
Structural Component Air Support
Used on f-15 acft. sill-lower outboard empennage support beam canted; fuselage station 672.680
01-236-3576
Structural Component Air Support
Used on f-15 acft. assy-brackets, angle, clip nut-conduit supports, wing
01-236-3577
Structural Component Air Support
Used on f-15 acft. sill-lower outboard empennage support beam canted; fuselage 672.680
01-236-3588
Structural Aircraft Panel
Used on f-5e aircraft. panel assembly-rh console removable; c/o: stud (10) , doubler (10) , pin (10) grommet (10) , -57 panel (1)
01-236-3611
Aircraft Former
3.400" overall length
01-236-3612
Aircraft Former
01-236-3613
Aircraft Former
01-236-3626
Aircraft Leading Edge
Consist of 3 layup, 1 core; opposite p/n -002; nha L3226031
01-236-3627
Airfoil Rib
7.620" overall length 2.620" overall width 0.050" material thickness
01-236-3628
Airfoil Rib
8.620" overall length 3.000" overall width 0.050" material thickness
01-236-3629
Airfoil Rib
7.350" overall length 3.000" overall width 1.750" material thickness
01-236-3630
Aircraft Skin
Used on F-16. 34.000" overall length 14.000" overall width
01-236-3631
Aircraft Skin
Used on F-15. 24.480" overall length 24.300" overall width
01-236-3632
Aircraft Skin
Used on F-15. 24.480" overall length 24.300" overall width
01-236-3633
Aircraft Skin
Used on acft model b-1b. consist of 1 closeout, 1 plate; nha L3226900
01-236-4674
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 type 3 comp c annealed; p/o sidewall closure engine fairing
01-236-4675
Structural Component Air Support
Used on f-15 acft. aluminum alloy 7075-T7351; p/o sidewall closure-engine fairing
01-236-4676
Structural Component Air Support
Used on f-15 acft. alluminum alloy 2024-0 alclad; p/o sidewall closure, engine fairing
01-236-4677
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 type 3 comp c annealed; p/o sidewall closure, engine fairing
01-236-4678
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 tpye 3 comp c annealed; p/o sidewall closure, engine fairing
01-236-4679
Structural Component Air Support
Used on f-15 acft. aluminum alloy 2024-0 alclad; p/o sidewall closure, engine fairing
01-236-4680
Structural Component Air Support
Used on f-15 acft. aluminum alloy 2024-0 alclad; p/o sidewall closure, engine fairing
01-236-4681
Structural Component Air Support
Used on f-15 acft. aluminum alloy 2024-0 alclad; p/o sidewall closure, engine fairing
01-236-4682
Structural Component Air Support
Used on f-15 acft. aluminum alloy 2024-0 alclad; p/o sidewall closure, engine fairing
01-236-4683
Structural Component Air Support
Used on f-15 acft. aluminum alloy 2024-0 alclad; p/o sidewall closure, engine fairing
01-236-4684
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-l-9046 type 3 comp c annealed; p/o sidewall closure, engine fairing
01-236-4685
Structural Component Air Support
Used on f-15 acft. titanium alloy per mil-t-9046 type 3 cond c annealed; p/o sidewall closure, engine fairing
01-236-4686
Structural Component Air Support
Used on f-15 acft. aluminum alloy 2024-0 alclad; p/o sidewall closure, engine fairing
01-236-4704
Structural Aircraft Panel
P/o cover, compartment-acft mtd auxiliary drive
01-236-4715
Aircraft Former
01-236-4716
Aircraft Former
01-236-4724
Aircraft Skin
Used on aircraft model av-8. aluminum alloy per qq-a-250/13, cond o
01-236-4725
Aircraft Trailing Edge
01-236-5133
Aircraft Fairing
33.250" overall length 14.880" overall width
01-236-5794
Control Surface Aircraft Fairing
20.547" overall length 0.500" material thickness
01-236-5795
Structural Component Air Support
Used on 1560-00-910-4259. type/model designation:t-38a/nf-5a/b aluminum alloy; left hand design
01-236-6951
Structural Component Air Support
01-236-6952
Structural Component Air Support
3.408" overall length
01-236-7765
Structural Aircraft Plate
Used on A-10. 6.500" overall length 5.500" overall width 0.050" material thickness 17-7ph sht
01-236-7766
Structural Aircraft Plate
Used on A-10. 6.500" overall length 5.500" overall width 0.050" material thickness 17-7 ph sheet
01-236-7767
Structural Aircraft Plate
Used on A-10. 6.500" overall length 2.500" overall width 0.050" material thickness
01-236-7768
Structural Aircraft Plate
Used on A-10. 7.000" overall length 1.630" overall width 0.032" material thickness
01-236-7769
Structural Aircraft Plate
Used on A-10. 7.000" overall length 2.500" overall width 0.050" material thickness
01-236-7770
Structural Aircraft Plate
Used on F-15. for inlet repair, engine; channel
01-236-7771
Structural Aircraft Plate
Used on F-15. channel
01-236-7774
Structural Aircraft Plate
Used on F-15. 27.000" overall length 7.350" overall width 0.063" material thickness web; opposite -2278
