01-264-8350
Air Circulating Ventilator
Used on acft,model f18.
01-264-8372
Former
Used on acft,model f18.
01-264-8604
Structural Aircraft Plate
Used on C-130. T6 clad
01-264-8605
Structural Aircraft Plate
Used on C-130. T6 alclad
01-264-8606
Aircraft Fairing
01-264-8607
Aircraft Fairing
01-264-8608
Aircraft Fairing
01-264-8609
Aircraft Fairing
01-264-8610
Aircraft Fairing
01-264-8611
Aircraft Fairing
01-264-8612
Aircraft Fairing
01-264-8613
Aircraft Fairing
01-264-8616
Aircraft Fairing
01-264-8617
Aircraft Fairing
01-264-8618
Aircraft Fairing
Nha 3F10232; opposite -201; same as -102
01-264-8619
Aircraft Fairing
01-264-8620
Structural Component Air Support
Used on f-16c/d aircraft. nha 16W1050-1
01-264-8622
Structural Component Air Support
Used on acft model b-1b.
01-264-8645
Aircraft Skin
Used on f-16c aircraft.
01-264-9215
Structural Component Air Support
0.063" material thickness primer epoxy-polyamide surface treated
01-264-9507
Structural Component Aircr Patch
Consists of four plies; 4.000 in. lg; 2.000 in. w
01-264-9508
Structural Component Aircr Patch
Consists of four plies; 6.000 in. lg; 4.000 in. w
01-264-9884
Aircraft Former
Used on C-141.
01-265-2023
Fuel Aircraft Tank
Used on oh-58d army helicopter improvement program (ahip) rotary wing aircraft.
01-265-2046
Aircraft Door
Used on ch-47 chinook. flight safety critical part, door emergency
01-265-2519
Aircraft Windshield Panel
Used on acft,model au8.
01-265-2876
Aircraft Fairing
30.000" overall length 5.000" overall width 0.065" material thickness
01-265-2877
Aircraft Fairing
30.000" overall length 5.000" overall width 0.065" material thickness
01-265-3591
Structural Aircraft Panel
01-265-3848
Structural Component Air Fitting
Engine control throttle gate
01-265-4004
Structural Aircraft Plate
Used on C-141. cond 0
01-265-4005
Structural Component Air Support
01-265-4006
Structural Component Air Support
01-265-4007
Structural Component Air Support
01-265-4015
Aircraft Former
T7351
01-265-4016
Aircraft Former
Used on F-5.
01-265-4017
Aircraft Former
Used on F-5.
01-265-4018
Aircraft Former
Nha 16T9190-5
01-265-4019
Aircraft Former
Used on C-141.
01-265-4084
Radome
Used on b-1b aircraft. nuclear hardness critical item; p/o: radome assy, side fuselage, sta YF636.00 to sta YF753.50 ctd; c/o: facesheets, core, plies, blocks, ram, strips, pykor layer, edge; opposite -082
01-265-4085
Radome
Used on b-1b aircraft. p/o: radome assy, fuselage side, YF758.5 ctd to YF863.5 ctd; u/o acft 9 thru 64 only; c/o: cores, plies & spcl plies, sawtooth, face sheets, blocks, inner rams, laminates, pykro layers, lightning diverter strips, contact, fittings, disks, grommets, studs, retainers, & misc hrdwre; opp -021
01-265-4086
Radome
Used on b-1b aircraft. featgp/o: radome assy, fuselage side, YF758.5 ctd to YF863.5 ctd; u/o acft 9 thru 64 only; c/o: cores, plies, spcl cores, sawtooth, face sheets, blocks, inner rams, laminates, pykro layers, lightning diverter strips, contacts, fittings, disks, grommets, studs, retainers, & misc hrdwre; opposite -022
01-265-4087
Radome
Used on b-1b aircraft. nuclear hardness critical item; p/o radome assy, side fuselage, sta YF636.00 to YF753.50; c/o: facesheets, core, plies, blocks, ram, strips, pykor layer edge; opposite -081
01-265-4959
Structural Aircraft Panel
01-265-5118
Access Aircraft Door
Used on f-16 aircraft.
01-265-5137
Airfoil Rib
7.000" overall length 5.000" overall width 0.032" material thickness
01-265-5141
Airfoil Rib
8.000" overall length 6.000" overall width 0.032" material thickness
01-265-5144
Airfoil Rib
6.000" overall length 5.000" overall width 0.032" material thickness
01-265-5145
Airfoil Rib
6.000" overall length 5.000" overall width 0.032" material thickness
01-265-5177
Intake Muffler
Used on f-16d aircraft. 8.700" overall length 3.000" overall width
