01-079-0683
Landing Gear Aircraft Fairing
Aluminum alloy qq-a-250/11, alloy 6061-0;
01-079-0684
Landing Gear Aircraft Fairing
Aluminum alloy qq-a-250/13, alloy 7075-T6;
01-079-0685
Landing Gear Aircraft Fairing
Aluminum alloy qq-a-250/13, alloy 7075-T6;
01-079-0686
Aircraft Skin
Used on aircraft model a-4m. aluminum alloy, 84.000 lg, 54.000 in. w, 0.190 in. thk
01-079-0687
Aircraft Skin
Used on aircraft model a-4m.
01-079-0688
Aircraft Skin
Used on aircraft model a-4m.
01-079-0689
Aircraft Skin
Used on ta-4j aircraft. aluminum qq-a-250/13, alloy 7075-0
01-079-0709
Fluid Aircraft Manifold
01-079-0815
Aircraft Fairing
01-079-0820
Aircraft Fairing
01-079-2036
Structural Component Air Support
Used on acft model 1f4c. alum alloy 7178-0 per qq-a-250/15 cond 0, stock size 0.040 in.thick, 5.70 in.wide, 20.90 in.length, right hand, used on 82r door
01-079-2038
Aircraft Stiffener
11.550" overall length 1.300" overall width 0.040" material thickness 0 temper
01-079-2039
Structural Component Air Bracket
4.000" overall length 1.300" overall width 0.100" material thickness
01-079-2131
Aircraft Skin
Used on C-141.
01-079-2133
Aircraft Windshield Panel
48.000" overall length 48.000" overall width procure w/o radar reflective coating; polycarbonate/acrylic laminated ply transparency
01-079-2134
Aircraft Window Panel
48.000" overall length 48.000" overall width polycarbonate/acrylic laminated ply transparency, procure w/o radar reflective coating
01-079-2137
Aircraft Windshield Panel
54.000" overall length 48.000" overall width polycarbonate/acrylic laminated ply transparency; color - golden yellow
01-079-2717
Thermal Special Purpo Insulation
Plastic epoxy, mil-p-18177; fscm 35351 p/n 161121-01
01-079-4106
Structural Component Air Support
C/o 1 support, 1 pad, misc hardw
01-079-4111
Structural Component Air Support
01-079-5647
Structural Component Air Bracket
4.120" overall length 1.930" overall width 1.620" material thickness bracket assembly; c/o: bracket p/n 7930687-01, bushing p/n NAS77-4-28; nha gen dyn p/n 12K3070-831
01-079-6235
Aircraft Skin
Used on acft c135. outboard panel, inboard door aft, main gear
01-079-6236
Aircraft Skin
01-079-6237
Aircraft Skin
Used on f-16 airplane.. 26.000" overall length 12.000" overall width
01-079-6238
Aircraft Skin
Used on f-16 airplane.. 26.000" overall length 12.000" overall width
01-079-6239
Aircraft Skin
Used on f-16 airplane.. 28.000" overall length 17.000" overall width
01-079-6376
Aircraft Fairing
Used on helicopter,model uh-1h.
01-079-7677
Structural Component Air Support
Used on acft model f-16. alum alloy 7075-T73 per qq-a-367 comp 7075, temper T73, verify heat treat per NDTS1500
01-079-8754
Access Aircraft Door
01-079-8755
Access Aircraft Door
01-079-8756
Access Aircraft Door
01-080-0240
Structural Component Air Support
Used on aircraft model a-10. cres sheet, mil-s-25043 cond a, 17-7 ph, passivated, mil-s-5002; one leg 3.080 in. lg, one leg 1.092 in. lg, 2.700 in. w; 0.016 in. thk; contains hole 0.240 in. min, 0.250 in. max dia
01-080-0948
Structural Aircraft Panel
5.750" overall length 3.370" overall width u/a:panel, console; matl:temp t-3
01-080-0950
Structural Aircraft Plate
34.400" overall length 5.100" overall width 0.063" material thickness
01-080-1020
Aircraft Deceleron
Form, fit
01-080-1022
Structural Component Air Fitting
P/o: front spar attachment to stabilizer 160D511400
01-080-1095
Structural Aircraft Plate
Used on acft model t-39. 15.500" overall length 1.250" overall width 0.040" material thickness bottom double for aft tail cone
01-080-1106
Aircraft Skin
Used on t-39 airplane.. 28.000" overall length 16.000" overall width heat treat per T4 mil-h-6088, finished with alodine film per mil-c-5541
01-080-1107
Aircraft Skin
Used on t-39 airplane.. 28.000" overall length 16.000" overall width heat treat cond T4 per mil-h-6088 finished with alodine film per mil-c-5541, painted with one coat of mil-p-23377 primer
01-080-3083
Structural Aircraft Panel
Used on F-16. p/n 16T7240
01-080-4055
Fuel Aircraft Tank
01-080-4063
Radome
Used on acft e3a.
01-080-4064
Stiffener Aircraft Rib
01-080-4065
Stiffener Aircraft Rib
Finish f-2.10
01-080-4066
Stiffener Aircraft Rib
Finish f-2.10
01-080-4086
Aircraft Skin
Used on F-15. 19.500" overall length 13.330" overall width ht treat to T62 per PS15534, chemical mill per PS20022
01-080-4087
Aircraft Skin
Used on F-16. 28.000" overall length 17.000" overall width
01-080-5303
Structural Component Air Fitting
01-080-5304
Structural Component Air Fitting
Matl:alum sh
01-080-5338
Aircraft Skin
Used on F-4. 11.500" overall length 9.000" overall width do not use cadmium plated tools on this item, titanium alloy 8mn per mil-t-9046 type 111 comp a annealed
