01-193-6749
Aircraft Channel
Used on H-50B. 2.380" overall length thru hole 0.203 inch diameter centered along length
01-193-7333
Structural Aircraft Panel
Used on acft model kc-135. vphosphoric acid anodize per BAC5555 all surfaces except core; prime with BMS5-104 type i class i per BAC5514; finish f-12.37; opposite p/n -7; consists of 1 skin outer, 4 light core, 1 dense core, 6 doubler, 1 skin inner, 4 zee members
01-193-7381
Thermal Insulation Pipe Covering
Acft c-130
01-193-8094
Structural Component Air Support
Used on acft model a-10a. made from forging 160612608f
01-193-8676
Access Aircraft Door
Used on f-16c/d usaf aircraft. edoor assy, access-7th stage connector
01-193-8677
Access Aircraft Door
Used on acft model b-1b. nuclear hardness critical item; opposite p/n -072; located yn 200.600-216.500; nha L3206635-102; used as lower nacelle hydraulic access door
01-193-8798
Structural Aircraft Plate
4.000" overall length 3.000" overall width 0.040" material thickness extension, heat shield
01-193-8799
Structural Aircraft Plate
Used on f-16c/d usaf aircraft. stock size-.020X5X15; material-commercially pure titanium per mil-t-9046, type i, comp b, cond a; part of--805 shield installation; nha-16B6312-805; eff on-5c 0008 0090, 0092 0092, 0118 0118, 0120 0120, 0122 0122, 0124 0124, 0128 0128
01-193-8800
Structural Aircraft Plate
4.000" overall length 3.000" overall width 0.040" material thickness extension, heat shield
01-193-8801
Structural Aircraft Plate
4.000" overall length 2.000" overall width 0.040" material thickness nha 16B6312-805; eff on 5c 0008 0090, 0092 0092, 0118 0118, 0120 0120, 0122 0122, 0124 0124, 0128 0128
01-193-8802
Structural Aircraft Plate
4.000" overall length extension, internal heat shield
01-193-8817
Structural Component Air Fitting
4.000" overall length 3.000" overall width
01-193-8819
Aircraft Wing Assembly
01-193-8840
Aircraft Bulkhead
01-193-8841
Structural Aircraft Plate
Used on f-4 aircraft. stock size..090X1.84x.6; material-2024-T3 al aly per qq-a-250/4, cond T3; part of -1 sill assy, door, access, fixed, inboard, leading edge
01-193-8842
Aircraft Fairing
11.760" overall length 4.180" overall width
01-193-8843
Aircraft Fairing
11.760" overall length 4.180" overall width
01-193-8844
Aircraft Fairing
01-193-8845
Aircraft Fairing
10.750" overall length 10.000" material thickness
01-193-8846
Aircraft Fairing
9.900" overall length 1.960" overall width 1.300" material thickness
01-193-8849
Structural Component Air Support
Used on f-16a belgium aircraft. c/o 5 ea. support
01-193-8850
Structural Component Air Support
Used on f-16c/d usaf aircraft. stock size-1.25X2X3; material-T1-6al-4v alloy per mil-t-9047, comp 6, cond a; finish-T450; location-engine track, rem, fs 446-479; nha-16B6312-807; 5c 0178 0178, 0180, 0182, 0188, 0190, 0192, 0194
01-193-8851
Structural Component Air Support
Used on f-16c/d usaf aircraft. stock size-1.25X2X4; material-T1-6al-4v alloy per mil-t-9047, comp 6, cond a; finish-T450; nha-16B6312-807; eff on-5c 0178 0178, 0180, 0182, 0188, 0190, 0192, 0194; location-engine track, rem, fs 446-479
01-193-8852
Structural Component Air Support
Used on f-16c/d usaf aircraft. stock size-1.50X2X3; material-T1-6al-4v alloy per mil-t-9047, comp 6, cond a; finish-T450; location-engine track, rem, fs 446-479; nha-16B6312-807; eff on-5c 0178 0178, 0180, 0182, 0188, 0190, 0192, 0194
01-193-8853
Structural Component Air Support
Used on f-16c/d usaf aircraft. stock size-1.25X2X3; material-T1-6al-4v alloy per mil-t-9047, comp 6, cond a; finish-T450; location-engine track-rem, fs 446-479; nha-16B6312-807; eff on-5c 0178 0178, 0180, 0182, 0188, 0190, 0192, 0194
01-193-8854
Structural Component Air Support
Used on f-16c/d usaf aircraft. stock size-1.25X2X3; material-T1-6al-4v alloy per mil-t-9047, comp 6, cond a; finish-T450; location-engine track-rem, fs 446-479; nha-16B6312-807; eff on-5c 0178 0178, 0180, 0182, 0188, 0190, 0192, 0194
01-193-8858
Structural Aircraft Panel
Used on acft model b-52. c/o 1 cover, 1 panel, 1 orifice plate, 1 adapter assy, 1 nutplate, screw
01-193-8864
Aircraft Skin
19.000" overall length 10.000" overall width finish A442; nha -16B6318-3; 5c 0170179, 0180, 0182, 0188, 0190, 0192, 0194
01-194-0862
Structural Component Air Support
3.685" overall length 0.520" overall width 0.125" material thickness
01-194-0958
Fuel Aircraft Tank
Rubber; 47.740 in.nom o/a lg; 36.120 in.nom o/a h; 44.740 in.nom o/a w
01-194-0959
Fuel Aircraft Tank
Rubber; 47.740 in.nom o/a lg; 36.120 in.nom o/a h; 44.740 in.nom o/a w
01-194-1127
Aircraft Windshield Panel
01-194-1257
Exhaust Muffler
01-194-2386
Structural Component Air Fitting
3.750" overall length 3.000" overall width 1.500 " material thickness
01-194-2399
Structural Component Air Support
Used on acft model a-10a. alternate for -7
01-194-2400
Structural Component Air Support
Used on acft model a-10a.
01-194-2407
Aircraft Former
8.300" overall length
01-194-2492
Aircraft Floor
Used on helicopter model sh-60b.
01-194-2493
Aircraft Floor
Used on helicopter model sh-60b. essential to weapon system performance or operation, or the preservation of life or safety of operating personnel
01-194-2494
Aircraft Floor
Used on helicopter model sh-60b.
01-194-2685
Supplemental Small Arms-fr Armor
Used on ah-1 , rotary wing aircraft.
01-194-2688
Supplemental Small Arms-fr Armor
Used on ah-1 , rotary wing aircraft.
01-194-3136
Structural Aircraft Panel
Consist of two doublers; one channel p/n 12W10204-17
01-194-3137
Structural Aircraft Panel
Consist of two doublers; one channel, p/n 123W10204-18
01-194-3741
Stiffener Aircraft Rib
4.100" overall length 2.600" overall width 0.063" material thickness
01-194-3742
Stiffener Aircraft Rib
4.100" overall length 2.600" overall width 0.063" material thickness
01-194-3807
Aircraft Fairing
Nuclear hardness critical item; opposite -002; nha L3058000
01-194-4358
Structural Component Air Support
Used on c-5b acft.
