01-192-0844
Structural Component Air Support
Used on c-5b acft. lug assy-fairing service door, forward
01-192-0852
Structural Aircraft Panel
Used on c-5b aircraft. 6.380" overall length 5.880" overall width
01-192-0853
Structural Aircraft Panel
Used on c-5b acft. forward wheel well fairing
01-192-0854
Structural Aircraft Panel
Used on c-5b acft. forward wheel well fairing
01-192-1077
Air Wing Fairing Inflatable Seal
Used on acft model b-1b. matl: cordura fabric-nylon outer material with a thin rubber backing; nha: L3058064-101
01-192-1113
Structural Component Air Support
Used on acft model b-52. made from forged block 7075-T411 per bms-7-186; heat treated to T73; stock size 52.0 in. lg, 12.0 in. w, 5.0 in. thk; opposite p/n -528; nha 35-29992
01-192-1114
Structural Component Air Support
Used on acft model b-52. 2024-T4 al alloy per qq-a-355; 5.00 in. long, 3.00 in. wide, 0.032 in. thick; finish f-2.115; nha 25-2693
01-192-1115
Structural Component Air Support
Used on acft model b-1b. al alloy bar 7075-T73511 per qq-a-200/11; 7.750 in. lg, 0.672 in. w, 0.850 tappered to 0.350 in. thk; 2 0.2130 in. dia thru holes counterbored 0.516 in. dia to 0.220 in. thk remaining, 6.429 in. between holes; nha L354427-001
01-192-1116
Structural Component Air Support
Used on acft model kc-135. inconel 625 forging per AMS5666, annealed ultrasonic inspect per BAC5439, class a; finish f-4.10; opposite p/n -514; nha 458-52245; sta 1168
01-192-1117
Structural Component Air Support
Used on acft model kc-135. inconel 625 forging per AMS5666, annealed ultrasonic inspect per BAC5439, class a; finish f-4.10; opposite p/n -513; nha 458-52245; sta 1168
01-192-1118
Structural Component Air Support
Used on acft model kc-135. 7075-T73 alum die forging per BMS7-186, ultrasonic inspect billet or preformed stock per BAC5439, class a; opposite p/n -505; finish f-2.959 plus f-12.101 except use fed-std-595, color no. 37200; shot peen all over except holes per BAC5730; nha 458-52245; sta at 1168
01-192-1119
Structural Component Air Support
Used on acft model kc-135. 7075-T73 alum die forging per BMS7-186, ultrasonic inspect billet or preformed stock per BAC5439, class a; opposite p/n -506; finish f-2.959 plus f-12.101 except use fed-std-595, color no. 37200; shot peen all over except holes per BAC5730; nha 458-52245; sta at 1168
01-192-1130
Aircraft Former
9.000" overall length 7.000" overall width 2.250" material thickness eff on 61-0001-0261; spares only
01-192-1131
Former
Used on f-16a/b usaf aircraft. 10.000" overall length 4.250" overall width 0.500" material thickness
01-192-1132
Aircraft Former
37.800" overall length 4.600" overall width 0.071" material thickness
01-192-1133
Aircraft Former
4.890" overall length
01-192-1136
Aircraft Stringer
55.000" overall length
01-192-2279
Access Aircraft Door
Used on c-5a acft.
01-192-2373
Structural Aircraft Panel
Used on c-5b acft. floor assy-flight station
01-192-2374
Structural Aircraft Panel
Used on c-5b acft. flight station floor assy
01-192-2379
Aircraft Skin
Used on C-141.
01-192-2380
Aircraft Skin
Used on C-130.
01-192-2381
Aircraft Skin
Used on F-15.
01-192-2382
Aircraft Skin
Used on F-15.
01-192-2618
Aircraft Wing Assembly
01-192-2678
Structural Aircraft Panel
Used on c-5b aircraft. location upper lh side, f.s. 764.00 to f.s. 784.00; part of 4F11561-101a fillet fairing instl, fus sta 484.00 to 804.00; c/o: -107a spacer, size .032X1X15in; -109a spacer, size .032X1X5in; -115a spacer, size .032X5X19in; matl 7475-T61 al alloy plate per STM07-121; -113a skin, size .063X7X20in, matl 7475-T61 alclad (1 side) per STM07-118; nut (2)
01-192-2682
Aircraft Skin
Used on T-38. 60.000" overall length T3
01-192-2683
Aircraft Skin
Used on T-38. 60.000" overall length 38.000" overall width T3
01-192-2774
Bell Crank
0.750" bore diameter
01-192-3109
Structural Aircraft Panel
Panel consist of 22 parts; 11 ri vets; 1 cord assy; 1 flap assy; 6 strap assy; 1 blanket assy; 2stifferner text
01-192-3835
Structural Component Air Support
Used on acft model kc-135. consists of p/n 9-66383-1, angle, 1; p/n 9-66383-2, angle, 1; p/n 9-66383-3, plate, 1; p/n 9-66383-4, channel, 1; p/n 9-66383-5, radius filler, 1
01-192-4756
Access Aircraft Door
Used on trainer aircraft model ta-7c.
01-192-4757
Access Aircraft Door
Used on trainer aircraft model ta-7c.
01-192-4817
Fuselage Aircraft Fairing
Used on trainer aircraft model ta-7c. cognizant service:navy;
01-192-4822
Horizontal Stabilizer
Used on aircraft model e-2c. cognizant service:navy;
01-192-4945
Fluid Aircraft Manifold
01-192-5057
Structural Component Air Support
Used on acft model e-3a. consist of 1 plate, 1 pin, 1 setscrew; nha 69-66434
01-192-5390
Structural Component Air Support
Used on acft model b-52g/h. 2084-T4 extrusion per qq-a-267, T4-temper; alter bac 1514-968 by 3.20 in. long; finish f-2.30
01-192-5395
Wing Aircraft Spoiler
Used on aircraft,model b-52g/h. 5.000" overall length 4.000" overall width 0.051" material thickness bulkhead, rear spar 7075-0 clad strip per qq-a-287, 0-temper, heat treat T6; finish f-2.115; opposite p/n-4; nha 35-2686; used as spoiler rear spar bulkhead
01-192-5396
Wing Aircraft Spoiler
Used on aircraft,model b-52g/h. 23.000" overall length 3.500" overall width 0.051" material thickness 75s-0 clad per qq-a-287, 0-temper; heat treat T6; finish f-2.115; opposite p/n-2; nha 5-71862
01-192-5397
Wing Aircraft Spoiler
Used on aircraft,model b-52g/h. 23.000" overall length 3.500" overall width 0.051" material thickness 75s-0 clad per qq-a-287, 0-temper; heat treat T6; finish f-2.115; opposite p/n-2; nha 5-71862; used as spoiler intermediate rib
01-192-5398
Wing Aircraft Spoiler
Used on aircraft,model b-52g/h. 23.000" overall length 3.800" overall width 0.040" material thickness 75s-0 clad per qq-a-287, 0-temper; heat treat T6; f-2.115; opposite p/n-2; nha 35-2688, 35-2687, and 35-2684; used as spoiler intermediate rib
01-192-5407
Aircraft Former
43.200" overall length 4.700" overall width 0.071" material thickness
01-192-5408
Aircraft Former
5.210" overall length
01-192-5409
Aircraft Former
8.210" overall length
01-192-5410
Aircraft Former
8.680" overall length
01-192-5411
Aircraft Former
8.450" overall length
01-192-5414
Aircraft Skin
Used on F-111. 32.000" overall length 24.000" overall width
01-192-6882
Structural Aircraft Plate
Used on acft model kc-135. 8630 steel sheet per an-s-12
01-192-6884
Aircraft Fairing
Nuclear hardness critical item; opposite -001; nha L3058000
