01-160-3119
Structural Component Air Support
01-160-3123
Structural Component Air Support
12.500" overall length 5.900" overall width 0.080" material thickness used as shear tie on mid spar outboard strut
01-160-3124
Structural Component Air Support
2.250" overall length 2.250" overall width 0.020" material thickness
01-160-3125
Structural Component Air Support
2.250" overall length 2.250" overall width 0.020" material thickness
01-160-3126
Structural Component Air Support
10.000" overall length 1.500" overall width 0.020" material thickness used on rib closure assembly, inboard strut
01-160-3127
Structural Component Air Support
10.000" overall length 1.500" overall width 0.020" material thickness
01-160-3128
Structural Component Air Fitting
41.000" overall length 4.000" overall width 4.000 " material thickness
01-160-3129
Structural Component Air Support
41.000" overall length 4.000" overall width 4.000" material thickness used on fitting assembly, front spar to wing attach link, inboard; matl 7079-T6
01-160-3130
Structural Component Air Support
Used on acft model b-52. aluminum alloy forging per 7079-f qq-a-367
01-160-3133
Structural Component Air Support
Used on acft model b-52. commercially pure titanium sheet ams 4900 annealed, 3.100 in. dia by 0.025 in, cup support
01-160-3134
Structural Component Air Support
Used on acft model c/kc-135. al tube 2024-T3 per ww-t-700/3, T3 temper; finish f-2.03; 1.625 in. o/d, 0.120 in. wall thk, 17.500 in. lg
01-160-3135
Structural Component Air Support
2.700" overall length 2.100" overall width 0.063" material thickness support-tube assembly
01-160-3136
Structural Component Air Support
Used on acft model c/kc-135. al die forging 7075-T73 per BMS7-186; finish f-2.20 plus desoto high temp primer; 8.370 in. lg; c/o 1 fitting, 1 spool, 4 washers, 1 nut
01-160-3137
Structural Component Air Support
Used on acft model c/kc-135. titanium 6al-4v forging per AMS4928, cond annealed; finish desoto high temp primer per BAC5710; 10.580 in. o/a lg, 6.910 in. w, 3.370 in. h; contains 2 bushings; opposite p/n -1
01-160-3138
Structural Component Air Support
Used on acft model c/kc-135. titanium 6al-4v forging per AMS4928, cond annealed; finish desoto high temp primer per BAC5710; 10.580 in. o/a lg, 6.910 in. w, 3.370 in. h; contains 2 bushings; opposite p/n -2
01-160-3139
Structural Component Air Support
Used on acft model c/kc-135. titanium 6al-4v forging per AMS4928, condition annealed; finish desoto high temp primer per BAC5710; 3.640 in. lg, 3.460 in. w, 3.620 in. h; opposite p/n -2; contains 2 bushings
01-160-3162
Aircraft Former
16.000" overall length 5.500" overall width 0.063" material thickness opp 39-14698-502
01-160-3163
Aircraft Former
15.400" overall length
01-160-3164
Aircraft Former
14.200" overall length
01-160-3165
Aircraft Former
14.900" overall length make from 10134-1205
01-160-3169
Aircraft Former
Used on acft model b-52. plastic, glass fabric reinforced per bac 5426 grade i
01-160-3175
Aircraft Skin
Used on B-52. 120.000" overall length 16.000" overall width
01-160-3176
Aircraft Skin
Used on B-52. 16.000" overall length 7.000" overall width
01-160-3177
Aircraft Skin
Used on B-52. 62.000" overall length 20.000" overall width
01-160-3178
Aircraft Skin
Used on B-52. 62.000" overall length 20.000" overall width opposite p/n 25-2304-13
01-160-3476
Supplemental Small Arms-fr Armor
Used on ah-64a aircraft.
01-160-3726
Aircraft Engine Build- Parts Kit
Used on CH-53.
01-160-3727
Aircraft Engine Build- Parts Kit
Used on CH-53.
01-160-3809
Aircraft Floor
Used on aircraft model p-3.
01-160-5409
Access Aircraft Door
Used on acft model f-16a. nha 16B1590-811; eff 61 0007 9999
01-160-5441
Structural Aircraft Panel
Used on c/kc-135 aircraft. 10.330" overall length 5.180" overall width aluminum alloy casting 356, heat treated to cond t-51; made from -2 casting; finish f-2.47; 2.360 in. dia outlet
01-160-5442
Structural Aircraft Panel
01-160-5443
Structural Aircraft Panel
01-160-5484
Structural Aircraft Panel
Used on F-16. replaces -805
01-160-5485
Structural Aircraft Panel
Used on F-16. replaces -806
01-160-5486
Structural Aircraft Panel
Used on b-52 aircraft. 10.000" overall length 7.700" overall width
01-160-5487
Structural Aircraft Plate
Used on f-16 aircraft. stock size-.050 x 6 x 8 in.; material spec-qq-a-250/4-T62; finish-A442
01-160-5488
Structural Aircraft Plate
Used on b-52 aircraft. used as bulkhead web on tail fairing installation right hand inboard strut; matl-clad 2024-0 qq-a-250/5; dimensions-30.000 in. lg, 25.000 in. w, 0.050 in. thk
01-160-5489
Structural Aircraft Plate
Used on b-52 aircraft. used as bulkhead web station 280.650 on tail fairing installation right hand inboard strut; matl-clad 2024-0 qq-a-250/5; dimensions-14.500 in. lg, 8.000 in. w, 0.063 in. thk
01-160-5490
Structural Aircraft Plate
Used on b-52 aircraft. used as doubler on tail fairing installation right hand inboard strut; matl-corrosion resistant steel sheet aisi 302 mil-s-5059 comp 302 annealed surface condition 2d; dimensions-12.000 in. lg, 1.700 in. w, 0.020 in. thk
01-160-5491
Structural Aircraft Plate
Used on b-52 aircraft. used as doubler on tail fairing installation right hand inboard strut; matl-clad 2024-0 qq-a-250/5; dimensions-12.300 in. lg, 9.000 in. w, 0.050 in. thk
01-160-5492
Structural Aircraft Plate
Used on b-52 aircraft. used as doubler on tail fairing installation right hand inboard strut; opposite p/n 25-2615-811
01-160-5493
Structural Component Air Support
Used on f-16 aircraft. material-aluminum alloy per qq-a-367, finish-A403; location-dorsal fairing, fs 357.670
01-160-5495
Structural Component Air Support
Used on acft model c/kc-135. al alloy die forging 7075-T73 per BMS7-186; finish f-2.20 plus desota hi temp primer per BAC5710; 11.180 in. lg, 2.000 in. w; c/o 1 fitting, 1 spool, 2 washers, 1 nut
01-160-5496
Structural Component Air Support
Used on acft model c/kc-135. corrosion resistant steel die forging 15-5ph per AMS5659; finish f-12.37 on all surfaces, plus f-12.100 (gray polytetrafluoroethylene) to hook end; 9.500 in. lg, 2.850 in. w, 0.830 in. thk, 19.450 in. radius; hook depth 0.610 in.
01-160-5497
Structural Component Air Support
Used on acft model c/kc-135. opposite p/n -501
01-160-5498
Structural Component Air Support
Used on acft model c/kc-135. al alloy 2024-T3 per qq-a-225/6; finish f-2.06; 2.910 in. o/a lg, 1.370 in. o/a dia, end pin:dia. 0.312 in., lg 1.100 in.
01-160-5499
Structural Component Air Support
Used on acft model c/kc-135. 15-5ph bar per AMS5659; heat treated to 150-170 ksi per BAC5619; finish f-1.108; 8.470 in. lg, 1.375 in. o/a dia; end threaded .4375-20 unjf, class 3b per mil-s-8879
