01-160-5500
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
01-160-5501
Structural Component Air Support
Used on acft model c/kc-135. opposite p/n -502
01-160-5515
Aircraft Former
Opp -503; nha -502
01-160-5516
Aircraft Former
Nha -501; opp -504
01-160-5523
Aircraft Skin
Used on f-16 aircraft. stock size-.125 x 11 x 26"; material-qq-a-250/4-T62; finish-A430; location-fuel tank, upper, fs 234.3 to fs 243.0
01-160-5524
Aircraft Skin
Nha p/n 16B415-3; eff 5c 0001 9999
01-160-6453
Structural Aircraft Panel
Used on b-52 aircraft. 10.300" overall length 7.700" overall width
01-160-6454
Structural Aircraft Plate
Used on acft model b52. cres steel aisi 301 per mil-s-5059 comp d, annealed, surf cond 2d, 0.040 in.thk, 1.300 in.w, 14.000 in.lg, used on tail fairing, outboard strut
01-160-6455
Structural Aircraft Plate
Used on acft model b52. cres steel aisi 301 per mil-s-5059, comp d, annealed, surf cond 2d, 0.025 in.thk, 30.000 in.w, 35.000 in.lg, used on tail fairing, outboard strut
01-160-6456
Structural Aircraft Plate
Used on acft model b52. al clad 2024-0 per qq-a-250/5, 0.050 in.thk, 25.000 in.w, 29.000 in.lg, used on tail fairing. outboard strut
01-160-6457
Structural Aircraft Plate
32.000" overall length 29.000" overall width 0.050" material thickness
01-160-6458
Structural Aircraft Plate
Used on acft model b52. al clad 2024-0 per qq-a-250/5, 0.050 in.thk, 25.000 in.w, 29.000 in.lg, used on tail fairing, outboard strut
01-160-6467
Structural Aircraft Plate
Used on b-52 aircraft. rused 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-11.100 in. lg, 1.700 in. w, 0.020 in. thk
01-160-6468
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-12.000 in. lg, 9.500 in. w, 0.050 in. thk
01-160-6469
Aircraft Fairing
Reinforced epoxy honeycomb core
01-160-6470
Structural Component Air Support
Used on b-52 aircraft. used as support angle on tail fairing installation right hand inboard strut
01-160-6471
Structural Component Air Support
Used on b-52 aircraft. used as support angle on tail fairing installation right hand inboard strut
01-160-6472
Structural Component Air Support
Used on b-52 aircraft. used as support angle on tail fairing installation right hand inboard strut
01-160-6473
Structural Component Air Support
C/o 102 parts
01-160-6474
Structural Component Air Support
Used on acft model b52. opposite p/n 361-11308-506, used on rear spar
01-160-6475
Structural Component Air Support
Used on acft model b52. opposite of p/n 361-11308-505, used on rear spar
01-160-6484
Aircraft Floor
Used on B-52. 10.000" overall length 10.000" overall width
01-160-6487
Aircraft Skin
Used on b-52 aircraft. used on tail fairing installation right hand inboard strut; matl-clad 2024-0 qq-a-250/5; dimensions-35.000 in. lg, 14.000 in. w, 0.071 in. thk
01-160-6623
Rotary Rudder Boom
Used on uh-1 series helicopters. c/o:185 parts plus rivets, vinyl tape
01-160-6768
Aircraft Windshield Panel
01-160-7180
Structural Aircraft Panel
Used on c/kc-135 aircraft. consist of one filler strip; one splice strap; one honeycomb panel assembly; opposite p/n -521; nha 458-58024
01-160-7181
Structural Aircraft Panel
C/o 1 splice strip, 4 spacer, 1 bonded panel assy, 1 aft skin assy, 1 airscoop, 16 bolts
01-160-7182
Structural Aircraft Panel
Used on kc-135r aircraft. finish f-12.37 on all non-bonded surfaces after bonding; opposite p/n -503; nha 458-58031-502
01-160-7183
Structural Aircraft Panel
01-160-7184
Structural Aircraft Panel
C/o 1 splice strip, 1 aft skin assy, 1 bonded panel assy; opposite -502; nha 458-58024
01-160-7199
Structural Component Air Support
Used on c-130 acft.
01-160-7209
Structural Aircraft Plate
5.300" overall length 2.900" overall width 0.020" material thickness
01-160-7210
Structural Aircraft Plate
5.300" overall length 2.900" overall width 0.020" material thickness
01-160-7211
Structural Aircraft Plate
Used on B-52. make from BAC1513-57 x 3.000 in.
01-160-7212
Structural Aircraft Plate
Used on B-52. make from BAC1513-283 x 2.500 in.
01-160-7213
Structural Aircraft Plate
Used on B-52. make from BAC1513-283 x 2.500 in.
01-160-7214
Structural Aircraft Plate
5.100" overall length 4.900" overall width 0.100" material thickness 6al-4v
01-160-7215
Structural Aircraft Plate
5.100" overall length 4.900" overall width 0.100" material thickness 6al-4v
01-160-7219
Structural Component Air Support
C/o 1 diagonal brace, 2 bushing
01-160-7220
Structural Component Air Support
0.880" material thickness make from bac-1512-0362
01-160-7221
Structural Component Air Support
0.900" material thickness make from bac-1512-436
01-160-7224
Aircraft Former
11.400" overall length 4.500" overall width 0.080" material thickness
01-160-7225
Aircraft Former
13.400" overall length 4.500" overall width 0.080" material thickness
01-160-7226
Aircraft Former
13.400" overall length 4.500" overall width 0.080" material thickness
01-160-7227
Aircraft Former
13.400" overall length 4.500" overall width 0.080" material thickness
01-160-7228
Aircraft Former
11.400" overall length 2.900" overall width 0.063" material thickness
01-160-7229
Aircraft Former
1.500" overall length make from BAC1506-403
01-160-7230
Aircraft Former
1.500" overall length from BAC1506-403
01-160-7231
Aircraft Former
11.500" overall length 5.700" overall width 0.080" material thickness
01-160-7232
Aircraft Former
11.500" overall length 5.700" overall width 0.080" material thickness
