01-160-7233
Aircraft Former
11.500" overall length 5.700" overall width 0.080" material thickness
01-160-7234
Aircraft Former
11.500" overall length 5.700" overall width 0.080" material thickness
01-160-7235
Aircraft Former
7.400" overall length 4.200" overall width 0.080" material thickness
01-160-7236
Aircraft Former
7.400" overall length 4.200" overall width 0.080" material thickness
01-160-7240
Aircraft Skin
Used on acft model kc-135r. fc/o 1 aft skin, 1 rub strip; al alloy 2024-T31 per qq-a-250/4; finish f-2.03; 10.900 in. lg, 5.100 in. w, 0.063 in. thk; rub strip-nylatron gs-hs; opposite assembly -5; nha 458-58031-2 or 458-58031-502
01-160-7241
Aircraft Skin
Used on acft model c/kc-135r. gc/o 1 aft skin, 1 rub strip; al alloy 2024-T31 per qq-a-250/4; finish f-2.03; 10.900 in. lg, 5.100 in. w, 0.063 in. thk; rub strip-nylatron gs-hs; opposite assembly -6; nha 458-58031-1
01-160-9053
Aircraft Skin
01-160-9247
Structural Aircraft Plate
Used on A-10. 20.600" overall length 2.700" overall width 1.300" material thickness ballistic foam thermarest AX5052
01-160-9248
Structural Aircraft Plate
01-160-9250
Structural Aircraft Plate
Used on A-10. 9.800" overall length 2.100" overall width 1.800" material thickness ballistic foam thermarest AX5052
01-160-9251
Structural Aircraft Plate
Used on A-10. 7.100" overall length 1.800" overall width 1.400" material thickness ballistic foam thermarest AX5052
01-160-9252
Structural Aircraft Plate
Used on A-10. 9.700" overall length 2.200" overall width 1.500" material thickness void filler ballistic foam thermarest AX5052
01-160-9256
Structural Aircraft Plate
Used on A-10. 10.200" overall length 3.600" overall width 3.200" material thickness ballistic foam thermarest AX5052
01-160-9280
Structural Aircraft Panel
Used on b-1b aircraft. nuclear hardness critical item
01-160-9281
Structural Aircraft Panel
Used on b-1b aircraft. consist of three honeycomb cores; two skin
01-160-9282
Structural Aircraft Panel
Used on b-1b aircraft. nuclear hardness critical
01-160-9283
Structural Aircraft Panel
Used on b-1b aircraft. consist of three honeycomb cores
01-160-9284
Structural Aircraft Panel
Used on b-1b aircraft. nuclear hardness critical item; consist of one core, p/n L3053744-004; one skin outer, p/n L3053744-006; one glass fabric, p/n L3053744-008; one glass fabric, p/n L3053744-010
01-160-9285
Structural Aircraft Panel
Used on b-1b aircraft. consist of three core
01-160-9286
Structural Aircraft Panel
Used on b-1b aircraft. consist of three skins; two cores; two fillers
01-160-9287
Structural Aircraft Panel
Used on b-1b aircraft. consist of three cores; three skins
01-160-9288
Structural Aircraft Panel
Used on acft model b-1b. nuclear hardness critical item, located from YF1214.500 to YF1240.169, left hand;
01-160-9290
Structural Aircraft Plate
Used on b-52 acft. matl cres st, 17-7ph cond a; matl size 0.063 by 3.000 by 11.000 in. lg; opposite to p/n 25-2365-29; used as angle on frame installation, nose cowl
01-160-9291
Structural Aircraft Plate
01-160-9292
Structural Aircraft Plate
6.500" overall length 3.800" overall width 0.050" material thickness
01-160-9294
Structural Aircraft Plate
Used on acft model kc-135r. al alloy clad sheet 2024-0 per qq-a-250/5; heat treated to cond T42; finish f-2.03; 2.500 in. lg, 2.000 in. w, 0.100 in thk; nha 458-58077-4; located nacelle sta. 224.465
01-160-9295
Structural Aircraft Plate
4.000" overall length 4.000" overall width 0.050" material thickness is attached to engine mount for support
01-160-9297
Aircraft Fairing
4.000" overall length 3.000" overall width 0.032" material thickness function-lower surface drain
01-160-9301
Structural Component Air Support
Used on f-4e aircraft; aircraft, phantom f-4. used as bellcrank support fitting, outer wing repair installation; componensts-fitting 1, spacer 1, plate 1, shim 2, bearing 2
01-160-9302
Structural Component Air Support
Used on f-4e aircraft. used as bellcrank support fitting, outer wing repair installation; components-fitting 1, spacer 1, plate 1, shim 2, bearing 2;
01-160-9303
Structural Component Air Support
Used on b-52 acft. used as fitting on stabilizer access door, elevator balance
01-160-9304
Structural Component Air Support
Used on b-52 acft. used as fitting on stabilizer access door, elevator balance; opposite to p/n 35-27721-1
01-160-9305
Structural Component Air Support
Used on b-52 acft. matl al alloy, qq-a-287, 7075-0 clad; matl size 0.071 by 4.000 by 4.000 in. lg; opposite to p/n 25-2365-19; used as bracket on frame installation nose cowl
01-160-9306
Structural Component Air Support
Used on b-52 acft. matl al alloy, qq-a-287, 7075-0 clad; matl size 0.071 by 3.000 by 3.500 in. lg; opposite to p/n 25-2365-807; used as gusset on frame installation on cowl nose fuselage sta 93.93
01-160-9308
Structural Component Air Support
Used on b-52 acft. matl cres st, 17-7ph cond a; matl size 0.063 by 3.000 by 11.000 in. lg; opposite to p/n 25-2365-30; used as angle on frame installation, nose cowl
01-160-9309
Structural Component Air Support
Used on b-52 acft. c/o plenum; seal, cooling air; orifice plat latch; retainer; screws 8 places; used as plenum assy kit
01-160-9310
Structural Component Air Support
Used on acft model kc-135r. al plate 2024-T351 per qq-a-250/4; finish f-2.16; 3.750 in. lg, 3.080 in. w, 0.620 in. thk; c/o 1 fitting, 1 bushing; nha 458-58042
01-160-9311
Structural Component Air Support
Used on acft model kc-135r.
01-160-9312
Structural Component Air Support
Used on acft model kc-135r. located nacelle sta 206.00
01-160-9313
Structural Component Air Support
Used on acft model kc-135r. al sheet 2024-T3 per qq-a-250/4; finish f-2.16; 2.620 in. lg, 2.570 in. w, 0.190 in. thk; c/o 1 fitting, 1 bushing; nha 458-58328
01-160-9314
Structural Component Air Support
Used on acft model kc-135r. al alloy 2024-T351 per qq-a-225/6; finish f-2.03; 1.860 in. lg, 1.260 in. w, 1.255 in. h; c/o 1 fitting, 1 bearing; nha 458-58066
01-160-9317
Structural Component Air Support
Used on acft model b-1b. c/o bearing 2 ea p/n MS27649-5, support 1 ea p/n L5234075-008, used on aft sector-wing pivot spoiler control
01-160-9318
Structural Component Air Support
Used on acft model b-1b. used on radome hinge, nose radome, left hand
01-160-9319
Structural Component Air Support
Used on acft model b-1b. used on radome hinge, nose radome, right hand
01-160-9320
Structural Component Air Support
Used on acft model b-1b. c/o support 1 ea p/n L3010262-003, bearing 1 ea p/n MS14101-4, 1.760 in.w, 2.190 in.h, 2.945 in.lg, used on center link, radome hinge
01-160-9321
Structural Component Air Support
Used on acft model b-1b. c/o 16 ea component parts, used on nose radome
01-160-9322
Structural Component Air Support
Used on acft model kc-135r. al alloy clad sheet 2024-0 per qq-a-250/5; heat treated to cond T42; finish f-2.03; 6.300 in. lg, 3.800 in. w, 0.080 in. thk; located nacelle sta. 224.465; opposite p/n -7; nha 458-58077-4
01-160-9328
Aircraft Former
Used on acft model f-16c usaf. stock size-30"; material specs-K14A19T8511; finish-A710; superseded 16B4450-16 ow per ecn 2E893; eff on 5c-0001-9999; nha 16B4701-5
01-160-9330
Aircraft Former
0.080" material thickness nha -58025, -028, -029, -031, -048
