01-196-2861
Aircraft Skin
Used on aircraft model av-8. aluminum alloy per qq-a-250/5, cond o, 0.100 in. thk
01-196-2948
Structural Aircraft Plate
Used on e-3a aircraft. stock BAC1512-3338X1.0; matl 2024-T4 per qq-a-200/3; finish f-2.30
01-196-2951
Structural Component Air Support
Used on e-3a aircraft. pan fitting assembly, main cargo door actuator support; c/o: fitting (1) , plug (1) , sleeve (2) , bushing (4) ; nha 65-25337
01-196-3438
Aircraft Latch Assembly
01-196-3736
Structural Component Air Support
Used on acft model f-111. material per 17-4 cres fms-0131, 9.000 in. lg, 2.750 in. w, 2.750 in. thk ftldgused on adapter, nose pivot-slat section to track, number 2 outboard
01-196-3737
Structural Component Air Support
Used on acft model f-111. material per 17-4 cres fms-0131, 7.000 in. lg, 2.500 in. w, 2.250 in. thk
01-196-3742
Aircraft Former
01-196-3961
Structural Component Air Support
1.250" overall length
01-196-4053
Vertical Stabilizer
Used on f-14 aircraft model. cognizant service:navy;
01-196-4159
Access Aircraft Cover
Used on b-1b aircraft. 0.256" hole diameter nuclear hardness critical item; mounting holes counterbored 0.415 in. dia by 0.126 in.; used as fuel tank access cover; nha L3010829; opposite p/n -012
01-196-4160
Access Aircraft Door
Used on acft model b-1b. consist of 1 door assy, 2 hinge, 1 hinge pin, 1 seal assy, misc hardware; located XFP247.524 to XFP308.114 wing outer panel access door
01-196-4161
Access Aircraft Door
Used on acft model b-1b.
01-196-4162
Access Aircraft Door
Used on acft model b-1b.
01-196-4163
Access Aircraft Door
Used on acft model b-1b. nha L3010060-101; located zf 34.0; used on forward fuselage wheel well closure
01-196-4329
Aircraft Door
Nha L3010050-101
01-196-4363
Structural Aircraft Plate
Al alloy sh, qq-a-250/4, T3, csk on one side, 0.062 in.thk
01-196-4364
Structural Aircraft Plate
7.500" overall length 1.400" overall width 0.090" material thickness
01-196-4365
Structural Aircraft Plate
1.622" overall length 0.880" overall width 0.080" material thickness
01-196-4366
Aircraft Fairing
2nd matl epoxy resin; finish r-77 type iii per DS30000
01-196-4373
Structural Component Air Support
Opposite -022; nha L1800000
01-196-4374
Structural Component Air Bracket
7.100" overall length 5.000" overall width 0.040" material thickness nha 65-2516
01-196-4376
Structural Component Air Support
Used on acft model f-111. aluminum alloy per qq-a-200/3
01-196-4377
Structural Component Air Support
Used on acft model f-111. aluminum alloy per qq-a-200/3
01-196-4378
Structural Component Air Support
Used on acft model f-111. aluminum alloy per qq-a-200/3
01-196-4380
Structural Component Air Support
Used on acft model f-111. aluminum alloy per qq-a-200/3
01-196-4381
Structural Component Air Bracket
01-196-4395
Structural Aircraft Panel
01-196-4396
Structural Aircraft Panel
Used on c-5b aircraft.
01-196-4397
Structural Aircraft Panel
Preimpregnated glass fabric per STM22-401 form ii, class 1
01-196-4398
Structural Aircraft Panel
Preimpregnated glass fabric per STM22-401 form ii, class 1
01-196-4399
Structural Aircraft Panel
Used on acft model c-5b. preimpregnated glass fabric per STM22-401, form ii, class 1
01-196-4400
Structural Aircraft Panel
Preimpregnated glass fabric per STM22-401 form ii, class 1
01-196-4401
Structural Aircraft Panel
Used on acft model c-5b. preimpregnated glass fabric STM22-401 form ii, class 1
01-196-4402
Structural Aircraft Panel
Used on acft model c-5b. preimpregnated glass fabric per STM22-401 form ii, class 1
01-196-4403
Structural Aircraft Panel
Used on acft model c-5b. preimpregnated glass fabric per STM22-401 form ii, class 1
01-196-4405
Structural Aircraft Panel
Preimpregnated glass fabric per STM22-401 form ii, class 1
01-196-4406
Structural Aircraft Panel
Used on c-5b aircraft. panel assy-closure, fillet fairing, f.s. 764.000 to f.s. 804.000; opposite -114a; c/o: spacer (5) , nut (1) , skin (1) ; matl 7475-T61 alclad
01-196-4407
Structural Aircraft Panel
Used on c-5b aircraft. panel assy-closure, fillet fairing, f.s. 764.000 to f.s. 804.000; opposite -113a; c/o: spacer (5) , nut (1) , skin (1) ; matl 7475-T61 alclad
01-196-4408
Structural Aircraft Panel
Used on c-5b aircraft.
01-196-4410
Structural Aircraft Panel
Used on c-5b aircraft. panel assy-close-out, fillet fairing; nha 4F11561; c/o: -107a spacer (2) , -111a spacer (1) , -119a skin (1) ; matl 7475-T61 alclad
01-196-4412
Structural Aircraft Panel
Used on c-5b aircraft. NHA4F75002, eff on 0082 & up; opposite p/n 4F72633-108a; high temperature, polyurethane 6 to 8 lbs cubic foot
01-196-4413
Structural Aircraft Panel
Used on c-5b aircraft. panel assy-upper fwd mlg fairing, fus sta 1084.000 to 1128.000; nha 4F75002, eff on 0082 & up; opposite -107a; matl - preimpregnated glass fabric per STM22-401 form ii class 1 using mil-c-9084 type viiib fabric; foam, high temp, polyurethane 6 to 8 lbs cubic foot
01-196-4414
Structural Aircraft Panel
M/f: preimpregnated glass fabric per STM22-4cl form i class 1 using mil-c-9084 type viii b fabric
01-196-4415
Structural Aircraft Panel
Used on c-5b aircraft. panel assy-lower fwd mlg fairing, fus sta 1084.000 to 1128.000; nha 4F75003, eff on 0082 & up; opposite -107a; matl - preimpregnated glass fabric per STM22-401 form ii class 1 using mil-c-9084 type viii b fabric; foam high temp. polyurethane 6-8lbs max per cubic foot
01-196-4416
Structural Aircraft Panel
Used on c-5b aircraft. 4opposite p/n 4F75877-102d; nha 4F75001, eff on 0082 & up; consist of two zee assemblies; one panel; two stiffeners; two beams; two zees; two retainers; four angles; one tee; one support; one clip; one fitting; twenty-one pins; twenty-one collars
01-196-4417
Structural Aircraft Panel
Used on acft model kc-135. consist of 1 panel, 1 channel, 15 nutplates; nha 458-58297
01-196-4423
Aircraft Former
12.000" overall length
01-196-4424
Aircraft Former
5.600" overall length 2.100" overall width 0.080" material thickness
01-196-4425
Aircraft Former
5.600" overall length 1.600" overall width 0.080" material thickness
01-196-6023
Fuel Tank Aircraft Baffle
