01-394-4082
Aircraft Intercostal
Used on f/a-18 and cf-18 airplane.
01-394-4086
Aircraft Skin
Used on f/a-18, hornet aircraft.
01-394-4087
Aircraft Skin
Used on f/a-18, hornet aircraft.
01-394-4088
Aircraft Skin
Used on f/a-18, hornet aircraft.
01-394-4089
Aircraft Skin
Used on f/a-18, hornet aircraft.
01-394-4090
Aircraft Intercostal
Used on f/a-18 and cf-18 airplane. 0.050" material thickness
01-394-4091
Aircraft Intercostal
Used on f/a-18 and cf-18 airplane. 0.050" material thickness nha; p/n 74A170002
01-394-4092
Aircraft Intercostal
Used on f/a-18 cf-18 airplane. 0.050" material thickness nha; 74A170002
01-394-4096
Aircraft Skin
01-394-4107
Structural Component Air Support
5.555" overall length 0.025" overall width
01-394-4334
Structural Component Air Fitting
22.800" overall length tension tube assembly
01-394-4335
Aircraft Stiffener
Make from -1 forging
01-394-4832
Structural Component Air Fitting
01-394-5232
Aircraft Stiffener
Finish f-2.30
01-394-5233
Structural Component Air Support
27.400" overall length opposite -2; finish srf-2.30
01-394-5234
Structural Component Air Support
27.400" overall length opp -1; finish srf-2.30
01-394-5235
Structural Component Air Bracket
3.700" overall length 3.700" overall width 0.072" material thickness u/a stiffener tie angle; opp -7
01-394-5236
Structural Component Air Fitting
6.700" overall length 2.500" overall width 0.800 " material thickness make from -1 forging; per adcn W2:matl 7075-T73511 extr; u/a:stiffener tie fitting
01-394-5237
Aircraft Stiffener
3.900" overall length 3.500" overall width 0.072" material thickness finish f-2.113; heat treat T6; nha 5-87827
01-394-5238
Aircraft Beam
141.000" material thickness u/a:keel beam chord; opp -8 exceptas noted on dwg; matt:alter bac 1520-708; temp T6
01-394-5239
Aircraft Beam
141.000" material thickness u/a:keel beam chord; opp -7 exceptas noted on dwg; matt:alter BAC1520-708; temp T6
01-394-5240
Aircraft Beam
141.000" material thickness u/a:keel beam chord; opp -1; matt:alter bac 1520-708; temp T6
01-394-5247
Aircraft Beam
242.000" overall length alter BAC1518-196; finish f-2.30
01-394-5295
Aircraft Skin
Used on f/a-18, hornet aircraft.
01-394-5296
Aircraft Skin
Used on f/a-18, hornet aircraft.
01-394-5297
Aircraft Skin
Used on f/a-18, hornet aircraft.
01-394-5301
Aircraft Skin
Used on f/a-18, hornet aircraft.
01-394-5696
Structural Aircraft Panel
Used on c-130, hercules aircraft. 1.125" overall length lacquer surface treated
01-394-5699
Structural Aircraft Panel
Used on c-130, hercules aircraft. 2.625" overall length 1.500" overall width lacquer surface treated
01-394-5711
Structural Component Air Support
Used on ch-53 helicopter. 0.042" material thickness strut bracket inst, nha; p/n 65217-02031
01-394-5887
Aircraft Beam
Dwg note:make from bac 1506-869; heat treat:T6; temper 0
01-394-5948
Structural Aircraft Panel
Used on hh-60h (active) and hh-60j(reserve) configurations. hcs/mrr window surround instl
01-394-5952
Structural Aircraft Plate
Used on aircraft model f/a-18 non-hsp (hornet support plan) support.
01-394-5958
Aircraft Fairing
Used on acft model f-14a. fairing assembly-missile, FS568.375-FS601.40
01-394-6265
Structural Aircraft Plate
Used on f-16 airplane.. 3.120" overall length 0.800" overall width 0.125" material thickness matt; ams-5520, stock size; 0.125 x 2 x 3 in. nha; p/n 16B1886.
01-394-6281
Structural Aircraft Panel
Used on c-130, hercules aircraft.
01-394-6282
Structural Aircraft Panel
Used on c-130, hercules aircraft.
01-394-6284
Structural Aircraft Plate
Used on c-130, hercules aircraft. 5.730" overall length 1.115" overall width 0.063" material thickness paint surface treated
01-394-6285
Structural Aircraft Plate
Used on c-130, hercules aircraft. 0.030" material thickness bend 3.180 in. from edge 0.160 r
01-394-6286
Structural Aircraft Plate
Used on c-130, hercules aircraft. 0.030" material thickness
01-394-6319
Structural Component Air Bracket
01-394-6320
Structural Component Air Bracket
01-394-6998
Structural Aircraft Panel
Used on c-130,hercules aircraft. 56.880" overall length 25.880" overall width
01-394-7065
Structural Component Air Fitting
Opp -4; make from -3 forging; matl:4330 modified steel
