01-593-8861
Structural Component Air Support
Used on c130 aircraft. brace installation - mian frame, fus sta .497-517, wl.175
01-593-9103
Structural Component Air Fitting
Used on KC-135. terminal fitting assy rear spar, stabilizer make from 5-87111-3; heat treat to 180.000 - 200.000 psi
01-593-9148
Structural Component Air Support
Used on c130b aircraft. brace instl mlg wheel well panel, fus sta 528.20 to 53700 wl 175.0 drawing indicates item is export controled.
01-593-9161
Structural Component Air Support
01-593-9167
Structural Component Air Support
Used on c130 aircraft. brace instl-mug wheel well panel, fus sta 557.0 to 557.4, WL175.0 contract number F33657-74-c-0226
01-593-9189
Structural Component Air Fitting
Used on kc-135 acft. terminal fitting assy-front spar stabilizer opposite -3004; make from p/n 5-86821-1; heat treat 180.000 - 200.000; finish f-1.30 except plating .000-.0005 thick
01-593-9193
Longeron
Longeron, web
01-593-9197
Longeron
Longeron
01-593-9199
Longeron
Longeron, web
01-593-9201
Structural Component Air Fitting
Used on 4-5203 kc-135. terminal fitting-rear spar, stabilizer opposite -8; make from 5-87111-3; heat treat 180.000 - 200.000 psi.
01-593-9236
Aircraft Former
9.000" overall length 4.000" overall width 0.100" material thickness gen cooling filler nozzle heat treat T82
01-593-9237
Aircraft Former
9.000" overall length 5.000" overall width 0.083" material thickness gen cooling nozzle doubler heat treat T82
01-593-9240
Structural Component Air Fitting
13.000" overall length 11.400" overall width 1.000 " material thickness
01-593-9246
Structural Component Air Fitting
13.000" overall length 11.400" overall width 1.000 " material thickness
01-593-9333
Aircraft Frame
01-593-9496
Structural Component Air Bracket
44.700" overall length tee heat treat T6; finish f-2.30; make from BAC1506-575
01-593-9501
Aircraft Stiffener
8.400" overall length angle make from AND10133-0701; heat treat T6; finish f-2.30
01-593-9507
Structural Component Air Bracket
44.800" overall length tee make alter BAC1506-575; heat treat T6; finish f-2.30
01-593-9512
Structural Component Air Bracket
45.000" overall length tee make from alter BAC1506-575; heat treat T6; finish f-2.30
01-593-9513
Aircraft Stringer
64.750" overall length stringer no. 2 -003 is opp the -004
01-593-9516
Structural Component Air Bracket
43.500" overall length tee make from alter BAC1506-974; heat treat T6; finish f-2.30
01-593-9537
Aircraft Stringer
64.000" overall length stringer no. 3 lwr
01-593-9703
Aircraft Stringer
64.880" overall length
01-593-9733
Stiffener Aircraft Rib
Rib, closeout inbd the -11 is opp -12
01-593-9745
Stiffener Aircraft Rib
Rib, closeout outbd
01-593-9996
Aircraft Door
01-594-0118
Fuel Aircraft Tank Assembly
Right side; main fuel tank
01-594-0283
Structural Aircraft Plate
Radius block u/o door 190 & 189; attach by bonding w/mil-s-8802 & riveting
01-594-0284
Structural Aircraft Plate
Radius block u/o door 190 & 189; attach w/mil-s-8802 & riveting
01-594-0286
Structural Component Air Bracket
Serrated stop
01-594-1330
Structural Aircraft Plate
Plate transition roller
01-594-1367
Structural Component Air Support
01-594-1368
Structural Component Air Support
01-594-1378
Structural Component Air Bracket
01-594-1386
Structural Component Air Support
01-594-1387
Structural Component Air Support
01-594-1514
Structural Aircraft Panel
01-594-1954
Aircraft Intercostal
Intercostal assy intercostal-stringer no. 1, assy of; -71 opp -72; nha L1804001
01-594-1974
Aircraft Door
Door, aircraft
01-594-1977
Aircraft Fairing
Synthetic spares fairing servo
01-594-1980
Access Aircraft Cover
Used on f-22 raptor.
01-594-2090
Aircraft Spar
64.250" overall length spar, front, flap no.1
01-594-2140
Structural Aircraft Plate
Splice, trailing edge splice, trailing edge, flap, wing panel
01-594-2179
Structural Aircraft Plate
Splice, trailing edge splice, trailing edge, flap, wing panel
01-594-2199
Structural Aircraft Plate
12.500" overall length 1.500" overall width 0.040" material thickness doubler -003 opp -004; doubler, qq-a-250/12 al bare sh alloy 7075-0
01-594-2226
Structural Aircraft Plate
8.800" overall length 7.450" overall width 0.063" material thickness doubler -009 opp -010; doubler, qq-a-250/12 al bare sh alloy 7075-0
01-594-2295
Structural Aircraft Panel
Used on retainer panel.
01-594-2373
Structural Aircraft Plate
64.990" overall length 4.200" overall width 0.063" material thickness splice splice, qq-a-250/12 al baresh alloy 7075-T73
01-594-2381
Air Wing Fairing Inflatable Seal
Used on seal nacelle fairing.
01-594-2395
Structural Component Air Bracket
2.500" overall length 2.250" overall width 0.063" material thickness clip -003 opp -004; qq-a-250/12 al bare sh aly 7075-0
