01-468-0110
Structural Aircraft Panel
01-468-0111
Structural Aircraft Panel
01-468-0112
Structural Aircraft Panel
01-468-0113
Structural Aircraft Panel
01-468-0114
Structural Aircraft Panel
01-468-0115
Structural Aircraft Panel
01-468-0238
Structural Component Air Fitting
Used on e-2c aircraft.
01-468-0248
Structural Component Air Support
Used on mh-53e aircraft.
01-468-0257
Structural Component Air Support
Used on mh-53e aircraft.
01-468-0264
Structural Component Air Support
Used on mh-53e aircraft.
01-468-0272
Structural Component Air Support
Used on mh-53e aircraft.
01-468-0363
Wing Rib
Used on f16 aircraft.
01-468-0418
Structural Component Air Support
122.690" overall length cap made from LS4252 extrusion, heat treat to T6 after forming; next higherassembly part numbers 356119, 356996, 388019, 370496, 356245, 375259, 3338374
01-468-0548
Aileron Rib
Used on f-16 aircraft.
01-468-0740
Structural Component Air Bracket
11.586" overall length 10.900" overall width 0.033" material thickness paint surface treated
01-468-0780
Structural Component Air Bracket
Used on ch-47d chinook helicopter. 11.600" overall length 2.800" overall width 0.040" material thickness
01-468-0811
Structural Component Air Support
1.000" overall length 2.500" overall width 0.160" material thickness
01-468-0846
Aircraft Channel
3.330" overall width 1.320" material thickness
01-468-0975
Structural Component Air Support
01-468-1095
Structural Component Air Fitting
90.250" overall length 16.800" overall width dim. are forgings
01-468-1143
Aircraft Pylon
01-468-1144
Aircraft Pylon
01-468-1469
Airfoil Rib
Used on aircraft. 27.750" overall length 8.250" overall width 3.810" material thickness opposite -002; nha L1702001; c/o 1 rib, 2 bearing; dimensions given in stock size; heat treat T852 per ST0170LB0045; finish 10AB02
01-468-1470
Structural Component Air Fitting
18.000" overall length 7.500" overall width 7.500 " material thickness 002 opposite; nha L1600001; heat treat T73 per ST0111LA0009; finish 10AB01; c/o 1 fitting, 1 bushing, 1 bearing; dimensions are stock size; matl per ST0170LB0043
01-468-1471
Structural Component Air Fitting
20.000" overall length 7.500" overall width 7.000 " material thickness opposite -022; nha L1600003; c/o 1 fitting, 1 bearing, 1 bushing; make from ST0170LB0043 al aly; dimensions givenin stock size; heat treat T73
01-468-1474
Door Aircraft Parts Kit
01-468-1475
Door Aircraft Parts Kit
01-468-1476
Structural Component Air Support
01-468-1477
Door Aircraft Parts Kit
01-468-1478
Door Aircraft Parts Kit
01-468-1526
Refueling Aircraft Probe
Used on fa 18 e/f. probe assembly, in flight refueling vibration driving is prohibited
01-468-1531
Aircraft Fairing
Fiaring-fixed, inflight refuel probe
01-468-1636
Aircraft Fairing
01-468-1646
Aircraft Floor
Used on c-17a aircraft.
01-468-1654
Aircraft Floor
Used on c-17a aircraft.
01-468-1839
Access Aircraft Door
01-468-1840
Aircraft Thrust Reverser Section
01-468-1841
Aircraft Thrust Reverser Section
01-468-2011
Aircraft Fairing
Used on c-17a aircraft.
01-468-2062
Aircraft Fairing
Used on ch-47 helicopter.
01-468-2095
Structural Component Air Support
3.000" overall length 5.000" overall width 0.063" material thickness matl:titanium sh, comml pure ti, type i, comp b, cond a; opp -004; u/o 1 & subq; u/a: support, seal land; dimensions listed are stock size
01-468-2098
Structural Component Air Support
6.000" overall length 5.000" overall width 0.063" material thickness matl: titanium sh, comml pure ti, type i, comp b, cond a; opp -020; u/o 1 & subq; u/a: support, seal land; dimensions listed are stock size
01-468-2099
Structural Component Air Support
6.000" overall length 5.000" overall width 0.063" material thickness matl:titanium sh, comml pure ti, type i, comp b, cond a: opp -019; u/o 1 & subq; u/a: support, seal land; dimensions listed are stock size
01-468-2100
Structural Component Air Support
6.250" overall length 5.000" overall width 0.063" material thickness matl:titanium sh, comml pure ti, type i, comp b, cond a; opp -024; u/o 1 & subq; u/a: support, seal land; dimensions listed are stock size
01-468-2101
Structural Component Air Support
6.250" overall length 5.000" overall width 0.063" material thickness matl:titanium sh, comml pure ti, type i, comp b, cond a; opp -023; u/o 1 & subq; u/a: support, seal land; dimensions listed are stock size
01-468-2102
Aircraft Fairing
Used on c-17a aircraft.
01-468-2682
Aircraft Fairing
Used on c-17a aircraft.
01-468-2713
Aircraft Fairing
Used on c-17a aircraft.
01-468-2728
Aircraft Fairing
Used on c-17a aircraft.
01-468-2737
Aircraft Fairing
Used on c-17a aircraft.
