01-549-8660
Structural Aircraft Panel
Used on shroud instl-read cockpit instrument panel. 28.000" overall length 20.000" overall width panel, lh side opposite -94; dim are stock material
01-549-8717
Aircraft Stiffener
Used on rib instla rudder nose. 37.700" overall length 13.700" overall width 0.250" material thickness nose rib heat treat T4;
01-549-8758
Structural Component Air Support
Used on KC-135. chord alter BAC1506 - 1418 x 51.9
01-549-8767
Aircraft Bulkhead
01-549-8802
Aircraft Bulkhead
01-549-8874
Aircraft Fairing
Used on harrier ii aircraft.
01-549-8892
Structural Component Air Bracket
Used on ef-18 hornet aircraft. 2.680" overall length 0.880" overall width 0.050" material thickness
01-549-9083
Structural Component Air Support
01-549-9120
Aircraft Bulkhead
01-549-9159
Aircraft Bulkhead
01-549-9174
Structural Component Air Support
01-549-9188
Aircraft Beam
01-549-9190
Structural Aircraft Plate
01-549-9193
Structural Component Air Support
01-549-9196
Structural Component Air Support
Angle opposite -19; m/f: clad 2024 sht, 0-temp, ht T4; fin: f-2.10
01-549-9252
Structural Component Air Support
01-549-9623
Aircraft Stiffener
01-549-9640
Structural Component Air Support
01-549-9660
Structural Component Air Support
01-549-9671
Aircraft Fairing
Used on clip-fairing, lower rudder nose. 6.400" overall length 2.200" overall width 0.040" material thickness clip-fairing dim are stock material
01-549-9677
Aircraft Channel
Used on channel-nose rib rudder balance. 4.700" overall length 3.500" overall width 0.040" material thickness channel dim are stock material
01-549-9678
Structural Component Air Support
01-549-9690
Structural Component Air Support
01-549-9740
Structural Component Air Support
01-549-9848
Aircraft Stiffener
01-550-0088
Structural Component Air Bracket
Used on f-22 raptor. 3.750" overall length 2.260" overall width bracket dim. are stocksize matl; mf 5PTC4005-1-32 support
01-550-0092
Movable Canopy
Used on f-22 raptor. canopy
01-550-0130
Stiffener Aircraft Rib
01-550-0140
Structural Component Air Support
01-550-0184
Structural Component Air Support
01-550-0239
Structural Aircraft Plate
Used on shear plate-hinge elevator & rudder. 3.500" overall length 2.700" overall width 0.375" material thickness shear plate dim are stock material; matt: STA000=steel 8630
01-550-0280
Access Aircraft Door
Used on door installation access rudder hinge. door assembly dim are stock material; c/o door (2) , doubler (2) ; u/o kc-135; station: rudder sta 103.98
01-550-0284
Stiffener Aircraft Rib
Used on nose rib rudder balance, bay ii. 14.100" overall length 6.000" overall width 0.063" material thickness nose rib dim are stock material
01-550-0365
Aircraft Bulkhead
Used on KC-135. 2.200" overall length 1.900" overall width 0.032" material thickness bulkhead heat treat T4; 0 temp; srf 2.115
01-550-0407
Structural Component Air Support
01-550-0513
Aircraft Channel
01-550-0539
Aircraft Channel
01-550-0558
Aircraft Frame
Used on f-22 raptor. c/o 1 frame (5HW02108-116) ; 1 skin, inbd (5HWO2503-106) ; 1 skin, outbd; 2 angle; 7 bracket assy; 6 bracket; 1 support; ref loft; ref stds maching; ref insp eddy cur; ref; ref shimming; ref mach composite; 1 housing assy; 3 hinge assy; 2 stiffener; 2 clip; 7 plate
01-550-0572
Aircraft Frame
Used on f-22 raptor. box, assy c/o 1 housing, assy; 3 hinge; 2 stiffener; 1 frame; 1 skin, outbd; 2 angle; 8 bracket, assy; 2 clips; 7 plate; 1 support; 7 bracket; 1 support
01-550-0574
Structural Component Air Support
Used on angle, seal support elevator. 11.000" overall length 1.600" overall width 0.032" material thickness angle-support dim are stock material; u/o pn 3-58199
01-550-0580
Structural Component Aircraf Web
Used on intercostal installation-bomb door. 7.000" overall length 5.000" overall width 0.025" material thickness web dim are stock material; u/o pn 9-34089
01-550-0590
Structural Aircraft Plate
01-550-0600
Structural Component Air Bracket
01-550-0602
Structural Component Air Support
01-550-0604
Stiffener Aircraft Rib