01-506-7275
Structural Aircraft Panel
Used on tristar acft. panel assy
01-506-7278
Structural Aircraft Panel
Used on tristar acft. panel assy
01-506-7280
Structural Aircraft Panel
Used on tristar acft. panel assy, lh
01-506-7283
Structural Aircraft Panel
Used on tristar acft. panel, upper rh
01-506-7285
Aircraft Fairing
Used on tristar acft. panel assy, lh
01-506-7289
Aircraft Intercostal
4.500" overall length 4.500" overall width 0.050" material thickness intercostal u/o e-3a; nha 204-70066; sonic environment detail part edges must meet the requirements of bac 5300 for structural parts; srf 2.30; -18 opp -19; dimsare stock material
01-506-7291
Aircraft Slat
Used on tristar acft. panel assy, lh
01-506-7302
Aircraft Intercostal
3.600" overall length 3.400" overall width 0.050" material thickness intercostal u/o e-3a; nha 204-70066; sonic environment detail part edges must meet requirements of bac 5300 for structural parts; srf 2.30; -21 opp -20; dims arestock material
01-506-7354
Bleed Air Duct Assembly
Used on tristar acft.
01-506-7358
Structural Aircraft Plate
Used on tristar acft. plate assembly
01-506-7405
Structural Component Air Bracket
Bracket assembly
01-506-7406
Structural Component Air Bracket
Bracket assembly
01-506-7469
Structural Aircraft Plate
Used on f-22 raptor. 31.000" overall length 15.000" overall width 3.000" material thickness louver, bypass forward i make from 5HP41501-113 louver
01-506-7470
Structural Aircraft Plate
Used on f-22 raptor. 31.000" overall length 15.000" overall width 3.000" material thickness louver, bypass forward i make from 1 5HP41501-114 louver
01-506-7657
Aircraft Frame
01-506-7866
Aircraft Wing Assembly
Used on C130.
01-506-7867
Aircraft Rudder
Used on c130j, mk4 and 5.
01-506-7870
Structural Aircraft Plate
Used on C130.
01-506-7979
Structural Component Air Bracket
7.150" overall length 3.390" overall width 0.125" material thickness bracket nha L3050015; u/o b-1b modification; ams 5518 cres sheet, alloy 301, cond 1/2 hard; protect per LA0116-020; finish per L0000024 code 60HA02
01-506-8040
Aircraft Door
Used on F/A-18. navydoor, landing gear
01-506-8044
Aircraft Door
01-506-8045
Access Aircraft Door
01-506-8046
Aircraft Door
01-506-8047
Access Aircraft Door
Used on 74a42500 cf18a. door, main landing gear assy of
01-506-8048
Aircraft Door
01-506-8188
Aircraft Fairing
01-506-8207
Structural Component Air Support
Angle, (lh only) ; side cowl panel, engine nacelle
01-506-8234
Structural Component Air Support
Fitting assembly, upper fuslage-b.l.6.50 sta 308.00-379.00
01-506-8334
Structural Component Air Support
Used on t-6a training aircraft. tailcone assembly
01-506-8578
Structural Component Air Support
Angle
01-506-8593
Structural Component Air Support
Angle
01-506-8630
Aircraft Tip
84.000" overall length 2.000" overall width 0.020" material thickness leading edge face sheet u/0 b-1b; dims are stock material; material is al clad sheet, heat treatr to t-62 per ST0111LA0009, finish 09 prior to bonding
01-506-9249
Trim Aircraft Tab
Used on tristar acft. seal tab, lh
01-506-9301
Aircraft Fairing
Used on tristar acft.
01-506-9307
Structural Aircraft Panel
Used on tristar acft. panel assy
01-506-9308
Structural Aircraft Panel
Used on tristar acft.
01-506-9309
Structural Aircraft Panel
Used on tristar acft. panel assy, rh
01-506-9311
Aircraft Leading Edge
Used on tristar acft.
01-506-9312
Structural Aircraft Panel
Used on tristar acft. panel assy
01-506-9313
Aircraft Latch Assembly
Used on tristar acft.
01-506-9338
Structural Component Air Bracket
Used on tristar acft.
01-506-9353
Structural Aircraft Plate
Used on f-22 raptor. 31.000" overall length 15.000" overall width louver-mid inlet bypass 3.000 plate
01-506-9358
Structural Aircraft Plate
Used on f-22 raptor. 31.000" overall length 15.000" overall width louver-mid inlet bypass
01-506-9378
Structural Component Air Bracket
Used on tristar acft.
01-506-9379
Structural Component Air Bracket
Used on tristar acft.
01-506-9460
Structural Component Air Support
Used on aircraft, ch-47. beam assembly, cargo tiedown adapter
01-506-9613
Structural Component Air Bracket
Used on aircraft, tomcat f-14. bay 1, W75, stowage bracket assembly
01-506-9663
Structural Component Air Support
5.250" overall length 4.440" overall width 2.750" material thickness support nha 68A324150; u/o f-15e CUM1-2; dims are stock material
01-506-9846
Structural Aircraft Plate
Used on f-22a raptor. 8.000" overall length 3.000" overall width 0.500" material thickness seal, assembly of wind swept surface critical item; dim. are stock material; c/o: -119 seal, LK204F3 nuts, & MS20426AD3-4 rivets; m/f: 2024-T851 alum plate
01-506-9852
Structural Aircraft Plate
Used on f-22a raptor. 8.000" overall length 3.000" overall width 0.500" material thickness seal wind swept surface critical item; m/f: 2024-T851 alum plate; c/o: -103 seal, nuts & rivets; dim. are stock material
