01-505-9142
Structural Component Air Support
13.000" overall length 5.000" overall width 4.000" material thickness filler foam next higher assy, 68A324905, u/o f-15e cum 1
01-505-9143
Structural Component Air Support
13.000" overall length 5.000" overall width 4.000" material thickness block next higher assy, 68A324905, u/o f-15e cum 1
01-505-9144
Structural Component Air Support
7.300" overall length 5.250" overall width 1.500" material thickness filler foam foam matl shall be polymide foam ac-406; dim are stock matl
01-505-9305
Rudder Balance Weight
01-505-9502
Aircraft Fairing
Used on aircraft, f-18 hornet.
01-505-9540
Fuel Tank Aircraft Baffle
Used on valve assembly, pressure fuel andtransfer; seasprite, aircraft.
01-505-9564
Structural Component Air Support
Used on h-60 aircraft. support aircraft support structure
01-505-9565
Aircraft Frame
Used on h-60 aircraft. frame aircraft support structure
01-505-9566
Structural Aircraft Panel
Used on h-60 aircraft. closure assembly instrument panel item
01-505-9848
Structural Component Air Support
12.000" overall length 2.650" overall width 1.000" material thickness liner NHA68A321011; u/o f-15a CUM1-97, f-15b CUM1-15, F15a SGT1; dims are stockmaterial
01-505-9849
Structural Component Air Support
8.000" overall length 0.750" overall width 0.500" material thickness liner nha 68A321070; u/o f-15a CUM1-365, f-15b CUM1-59, FMF15a CUM1&up, FMTF15a CUM1&up, f-15a SGT1; dims are stock material
01-505-9850
Structural Component Air Support
4.000" overall length 2.550" overall width 0.500" material thickness liner nha 68A321070; u/o f-15a CUM1-365, f-15b CUM1-59, FMF15a CUM1&up, FMTF15a CUM1&up, f-15a SGT1; dims are stock material
01-505-9863
Access Aircraft Door
Used on f/a-18e/f acft. (navy) door, access, aircr
01-505-9864
Access Aircraft Door
Used on door installation;f/a-18e/f support of ecp 6038. (navy) door, access, aircr
01-505-9865
Access Aircraft Door
Used on f/a-18e/f acft. (navy) door, access, aircr
01-505-9866
Access Aircraft Door
Used on f/a-18e/f support of ecp 6038. (navy) door, access, aircr
01-505-9869
Aircraft Fairing
Used on f/a-18e/f support of ecp 6038. fairing, aircraft, ai
01-505-9870
Structural Component Air Support
Used on f/a-18 e/f aircraft. (navy) rib, aircraft - hinge/drive, inbd, aileron
01-505-9873
Aircraft Hinge
01-505-9874
Access Aircraft Door
Used on f/a-18e/f support of ecp 6038. (navy) door, access, aircr
01-505-9875
Access Aircraft Door
Used on f/a-18e/f support of ecp 6038. (navy) door, access, aircr
01-505-9876
Access Aircraft Door
Used on f/a-18e/f support of ecp 6038. (navy) door, access, aircr
01-505-9883
Aircraft Hinge
01-505-9887
Aircraft Hinge
01-505-9888
Aircraft Hinge
01-505-9889
Structural Component Air Support
Used on f/a-18 e/f aircraft. (navy) rib, aircraft - hinge/drive, inbd, aileron
01-505-9914
Access Aircraft Cover
Used on suu-78a/a pylon, 74a736001-1007;f/a-18e/f support of ecp 6038. (navy) cover, access, airc
01-505-9929
Access Aircraft Cover
Used on ancillary equip;f/a-18e/f support of ecp 6038. (navy) cover, access-ALE5
01-506-0349
Aircraft Fairing
Used on f/a-22 raptor. forward chine assembly consists of (1) 5HU05020-101 skin
01-506-0356
Structural Component Air Support
Used on f/a-22 raptor. 25.000" overall length 17.000" overall width 0.040" material thickness shroud assembly-forward equipment shelf-forward fuse made from 3 5HF11381-106 stiffeners 2" wide, 8" long; 1 5HF11381-109 shroud; 30 MS20470AD4-5 rivets; 27 in 2310BS002 nitrile
01-506-0358
Structural Component Air Support
Used on f/a-22 raptor. 8.000" overall length 2.000" overall width 0.040" material thickness shroud assembly ams 4085
01-506-0359
Movable Canopy
Transparency canopy
01-506-0361
Structural Aircraft Panel
Used on f-22 raptor. panel assy 21 gasket, 50 ring, 46 stud bolt
01-506-0375
Structural Component Air Support
7.620" overall length 7.370" overall width 1.400" material thickness honeycomb block nha 68A321400, u/o f-15e cum 210
01-506-0376
Structural Component Air Support
7.100" overall length 5.500" overall width block nha 68A321451; f-15c CUM1-BLK23, f-15d CUM1-BLK23
01-506-0377
Structural Component Air Support
5.600" overall length 0.750" overall width block nha 68A321451; f-15c CUM1-BLK23, f-15d CUM1-BLK23
01-506-0378
Structural Component Air Support
6.000" overall length 3.250" overall width 2.180" material thickness foam block next higher assy, 68A321451, u/o f-15c, cum 1-150, f-15d cum 1-25, f-15dj cum 1-4, f-15j cum 1
01-506-0379
Structural Component Air Support
10.500" overall length 2.360" overall width block nha 68A321451; f-15c CUM1-BLK23, f-15d CUM1-BLK23
01-506-0380
Structural Component Air Support
7.600" overall length 2.070" overall width block nha 68A321451; f-15c CUM1-BLK23, f-15d CUM1-BLK23
01-506-0381
Structural Component Air Support
5.500" overall length 1.820" overall width block nha 68A321451; f-15c CUM1-BLK23, f-15d CUM1-blk 23
01-506-0383
Structural Component Air Support
7.300" overall length 5.250" overall width 1.500" material thickness filler foam next higher assy, 68A324968, u/o f-15e, s cum 1
01-506-0384
Structural Component Air Support
13.400" overall length 6.750" overall width 4.000" material thickness block next higher assy, 68A324905, u/o f-15e cum 1
01-506-0425
Structural Aircraft Plate
9.000" overall length 1.900" overall width 0.050" material thickness weight retainer, control tab rudder finnish per SRF2.115; nha 65-5345
01-506-0431
Structural Aircraft Plate
01-506-0462
Structural Aircraft Plate
01-506-0464
Access Aircraft Door
01-506-0467
Structural Aircraft Plate
2.800" overall length 1.900" overall width 0.050" material thickness weight retainer finnish per SRF2.115; nha 65-5345
01-506-0496
Aircraft Fairing
Used on aircraft model code for f/a-18e/f.
01-506-0503
Aircraft Fairing
Used on fighter aircraft-first (f18 e/f).
01-506-0545
Structural Aircraft Plate
Used on mh060 helicopter. thick/gage .025; weight 0.30; nha duck exhaust-a.p.u.
