01-457-8280
Stiffener Aircraft Rib
Used on e-2 aircraft.
01-457-8396
External Surface Aircra Covering
Used on aircraft c-17a.
01-457-8808
Structural Aircraft Panel
C/o:core (-002) , skin (-005 & -006) stiffeners (-009, -013, -017) , screen (-023) ; p/o -302 assy; opposite -001; u/o acft 1 & subq
01-457-8813
Structural Aircraft Panel
01-457-8814
Structural Aircraft Panel
01-457-8823
Fuselage Parts Kit
Aircraft location - fuselage, center section - sta 243.000 to sta 373.800, assembly of, mod of; end item - f-16 aircraft, same as nsn 1560-01-450-9124 except minus p/n 16B5120-35
01-457-8848
Airfoil Rib
Used on e-2 aircraft.
01-457-9161
Aircraft Pylon
Adapter, targeting used on lta-1 cum 258
01-457-9618
Structural Aircraft Panel
35.000" overall length 33.500" overall width manufacturer suggested name-core; matl: grade b, class 2, al honeycomb, 8.1-8/1-20 (20150561t
01-458-0010
Structural Component Air Bracket
Used on merlin helicopter.
01-458-0352
Aircraft Stiffener
Used on f-14a-dcn aircraft. 22.000" overall length 5.000" overall width 0.063" material thickness
01-458-0354
Aircraft Stiffener
Used on f-14a aircraft.
01-458-0366
Aircraft Fairing
Manufacturer suggested name - fairing, sliding, upper, horizontal stabilizer; nha 17P5T4501
01-458-0367
Structural Aircraft Panel
01-458-0371
Structural Aircraft Plate
Used on pacer special. 18.000" overall length 6.000" overall width 0.160" material thickness nuclear hardness critical item; manufacturer suggested name: rub strip; matl: cres sht, 17-7ph cond a; ht to th 1050 per h-110; opposite -008
01-458-0372
Structural Aircraft Plate
Used on pacer special. 14.000" overall length 6.000" overall width 0.160" material thickness nuclear hardness critical item; manufacturer suggested name: rub strip; matl: cres sht, 17-7ph cond a; ht to th 1050 per h-110; opposite -029
01-458-0373
Structural Aircraft Plate
Used on pacer special. 14.000" overall length 6.000" overall width 0.160" material thickness nuclear hardness critical item; manufacturer suggested name: rub strip; matl: cres sht, 17-7ph cond a; ht to th 1050 per h-110; opposite -022
01-458-0374
Structural Aircraft Plate
Used on pacer special. 18.000" overall length 6.000" overall width 0.160" material thickness nuclear hardness critical item; manufacturer suggested name: rub strip; matl: cres sht, 17-7ph cond a; ht to th 1050 per h-110; opposite -020
01-458-0376
Bleed Air Duct Assembly
C/o 3 tube, 1 subassy, 1 nameplate, 1 flange, 2 doubler, 1 bracket, 1 ferrule; manufacturer suggested:duct
01-458-0377
Structural Aircraft Plate
Used on pacer special. 14.000" overall length 6.000" overall width 0.160" material thickness nuclear hardness critical item; manufacturer suggested name: rub strip; matl: cres sht, 17-7ph cond a; ht to th 1050 per h-110; opposite -026
01-458-0382
Structural Aircraft Panel
01-458-0386
Structural Aircraft Panel
01-458-0500
Structural Aircraft Plate
Used on kc-135 aircraft.
01-458-0501
Structural Aircraft Plate
Used on kc-135 aircraft.
01-458-0503
Structural Aircraft Plate
Used on kc-135 aircraft.
01-458-0504
Structural Aircraft Plate
Used on kc-135 aircraft.
01-458-0845
Aircraft Skin
01-458-0847
Aircraft Fairing
70.000" overall length 4.500" overall width 0.500" material thickness low observable critical item; u/ablade seal assy; matl:ti pl, ti 6242, ams 4919; opp -051; n/a DAA3652B626 u/o 01022 & subq; n/a DAA3652M639 u/o 05002, 05006-05021, 04001, 04003-04005
01-458-0851
Structural Aircraft Panel
01-458-0852
Structural Aircraft Panel
01-458-0854
Structural Aircraft Panel
01-458-0856
Structural Aircraft Panel
01-458-0857
Structural Aircraft Panel
01-458-0858
Structural Aircraft Panel
01-458-1144
Structural Component Air Support
01-458-1153
Structural Component Air Support
Used on a-4 aircraft converter. bracket, support
01-458-2560
Structural Component Air Fitting
Used on oh-58d helicopter.
01-458-2573
Explosion Suppressa Foam Segment
C/o foam blocks 68B580059-2121, 2123, 2125
01-458-2593
Explosion Suppressa Foam Segment
C/o foam blocks 68B580059-2001, 2007, 2013
01-458-2601
Explosion Suppressa Foam Segment
C/o foam blocks 68B58059-2221, 2219, 2223
01-458-2610
Explosion Suppressa Foam Segment
C/o foam blocks 68B580059-2225, 2227, 2229, 2231, 2233
01-458-2697
Aircraft Stiffener
Used on f-15 eagal aircraft.
01-458-2754
Fuselage Parts Kit
Used on f-15i aircraft. embedded global positioning system installation kit; rack build-up
01-458-3750
Access Hole Aircraft Frame
01-458-3908
Structural Aircraft Plate
Used on pacer special. 18.000" overall length 6.000" overall width 0.160" material thickness nuclear hardness critical item; manufacturer suggested name-rub strip; opp -027; n/a:DAA3150A515; heat treat to th 1050 per h-110; u/o 01002 & subq
01-458-3915
Structural Aircraft Plate
Used on pacer special. 18.000" overall length 6.000" overall width 0.160" material thickness nuclear hardness critical item; manufacturer suggested name-rub strip; opp -007; n/a:DAA3150A415; heat treat to th 1050 per h-110; u/0 01003, 01006 & subq
01-458-3916
Structural Aircraft Plate
Used on pacer special. 14.000" overall length 6.000" overall width 0.160" material thickness nuclear hardness critical item; manufacturer suggested name-rub strip; opp -030; n/a:DAA3150A515; heat treat to th 1050 per h-110; u/o 01002 & subq
01-458-3917
Structural Aircraft Plate
Used on pacer special. 18.000" overall length 6.000" overall width 0.160" material thickness nuclear hardness critical item; manufacturer suggested name-rub strip; opp -025; n/a:DAA3150A415; heat treat to th 1050 per h-110; u/o: 01002 & subq
01-458-3918
Structural Aircraft Plate
Used on pacer special. 18.000" overall length 6.000" overall width 0.160" material thickness nuclear hardness critical item; manufacturer suggested name-rub strip; opp -028; n/a:DAA3150A515; heat treat to th 1050 per h-110; u/o 01002 & subq
01-458-3978
Aircraft Bulkhead
Used on f-16 falcon aircraft. bulkhead, upper-outboard, sta 325.800
