01-488-9174
Structural Aircraft Plate
13.000" overall length 6.000" overall width 0.100" material thickness dimensions are stocksize; cres, sh. 17-7ph, cond. a; manufactured suggested name (strl pl-stif splc) ; nha -2
01-488-9293
Structural Aircraft Panel
Used on f-22a raptor. shield, assembly of durabilty critical item; m/f: PH15-7mo soln treated stainless steel, final cond TH1050; c/o: -113 plate, -118 shield, & MS20427M5-8 rivets; dim. are stock material
01-488-9296
Structural Aircraft Panel
Used on f-22 raptor. shield assy consists of shield pn 5HJ53030-117, plate 5HJ53030-113
01-488-9623
Aircraft Latch Assembly
Used on f-22 raptor. latch
01-488-9631
Structural Aircraft Plate
11.000" overall length 8.000" overall width 0.187" material thickness and ws 79.0 lh; dimensions are stocksize; strength T6 bare; nha -4; manf.suggested name (a/oa-10a wing ctr. panel repair-frt. spar web)
01-488-9632
Structural Aircraft Plate
15.000" overall length 6.000" overall width 0.100" material thickness and ws 79.0 lh; dimensions are stocksize; nha -2; strength T6 bare; manufacture suggested name (a/0a-10a wing ctr. panel repair-frt. spar web)
01-488-9633
Structural Aircraft Plate
15.000" overall length 15.000" overall width 0.125" material thickness strength T6 bare; dimension are stocksize; nha is -3;
01-488-9634
Structural Aircraft Plate
11.000" overall length 0.187" overall width 8.000" material thickness and WS79.0 lh; dimensions are stocksize; nha is -3; strength T6 bare; manufacture suggested name (a/oa-10a wing center panel repair-front spar web
01-488-9635
Structural Aircraft Plate
11.000" overall length 7.900" overall width 0.063" material thickness dimensions are stocksize; cres. sheet 17-7ph cond. a; nha -7;
01-488-9636
Structural Aircraft Plate
15.000" overall length 15.000" overall width 0.125" material thickness strength T6 bare; ws 79 lh; nha -4; c/o 1 strl plate-spar web, 1 strl pl-doubler; dimensions are stocksize
01-488-9687
Structural Component Air Support
Used on f/a-22 raptor. support, seal-vertical nozzle
01-488-9826
Aircraft Stiffener
01-488-9827
Structural Aircraft Plate
01-489-0068
Aircraft Latch Assembly
Used on c259 transport aircraft. pin type latch assembly
01-489-0090
Structural Aircraft Plate
01-489-0094
Tubing Aircraft Support
01-489-0272
Structural Aircraft Plate
01-489-0514
Structural Aircraft Panel
Used on c-130 aircraft.
01-489-0515
Structural Aircraft Plate
Used on sc-130b. doubler assembly
01-489-0742
Structural Component Air Support
Used on f/a-22 raptor.
01-489-0837
Structural Component Air Support
4.800" overall length 0.800" overall width 0.400" material thickness manf suggested name-cushion-cut shape, polyethylene foam
01-489-0986
Aircraft Latch Assembly
Used on f/a-22 raptor. latch, spring
01-489-0999
Structural Component Air Fitting
01-489-1035
Access Aircraft Door
01-489-1036
Access Aircraft Door
Used on fighter aircraft-first (f18 e/f). (navy) door, access, aircraf
01-489-1039
Access Aircraft Door
01-489-1040
Access Aircraft Door
01-489-1047
Aircraft Hinge
Used on f-18 e/f. hinge half, door mlg
01-489-1053
Aircraft Windshield Panel
Used on f18 e/f. windshield panel, ai
01-489-1063
Structural Component Aircraf Web
01-489-1079
Aircraft Windshield Assembly
01-489-1124
Structural Aircraft Plate
01-489-1139
Structural Aircraft Plate
01-489-1190
Structural Component Air Bracket
Used on chinook mk ii.
01-489-1349
Aircraft Intercostal
Used on f-22 raptor. 20.000" overall length 4.000" overall width 2.500" material thickness intercoastal, ftg 5PTM7T01 6-2222 sta titunium plate
01-489-1353
Aircraft Intercostal
Used on f-22 raptor. 20.000" overall length 4.000" overall width 2.500" material thickness intercoastal, ftg 5PTM7T01 6-2222 sta titunium plate
01-489-1495
Door Aircraft Hinge
Used on f/a-22 raptor. gooseneck hinge- access door
01-489-1625
Access Aircraft Door
Used on military aircraft.
01-489-1670
Aircraft Intercostal
Used on f-22 raptor.
01-489-5350
Structural Component Air Support
15.000" overall length 0.094" material thickness and WS79.0 lh; al shp/T6511; dimensions are stocksize, and 10136-1702; nha-2; manf. suggest name (tee-spcl, a/oa-10a wing ctr. panel repair-frt. spar web)
01-489-5351
Structural Aircraft Plate
15.000" overall length 6.000" overall width 0.100" material thickness and WS79.0 lh; dim. are stocksize; nha -2; strength T6 bare; manf. suggested name (a/oa-10a wing ctr. panel-frt. spar web)
01-489-5352
Structural Aircraft Plate
8.000" overall length 5.200" overall width 0.090" material thickness cres, sh, 17-7ph, cond a; nha -7; ANDWS79.0 lh; manf. suggested name (a/oa-10a wing ctr panel repair-frt spar web
01-489-5353
Fuel Tank Parts Kit
01-489-5354
Structural Aircraft Plate
01-489-5414
Structural Component Air Support
01-489-5502
Structural Aircraft Plate
Used on f/a-22 raptor. plate - splice ircm/ammo reload matt 2124-T8151 alum 2.000 plate
01-489-5573
Aircraft Latch Assembly
Used on c0890, panavia aircraft.
