01-486-9844
Structural Aircraft Panel
Used on f/a-22 raptor. panel - bonded part, upper no 2
01-486-9845
Structural Aircraft Panel
Used on f-22 raptor. panel assembly wind swept surface critical item; carbon/bmi & glass/bmi composite materials; c/o: fairing core (3) , clip (16) , bracket (5) , rings (45) , misc hardware
01-486-9846
Structural Aircraft Panel
Used on f-22 raptor. panel 104 opposite -103
01-486-9848
Structural Aircraft Panel
Used on f-22 raptor. panel, bonded 104 opposite
01-486-9850
Window Aircraft Frame
01-486-9851
Window Aircraft Frame
01-486-9852
Structural Aircraft Panel
Used on f-22 raptor. skin panel wind swept surface critical item; opposite -103; m/o: carbon/bmi & glass/bmi composite materials
01-486-9853
Window Aircraft Frame
01-486-9855
Structural Aircraft Panel
Used on f-22 raptor. panel, skin opposite -104
01-486-9856
Structural Aircraft Panel
Used on f-22 raptor. panel, bonded 103 opposite
01-486-9858
Structural Aircraft Panel
Used on f-22 raptor. panel bonded, skin 104 is opposite
01-486-9860
Stiffener Aircraft Rib
Used on f-22 raptor. 6.000" overall length 4.000" overall width rib plate; -104 opposite
01-486-9864
Structural Aircraft Panel
Used on f-22 raptor. panel, skin opposite -103
01-486-9865
Stiffener Aircraft Rib
Used on f-22 raptor. 4.992" overall length 4.000" overall width rib width dim. is stock material; opposite -103; m/o: 7075-T7451 aluminum plate
01-486-9868
Structural Aircraft Panel
Used on f/a-22 raptor. 6.000" overall length 3.000" overall width fitting plate
01-486-9869
Structural Aircraft Panel
Used on f-22 raptor. panel assembly wind swept surface critical item; c/o: 5HW84752-107 panel
01-486-9870
Structural Aircraft Panel
Used on f-22 raptor. panel assy opposite -219; consist of 1 panel, 1 splice, (ref) smothness, std. dod barcode, ident marking, raw matl., 6 rivet, 4 pin, 3 nut, 4 collar, 2 label, sealant (ar)
01-486-9872
Aircraft Skin
Used on f/a-22 raptor. caron/bmi
01-486-9873
Structural Aircraft Panel
Used on f-22 raptor. panel assy opposite -217; c/o 1 (panel, lwr 5HW84752-108) , (ref smoothness, std dod barcode, ident. marking, raw matl.) , 2 label
01-486-9875
Access Aircraft Door
Used on f-22 raptor. finish assy c/o 1 (ref 5HA41501-105 door assy, lh ob) , 3 coating appl., 2 label, 1 filler; 5HY03323-151 maybe used as alternate; used on main weapons bay
01-486-9876
Aircraft Door
Used on f-22 raptor. finish assembly wind swept surface critical item / durability critical item
01-486-9877
Structural Aircraft Panel
Used on f-22 raptor. finish assy
01-486-9878
Access Aircraft Door
Used on f-22 raptor. finish assy c/o ref ( 5HA41501-107 dorr assy, rh ob) , 1 coating appl (5HY03320-102) , 1 coating appl (5HY03321-108
01-486-9880
Access Aircraft Door
Used on f-22 raptor. finish assy c/o 1 ref (5HA44101-104 door assy) , 1 coating (5HY03320-106) , 2 coating (5HY03321-114
01-486-9884
Access Aircraft Door
Used on f-22a raptor. finish assembly wind swept surface critical item
01-486-9885
Access Aircraft Door
Used on f-22 raptor. finish assy u/o gun
01-486-9886
Access Aircraft Door
Used on f-22 raptor. finish assy c/o 1 (ref 5HA42501-105 door assy) , 2 label, 1 filler, 1 coating 5HY03320-107, 2 coating 5HY03321-119
01-486-9887
Aircraft Door
Used on f-22 raptor. finish assy c/o 1 (ref) door assy, 2 labels, 1 filler, 3 coating appl.
01-486-9888
Structural Aircraft Panel
Used on f/a-22 raptor. finish assy
01-486-9889
Aircraft Door
Used on f-22 raptor. door assy c/o 1 (ref 5HF13230-102) bleed door assy, 2 coating appl, 2 label
01-486-9890
Aircraft Door
Used on f-22 raptor. finish assy c/o 1 (ref) door assy, 3 coatings, 2 labels
01-486-9891
Aircraft Door
Used on f-22 raptor. finish assy c/o 1 (ref) door assy, 3 coating appl., 2 label
01-486-9892
Aircraft Door
Used on f-22 raptor. door assembly wind swept surface critical item
01-486-9893
Access Aircraft Door
Used on f-22 raptor. finish assy used on engine, service, aft, fwd; c/o 1 (ref 5HF75110-103 door assy) , 3 coating appl, 2 labels, 1 filler
01-486-9894
Aircraft Door
Used on f-22 raptor. finish assembly wind swept surface critical item
01-486-9895
Access Aircraft Door
Used on f-22 raptor. finish assy used on engine, service, aft, fwd; c/o 1 (ref 5HF75110-107 door assy) , 3 coating appl, 2 label, 1 filler
01-486-9896
Access Aircraft Door
Used on f-22 raptor. finish assy c/o 1 ref (5HF46064-109 door assy) , 3 coating appl, 2 labels, 1 filler; used on ircm
01-486-9897
Access Aircraft Door
Used on f-22 raptor. finish assy used on ircm; c/o 1 (ref 5HF46065-109 door assy) , 3 coating appl, 2 labels, 1 filler
01-486-9898
Access Aircraft Door
Used on f-22 raptor. finish assy c/o 1 (ref 5HF75101-127 door assy) , 3 coating appl., 79 ring, 2 label, 79 bolt, 1 filler; used on engine, service, aft, fwd
01-486-9899
Access Aircraft Door
Finish assy used on ircm; c/o 1 (ref 5HF46072-109 door assy) , 3 coating appl, 2 labels, 1 filler
01-486-9900
Access Aircraft Door
Used on f-22 raptor. finish assy used on engine, service, aft, fwd; c/o 1 (ref 5HF75107-105 assy, 3 coating appl., 74 ring, 2 label 1 filler, 74 bolts
01-486-9903
Structural Component Air Fitting
3.000" overall length 0.500" overall width 0.500 " material thickness nha 160J611311; effectivity 1 thru on; forging ams 6526 alloy steel, superstrength; holes will require reaming when installing part; dimensions are stocksize
01-486-9904
Aircraft Skin
55.000" overall length 17.500" overall width alclad; dimensions are stocksize; part of -1 assembly
01-487-0024
Outer Wing Section
01-487-0180
Structural Component Air Fitting
Used on f/a-22 raptor.
01-487-0187
Structural Aircraft Plate
23.000" overall length 5.000" overall width 0.090" material thickness nha 160J611311; manf. suggested name: details shim; dim. are stocksize
01-487-0188
Structural Aircraft Panel
46.000" overall length 20.000" overall width
01-487-0189
Structural Aircraft Panel
42.000" overall length 15.000" overall width
01-487-0192
Structural Aircraft Panel
C/o 1 floor assembly, 5 double angle brackets, 10 closures, 1 coor panel, 12 bracket angles, 2 plates, 4 double angle supports, 48 plate nuts; rivets, epoxy adhesive & sealant as required; manf. suggest name: floor-fuel cell; corrugated
01-487-0193
Structural Component Air Support
42.000" overall length 5.000" overall width 0.050" material thickness alcd sheet; manf. suggested name:closure; part of -3 assembly; dimensions are stocksize
