00-515-4800
Aircraft Skin
140.000" overall length 48.000" overall width
00-515-4978
Structural Component Air Support
Used on acft model f4. left hand, used on tip outer wing ye 101.260
00-515-4979
Structural Component Air Support
Used on acft model f4. right hand, used on tip outer wing ye 101.260
00-515-4980
Structural Component Air Support
Used on acft model f4e. material spec mms-159 cond T7351, 3.500 in.w, 4.000 in.h, 6.000 in.lg, used on radome tip
00-515-5242
Aircraft Spar
00-515-5251
Aircraft Spar
00-515-5611
Aircraft Trailing Edge
00-515-5628
Aircraft Trailing Edge
00-515-5631
Aircraft Trailing Edge
00-515-5636
Aircraft Trailing Edge
00-515-5646
Aircraft Skin
84.000" overall length 48.000" overall width
00-515-6036
Stiffener Aircraft Rib
00-515-6038
Vertical Stabilizer Rib
00-515-6041
Stiffener Aircraft Rib
00-515-6043
Stiffener Aircraft Rib
00-515-6669
Structural Aircraft Plate
Used on UH-1. navy:door, access, aircraft
00-515-6670
Access Aircraft Door
00-516-2892
Structural Component Air Support
Used on acft model kc-135. cres
00-516-7007
Attachment Molded Tank Flange
00-516-8055
Access Aircraft Cover
00-516-8570
Attachment Molded Tank Flange
0.280" hole diameter
00-516-8674
Attachment Molded Tank Flange
0.280" hole diameter
00-516-8690
Attachment Molded Tank Flange
0.280" hole diameter
00-516-8892
Exhaust Muffler
21.000" overall length
00-516-8913
Aircraft Skin
Used on aircraft,model f14.
00-516-8925
Aircraft Skin
Used on aircraft,model f15.
00-516-9029
Filler Opening Cap
4.375" outside diameter pressure fuel servicing
00-517-9807
Aircraft Fairing
6.000" overall length 1.250" overall width 1.000" material thickness
00-517-9949
Structural Component Air Support
00-518-2382
Aircraft Frame
00-518-2383
Access Hole Aircraft Frame
00-518-2388
Aircraft Fairing
Sandwich construction with glass fabric skin
00-518-2389
Aircraft Fairing
Sandwich construction with glass fabric skin
00-518-2392
Access Aircraft Cover
Used on f-4 aircraft.
00-518-2419
Former
Aluminum alloy, qq-a-250-15;
00-518-2424
Aircraft Channel
9.000" overall length 0.380" material thickness u/o starter bracket
00-518-2437
Structural Component Air Support
Used on mcdonnell p/n 53-42001-series. type/model designation:f-4f/rf-4f/gy/phantom steel comp 4130, mil-s-6758, cond c; cadmium plated, qq-p-416, type 2, class 2; right hand angle design; baseflange 1.172 in. w by 1.547 in. lg by 0.100 in. thk; left side flange 1.906 in. w by 1.760 in. lg by 0.200 in. thk; surface finish 125.0 min microinch; heat treated 180000 to 20000 psi
00-518-2438
Structural Component Air Support
Type/model designation:f-4f/rf-4f (gy) phantom material-4130 steel per mil-s-6758, cond c, cad plate .0003-.0005 thk, type ii, class 2 per ps 13101; dim-stock-2.01 in x 1.76 x 1.17; heat treated to 180, 000-200, 000 psi per PS15015; surf fin 125.0 min microinch; left hand angle design; lh side flange 1.76 in w x 1.91 h x .20 thk, base flange 1.56 w x 1.17 l x .10 thk
00-518-2786
Aircraft Spar
00-518-2787
Aircraft Skin
00-518-2790
Aircraft Skin
00-518-2791
Structural Aircraft Plate
Aluminum alloy, qq-a-250/13 comp 7075 cond T6, 9.590 in. lg, 0.750 in. w, 0.080 in. thk
00-518-2825
Structural Component Air Bracket
Aluminum alloy qq-a-367
00-518-2856
Structural Component Air Support
Used on f-4c acft. matl plastic, mil-p-15047; matl size 0.015 by 0.500 by 14.180 in. lg; used on door assy-starter exhaust lh
00-518-4802
Structural Aircraft Panel
