01-260-1073
Airfoil Rib
16.350" overall length 9.400" overall width 0.050" material thickness
01-260-1075
Airfoil Rib
17.040" overall length 9.910" overall width 0.050" material thickness
01-260-1079
Aircraft Skin
Used on F-15. 31.500" overall length 23.800" overall width
01-260-1080
Aircraft Spar
83.000" overall length 4.000" overall width 3.750" material thickness opposite -2035; replaces -2030; nha 68A116119
01-260-1081
Aircraft Spar
83.000" overall length 4.000" overall width 3.750" material thickness opposite -2036; replaces -2029; nha 68A116119
01-260-1490
Structural Aircraft Plate
3aluminum alloy, qq-a-250/5 2024-T3, primer, epoxy polyamide, GSS4310 grumman aerospace corp; 2.500 in. long; 0.810 in. wide, 0.032 in. thk; 2 holes 0.342 in. min 0.349 in. max dia; 1 hole 0.500 in. dia; chamfer 4 corners 0.311 in. long, 45.0 degrees
01-260-1491
Structural Component Air Support
01-260-1492
Structural Component Air Support
4.062" overall length 2.500" overall width
01-260-1737
Structural Component Air Support
01-260-1774
Wing Landing Flap
01-260-2949
Structural Aircraft Plate
19.700" overall length 18.250" overall width 1.9900" material thickness plate, adaper-rescue hoist
01-260-2950
Structural Aircraft Plate
Used on C-141.
01-260-2955
Structural Component Air Support
1.800" overall length 1.600" overall width
01-260-2959
Structural Component Air Support
Used on c-130 acft.
01-260-2960
Structural Component Air Support
01-260-2962
Structural Aircraft Panel
P/o leading edge, ram air plenum
01-260-2974
Aircraft Former
Used on C-130.
01-260-2975
Aircraft Former
Used on C-130. 0 T4 clad
01-260-2979
Airfoil Rib
Used on C-130.
01-260-2980
Airfoil Rib
Used on C-130. cond 0 clad
01-260-4913
Structural Component Air Support
01-260-4954
Airfoil Rib
0.080" material thickness chromate surface treated
01-260-5279
Access Aircraft Cover
Rh upper strake FS279.40 to FS293.80
01-260-5283
Access Aircraft Door
Used on f-16c/d aircraft.
01-260-5343
Structural Aircraft Plate
Used on acft model b-1b. nuclear hardness critical item;
01-260-5344
Structural Aircraft Plate
Used on B-1B. together with -003 hinge pin replaces L5342982
01-260-5345
Structural Aircraft Plate
Used on C-130. 5.700" overall length 2.000" overall width stiffener, cond 0 clad
01-260-5347
Structural Aircraft Plate
Used on C-141. 110.000" overall length T6 bare plate; nha 3F30222; opposite p/n -104
01-260-5348
Structural Aircraft Plate
Used on C-141. 110.000" overall length opposite -106; nha 3F30222; T6 bare plate
01-260-5349
Aircraft Fairing
01-260-5350
Aircraft Fairing
01-260-5351
Aircraft Fairing
01-260-5352
Aircraft Fairing
01-260-5353
Aircraft Fairing
01-260-5354
Aircraft Fairing
01-260-5355
Aircraft Fairing
01-260-5357
Aircraft Fairing
01-260-5358
Aircraft Fairing
01-260-5359
Aircraft Fairing
01-260-5360
Aircraft Fairing
01-260-5361
Aircraft Fairing
01-260-5362
Aircraft Fairing
01-260-5363
Aircraft Fairing
