01-287-4113
Aircraft Former
26.250" overall length 21.500" overall width 1.750" material thickness
01-287-4114
Aircraft Former
26.250" overall length 21.500" overall width 1.750" material thickness
01-287-4115
Aircraft Former
Consist of 1 former, 3 angle, 1 strut, 1 doubler, 6 bracket, misc hardware; nha 68A250700
01-287-4118
Aircraft Skin
95.000" overall length 24.000" overall width nha 68A250565; cond T76
01-287-4119
Aircraft Skin
01-287-4122
Aircraft Spar
01-287-4123
Aircraft Spar
01-287-4124
Aircraft Spar
01-287-4532
Structural Aircraft Plate
Used on F-15. 0 alclad
01-287-4533
Structural Aircraft Plate
Used on F-15. 0 alclad
01-287-4534
Structural Aircraft Plate
Used on F-15. 0 alclad
01-287-4535
Structural Aircraft Plate
Used on F-15. 0 alclad
01-287-4536
Structural Aircraft Plate
Used on F-15. 0 alclad
01-287-4537
Structural Aircraft Plate
Used on F-15. 0 alclad
01-287-4538
Structural Aircraft Plate
Used on F-15. 0 alclad
01-287-4539
Structural Aircraft Plate
Used on F-15. 0 alclad
01-287-4540
Structural Aircraft Plate
Used on F-15. 0 alclad
01-287-4541
Structural Aircraft Plate
Used on F-15. 0 alclad
01-287-4542
Structural Aircraft Plate
Used on F-15. 0 alclad
01-287-4543
Structural Aircraft Plate
Used on F-15. 0 alclad
01-287-4583
Fuel Aircraft Tank
Outside diameter:1.280 in.nom; drain plug:included; mounting bracket:provided; baffle:provided; mounting position:vertically across length; filler neck:included; drain opening:included; equipment on which mounted:mau-12c/a bomb ejector rack; quantity:1; shape:cylindrical or oval;
01-287-5355
Pylon Aircraft Fairing
01-287-5468
Structural Aircraft Plate
1.000" overall width one 0.628 in. dia hole; two 0.209 in. dia holes
01-287-5469
Structural Component Air Support
4.060" overall length 3.000" overall width
01-287-5470
Structural Component Air Support
01-287-5471
Structural Component Air Support
01-287-5472
Structural Component Air Support
Unpkg unit weight:1.334 lbs; spec proj era/80132;
01-287-5473
Structural Component Air Support
01-287-5474
Structural Component Air Support
1.152" overall length 0.063" material thickness
01-287-5477
Structural Aircraft Panel
Three 0.217 in. min, 0.233 in. max dia holes; three 0.186 in. min, 0.192 in. max dia holes; 125 microinch surface; 200 microinch holes
01-287-5478
Structural Aircraft Panel
Eight 0.217 in. min 0.223 in. max dia holes; 125 microinch surfaces; 200 microinch holes
01-287-5483
Airfoil Rib
Used on aircraft,a-7. 5.600" overall length 4.300" overall width 0.040" material thickness
01-287-5484
Airfoil Rib
Used on aircraft,a-7. 7.100" overall length 5.100" overall width 0.032" material thickness
01-287-5485
Airfoil Rib
Used on aircraft,a-7. 5.700" overall length 4.400" overall width 0.040" material thickness
01-287-5488
Cowling
Used on aircraft f-14. 1.240" overall length 0.860" overall width
01-287-6090
Access Aircraft Door
Used on acft model b-1b. al bare plate 2024-T851 per qq-a-250/4; 40.40 in lg, 34.00 in wd, 0.250 in thk; located YF899.5 to YF932; usesed on lower outbd controls bay
01-287-6091
Access Aircraft Door
Used on acft model b-1b. al bare plate 2024-T851 per qq-a-250/4; 40.40 in lg, 34.00 in wd, 0.250 in thk; located YF899.5 to YF932; usesed on lower outbd controls bay
01-287-6116
Aircraft Fairing
This item has been determined to be a critical application item. in-flight failure of this item would create a hazardous condition
01-287-6117
Structural Component Air Support
Used on t-38 aircraft. part of beam installation-supportpanel, speed brake, fuselage sta 326.10
01-287-6118
Structural Component Air Support
Used on acft model b-1b. consist of 1 fitting, 2 bushing; nha L1800075
01-287-6119
Structural Component Air Support
Used on acft model b-1b. consist of 1 fitting, 2 bushing; nha L1800075
01-287-6120
Structural Component Air Support
Used on acft model b-1b. consist of 1 fitting, 2 bushing
01-287-6121
Structural Component Air Support
Used on acft model b-1b. consist of 1 fitting, 2 bushing; nha L1800075
01-287-6122
Structural Component Air Support
Used on acft model b-1b. consist of 1 fitting, 2 bushing; nha L1800075
01-287-6135
Aircraft Former
01-287-6136
Aircraft Former
0 alclad
01-287-6137
Aircraft Former
0 alclad
01-287-6139
Stiffener Aircraft Rib
C/o 1 stud, 3 bushing, 1 seal, 1 rib, 1 insert; nha L1804005
01-287-6140
Stiffener Aircraft Rib
C/o 1 rib, 1 seal, 3 bushing; nha L1804005
01-287-6141
Stiffener Aircraft Rib
C/o 1 seal, 1 stud, 3 bushing, 1 rib, 1 insert; nha L1804006
