01-244-1328
Wing Aircraft Spoiler
01-244-1337
Canopy Aircraft Frame
Used on f-15 acft. frame, canopy lh
01-244-1367
Canopy Transparency
Used on F-15. canopy, fwd frame channel, canopy, forward frame; alclad 0
01-244-1368
Structural Aircraft Plate
Used on C-141. make from LS33743-1 x 6; ; ht tr T73; nha 3W19030, 3W19039, 3W19049
01-244-1370
Structural Aircraft Plate
Used on F-15. channel, canopy
01-244-1377
Structural Component Air Support
Used on acft model f-15.
01-244-1423
Aircraft Former
9.000" overall length 1.000" overall width 1.000" material thickness nha 3W19030, 3W19039, 3W19049
01-244-1424
Aircraft Former
9.000" overall length 1.000" overall width 1.000" material thickness nha 3W19030, 3W19039, 3W19049
01-244-1426
Aircraft Former
76.000" overall length 3.000" overall width 0.071" material thickness heat treat T6
01-244-1434
Aircraft Skin
Used on F-15.
01-244-1435
Aircraft Skin
Steel, ams 5510; primer, epoxy polyamide, GP111V1
01-244-1865
Vertical Stabilizer
01-244-1899
Aircraft Skin
Used on acft model f-111. steel per mil-s-6721 cres 321, 45.000 in. lg, 40.000 in. w, 0.020 in. thk
01-244-2850
Structural Aircraft Panel
01-244-2851
Structural Aircraft Panel
01-244-3023
Stiffener Aircraft Rib
01-244-3024
Stiffener Aircraft Rib
01-244-3075
Structural Component Air Support
Used on acft model f-15e. 6al-6v-2sn per mms-1203; 4.80 in. lg, 1.74 in. wd, 0.063 in. thk; opposite p/n -2049; nha 68A331000; located on fs 672.680
01-244-3076
Structural Component Air Support
Used on acft model f-15e. 6al-6v-2sn per mms-1203; 4.80 in. lg, 1.74 in. wd, 0.063 in. thk; opposite p/n -2050; nha 68A331000; located on fs 672.680
01-244-3077
Structural Component Air Support
Used on acft model f-15e. 6al-6v-2sn per mms 1203; 3.45 in. lg, 2.25 in. wd, 0.063 in. thk; opposite p/n -2047; nha 68A331000; located on fs 672.680
01-244-3078
Structural Component Air Support
Used on acft model f-15e. 6al-6v-2sn per mms-1203; 3.16 in. lg, 1.60 in. wd, 0.063 in. thk; opposite p/n -2045; nha 68A331000; located on fs 672.680
01-244-3079
Structural Component Air Support
Used on acft model f-15e. 6al-6v-2sn per mms-1203; 37.71 in. lg, 7.81 in. wd, 0.090 in. thk; opposite p/n -2043; nha 68A331000; located on fs 672.680
01-244-3081
Structural Component Air Support
Used on f-15 acft.
01-244-3082
Structural Component Air Support
Used on f-15 acft.
01-244-3095
Aircraft Former
10.500" overall length 3.500" overall width 1.000" material thickness 6al-4v; opposite pn -2011; nha 68A331014
01-244-3096
Aircraft Former
10.500" overall length 3.500" overall width 1.000" material thickness 6al-4v; opposite pn -2012; nha 68A331014
01-244-3097
Aircraft Former
Used on F-15. lower
01-244-3098
Aircraft Former
Used on F-15. lower
01-244-3101
Longeron
Used on F-15.
01-244-3102
Aircraft Pylon
01-244-3103
Aircraft Skin
60.000" overall length 9.500" overall width nha p/n 68A314022 & 68T060138
01-244-3104
Aircraft Skin
Used on F-15.
01-244-3106
Aircraft Skin
Used on F-15.
01-244-3107
Aircraft Skin
Used on F-15.
01-244-3108
Aircraft Skin
Used on F-15.
01-244-3109
Aircraft Spar
01-244-4091
Aircraft Former
21.000" overall length 2.000" overall width 0.032" material thickness stiffener-fairing, arg hook
01-244-4092
Aircraft Former
28.000" overall length 3.000" overall width 0.040" material thickness stiffener-fairing, arg hook
01-244-4093
Aircraft Former
28.000" overall length 3.000" overall width 0.040" material thickness stiffener-fairing, arg hook
01-244-4094
Aircraft Former
21.000" overall length 2.000" overall width 0.032" material thickness stiffener-fairing, arg hook
01-244-4096
Aircraft Former
14.000" overall length 3.000" overall width 0.040" material thickness stiffener-fairing, arg hook
01-244-4752
Structural Component Air Support
Aluminum alloy, qq-a-250/13 7075-T6 or aluminum alloy, qq-a-250/5 2024-T62; primer, epoxy polyamide, mil-p-23377 or GSS4310 grumman aerospace corp, bethpage, ny; 0.063 in. material thk
01-244-4879
Structural Component Air Support
01-244-5141
Structural Aircraft Plate
01-244-5142
Structural Aircraft Plate
01-244-5451
Structural Aircraft Plate
Used on acft model e-3a.
01-244-5452
Structural Aircraft Plate
Used on F-15.
01-244-5453
Structural Aircraft Plate
Used on F-15.
01-244-5458
Structural Component Air Support
Used on acft model b-1b. replacing -003; ST0160LB0013; nha L6319001; located YF793.00
01-244-5468
Aircraft Floor
