01-223-0634
Structural Component Air Support
Type/model designation:f-4e/gy/ aluminum alloy 5052-0 ww-t-700/4 matl 1.000 in. thk BY0.281 in. w by 4.703 in. lg
01-223-0635
Structural Component Air Support
Aluminum alloy, qq-a-367, T6; 4.580-4.640 in. lg; 4 mtg holes 0.249-0.255 in. dia; 14 rivet holes
01-223-0636
Structural Component Air Support
Aluminum alloy, qq-a-367, T6; 4.580-4.640 in. lg; 4 mtg holes 0.249-0.255 in. dia; 14 rivet holes
01-223-1113
Access Aircraft Door
Used on F-16. engine lh access FS345 to FS389
01-223-1207
Structural Component Air Fitting
01-223-1217
Structural Component Air Support
Used on acft model b-1b. al alloy 7075-t-76511 per AMS4340; 5.000 in. o/a dia, 3.040 in. dia center opening, 1.120 in. o/a h; includes 12 attached nutplates; nha L5338278
01-223-1219
Structural Component Air Support
Used on f-15 acft. material per 1MA10274-D05 x 3.200 in. lg
01-223-1223
Structural Aircraft Panel
Used on acft model e-3a. c/o 1 panel, dacron cloth, velcro tape, rigid vinyl, 1 bronze staple
01-223-1224
Structural Aircraft Panel
Used on acft model e-3a. c/o 1 panel, 1 gap cover, dacron cloth, velcro tape, rigid vinyl, 2 inserts, 1 bronze staple
01-223-1225
Structural Aircraft Panel
Used on acft model e-3a. c/o 1 panel, 1 door assembly, dacron cloth, velcro tape, rigid vinyl, 1 bronze staple
01-223-1227
Structural Aircraft Panel
Used on acft model e-3a. c/o 1 panel, 4 rubber supports, dacron cloth, velcro tape, rigid vinyl, 2 inserts, 1 bronze staple
01-223-1229
Structural Aircraft Panel
Used on acft model e-3a. c/o 1 panel, 2 rubber supports, 1 gap cover, dacron cloth, velcro tape, rigid vinyl, bronze staple
01-223-1230
Structural Aircraft Panel
C/o 1 panel, 3 rubber supports, 1 gap cover, dacron cloth, velcro tape, rigid vinyl, bronze staple
01-223-1231
Structural Aircraft Panel
Used on acft model e-3a. c/o 1 panel, 3 rubber supports, 1 gap cover, dacron cloth, velcro tape, rigid vinyl, 1 bronze staple
01-223-1232
Structural Aircraft Panel
C/o 1 panel, 3 spacers, 1 rubber seal, dacron cloth, rigid vinyl, 4 spacer insert, 1 bronze staple
01-223-1233
Structural Aircraft Panel
Used on acft model e-3a. c/o 1 panel, 2 rubber supports, 1 gap cover, dacron cloth, velcro tape, rigid vinyl, 1 bracket assembly, 11 inserts, 1 bronze staple
01-223-1236
Aircraft Former
01-223-1237
Aircraft Former
20.500" overall length 8.000" overall width 3.000" material thickness material per mms 149 condition T851 2124-T851
01-223-1238
Airfoil Rib
Used on F-15.
01-223-1239
Aircraft Skin
01-223-1240
Aircraft Skin
Used on F-15.
01-223-1241
Aircraft Skin
Used on F-15.
01-223-1242
Aircraft Skin
Used on F-15.
01-223-1243
Aircraft Skin
Used on F-15.
01-223-1244
Aircraft Skin
Used on F-15.
01-223-1245
Aircraft Skin
Used on F-15.
01-223-1355
Fluid Aircraft Manifold
13.180" overall length 8.990" overall width nha L4801629-102; used on acft model b-1b
01-223-1612
Access Aircraft Door
Used on aircraft model av-8.
01-223-1648
Aircraft Skin
Used on aircraft model av-8. aluminum alloy per qq-a-250/13, cond-o
01-223-1649
Aircraft Skin
Used on aircraft model av-8. aluminum alloy per qq-a-250/13, cond-o
01-223-1650
Aircraft Skin
Used on aircraft model av-8. aluminum alloy per qq-a-250/13, cond-o
01-223-1651
Aircraft Skin
01-223-1652
Structural Aircraft Panel
Used on EA-6A.
01-223-1653
Structural Aircraft Panel
01-223-1655
Structural Aircraft Panel
01-223-1656
Structural Aircraft Panel
01-223-2275
Structural Aircraft Plate
Type/model designation:f-4e/gy/ iron alloy uns K66286 ams 5525, matl 0.032 in. thk by 1.641 in. w by 6.500 in. lg
01-223-2277
Structural Aircraft Plate
2.000" overall length 1.500" overall width 0.250" material thickness material per fms 1011
01-223-2278
Structural Component Air Support
Used on 1560-00-894-4186. type/model designation:f-4e/gy/ aluminum alloy 7075 qq-a-250/13, to; matl 0.032 in. thk by 1.234 in. w by 1.922 in. lg
01-223-2280
Structural Component Air Support
Used on c-5a aircraft.
01-223-2281
Structural Component Air Support
01-223-2282
Structural Component Air Support
Make from A356-T6 casting
01-223-2283
Structural Component Air Support
01-223-2284
Structural Component Air Support
01-223-2286
Structural Component Air Support
Used on acft model f-111 a/c.
01-223-2287
Structural Component Air Support
Used on acft model f-111a,d,e,f,ef-111a. steel per mil-s-7720 condition a composition 303, 1.200 in. lg, 0.200 in. w, 0.750 in. thk
01-223-2288
Structural Component Air Support
Used on acft model f-111. c/o steel fitting per fms-1011 D6ac, 2 ea. insert p/n 12S1127-7, as required compound
01-223-2294
Structural Aircraft Panel
Used on acft model e-3a. c/o 1 panel, 1 face sheet, 1 air grill, 6 inserts; nha 204-40501
01-223-2295
Structural Aircraft Panel
01-223-2296
Structural Aircraft Panel
