01-108-1295
Structural Component Air Support
8.500" overall length 3.500" overall width 0.063" material thickness finish F02.30; heat treat T42
01-108-1298
Structural Component Air Bracket
5.000" overall length 2.000" overall width 0.090" material thickness heat treat T42; finish f-2.30
01-108-1299
Structural Component Air Bracket
5.000" overall length 2.000" overall width 0.090" material thickness heat treat T42; finish f-2.30
01-108-1300
Structural Component Air Fitting
01-108-1301
Structural Aircraft Plate
3.200" overall length 2.400" overall width 0.063" material thickness finish f-12.206; ht 150-170 ksi
01-108-1302
Structural Component Air Fitting
01-108-1303
Structural Aircraft Plate
01-108-1305
Structural Component Air Fitting
Heat treat 160-180 ksi; finish f-1.285
01-108-1306
Structural Component Air Fitting
Heat treat 160-180 ksi; finish 1.285
01-108-1307
Structural Component Air Fitting
Heat treat 160-180 ksi; finish f-1.285
01-108-1308
Structural Component Air Fitting
Heat treat 160-180 ksi; finish f-1.285
01-108-1312
Aircraft Door
7.600" overall length 5.000" overall width finish f-2.30
01-108-1316
Structural Component Air Fitting
2.100" overall length 1.500" overall width 0.500 " material thickness finish f-2.30
01-108-1317
Aircraft Latch Assembly
Used on acft e3a. side cowl panel, 3.000 in. lg, 1.000 in. thk, 1.500 in. w, 2024-T851 bar per qq-a-250/4 finish SRF2.30
01-108-1327
Aircraft Door
01-108-1342
Structural Aircraft Plate
15.800" overall length 8.400" overall width 0.050" material thickness finish f-2.30; heat treat T42
01-108-1343
Structural Aircraft Plate
01-108-1344
Structural Aircraft Plate
01-108-1345
Structural Aircraft Plate
Inbd
01-108-1353
Longeron
51.000" overall length 9.500" overall width 0.050" material thickness heat treat T42; finish srf-2.30
01-108-1354
Longeron
51.000" overall length 9.500" overall width 0.050" material thickness 20ij-0 sht clad, heat treat T42; finish srf-2.30
01-108-1355
Aircraft Skin
Used on F-111. 28.000" overall length 20.000" overall width
01-108-1367
Aircraft Door
Used on acft model f-16a/b usaf. c/o door assy 1 ea p/n 16B4505-93, bolt 44 ea p/n C9537-4-4, ring 44 ea, p/n C9538-4, gen sealant as requiredp/n 16B4505-87, locted from fs 217.00 to fs 243.00; superseded p/n 16B4505-813 ni per ecn 93860; nha 16B410-99; eff 61-0262-9999
01-108-2677
Access Aircraft Cover
Used on F-16. rh equipment bay
01-108-2774
Structural Aircraft Plate
Used on acft model f4. al alloy 2024-0 per qq-a-250/5 cond 0., 0.050 in.thk, 4.000 in.w, 6.000 in.lg, left hand
01-108-2776
Structural Aircraft Plate
Used on acft model f4e. used on door assy number 5, engine access, located from fs 447.05 to fs 493.00, left hand
01-108-2779
Movable Canopy
01-108-2780
Movable Canopy
01-108-2784
Aircraft Skin
95.000" overall length 54.000" overall width cond 0
01-108-2785
Aircraft Skin
89.000" overall length 54.000" overall width cond 0; opposite to p/n 3F41095-119
01-108-2786
Aircraft Skin
89.000" overall length 59.000" overall width cond 0; opposite to p/n 3F41095-122
01-108-2787
Aircraft Skin
83.000" overall length 54.000" overall width cond 0; opposite to p/n 3F41095-121
01-108-3508
Structural Component Air Support
Used on uh-60a helicopter.
01-108-3510
Structural Aircraft Panel
Used on uh-60a helicopter.
01-108-3715
Cowling
Used on uh-60a helicopter.
01-108-4007
Structural Component Air Fitting
01-108-4010
Structural Component Air Support
01-108-4011
Structural Component Air Support
01-108-4012
Structural Component Air Support
2.100" overall length 0.625" material thickness finish f-8.07
01-108-4048
Structural Aircraft Panel
Used on 1520010350266.
01-108-4049
Aircraft Fairing
01-108-4050
Aircraft Fairing
01-108-4051
Aircraft Fairing
30.500" overall length 24.000" overall width 0.080" material thickness finish SRF2.30
01-108-4052
Aircraft Fairing
30.500" overall length 24.000" overall width 0.080" material thickness finish srf-2.30
