01-394-0975
Aircraft Window Panel
01-394-0979
Aircraft Window Panel
01-394-1089
Aircraft Door
01-394-1090
Structural Aircraft Plate
01-394-1133
Aircraft Frame
01-394-1182
Aircraft Skin
01-394-1183
Aircraft Skin
01-394-1184
Aircraft Skin
01-394-1185
Structural Component Air Bracket
01-394-1186
Aircraft Skin
01-394-1187
Structural Component Air Bracket
01-394-1188
Aircraft Door
01-394-1189
Aircraft Door
01-394-1190
Aircraft Fairing
01-394-1191
Aircraft Fairing
01-394-1201
Structural Component Air Fitting
01-394-1247
Structural Aircraft Panel
Cover assembly, rear; ac-130u mod
01-394-1248
Structural Aircraft Panel
Cover assembly, side r.h.; ac-130u mod
01-394-1258
Aircraft Skin
Material stock p/n 68A112137-2007, 6al-4v titanium plate
01-394-1260
Aircraft Skin
Material stock p/n 68A112137-2008, 6al-4v titanium plate
01-394-2019
Aircraft Beam
281.860" overall length used as a chord-keel beam; opp -7; matl:alter bac 1506-566; T6 temp
01-394-2241
Structural Aircraft Panel
Primer surface treated
01-394-2242
Aircraft Wing Assembly
Used on sh-60f acft.
01-394-2245
Structural Aircraft Panel
Anodize surface treated
01-394-2246
Aircraft Window Panel
Used on sh-60f acft.
01-394-2252
Structural Aircraft Panel
01-394-2255
Structural Aircraft Panel
Used on hh-60h (active) and hh-60j(reserve)configurations. hcs/mrr window surround instl
01-394-3041
Fuselage Section
Used on aircraft f16a, mod kit 'e', generl dynamics corp.
01-394-3045
Fuselage Section
Used on aircraft f16a, mod kit 'e', generl dynamics corp.
01-394-3274
Aircraft Strut
01-394-3312
Structural Component Air Bracket
Used on ab205 helicopter.
01-394-3436
Aircraft Stiffener
Nha 5-86872; finish 2.30
01-394-3437
Aircraft Stiffener
Finish srf-2.30; nha 5-87831
01-394-3438
Aircraft Stiffener
Finish f-2.30
01-394-3439
Aircraft Stiffener
Finish f-2.30; nha 5-87828
01-394-3440
Aircraft Stiffener
Finish f-2.30; nha 5-87824
01-394-3441
Aircraft Stiffener
4.350" overall length 3.700" overall width 0.064" material thickness finish f-2.115; nha 5-87828
01-394-3442
Aircraft Stiffener
4.200" overall length 3.900" overall width 0.081" material thickness nha 5-87828; finish f-2.115
01-394-3443
Aircraft Stiffener
75.000" overall length nha 5-89532; opposite -2; finish f-2.10; heat treat T6; make from BAC1509
01-394-3444
Aircraft Stiffener
75.000" overall length make from bac 1509; finish f-2.10; heat treat T6; opposite -1; nha 5-89532
01-394-3445
Aircraft Stiffener
4.200" overall length 3.900" overall width 0.081" material thickness finish f-2.115; nha 5-87828
01-394-3446
Aircraft Stiffener
Finish f-2.30
01-394-3447
Aircraft Stiffener
Finish f-2.30; nha 5-87831
01-394-3450
Aircraft Stiffener
Nha 5-87831
01-394-3452
Structural Component Air Fitting
Opposite -5; make from 4330 steelforging per mil-s-8699; finish SRF1.30
01-394-4022
Structural Component Air Fitting
01-394-4026
Aircraft Stiffener
01-394-4027
Structural Component Air Fitting
Hinge assembly, used on access door to engine
01-394-4056
Structural Aircraft Panel
6.000" overall length 4.750" overall width matt; steel plate 0.750 in. thk, 4130 per mil-s-18729, cond n. cadmium surface treated
01-394-4061
Structural Aircraft Panel
Used on mh-60g helicopter. 5.000" overall length 4.560" overall width pan-cargo door BL39.120; materal steel plate .750 thick, 4130 cond n; heat treat 180, 000psi min ts rockwell 39-43 per mil-h-6875; cadmium plate per qq-p-416, cl 2 type 2 then one coat epoxy primer
