00-035-2042
Aircraft Door
00-035-2054
Aircraft Former
00-035-2076
Structural Component Air Support
00-035-2081
Movable Canopy
00-035-2136
Aircraft Windshield Panel
Used on c-130 aircraft. 24.602" overall length 21.850" overall width 30 holes along outer edge, 0.309 min dia, 0.317 max dia, laminated
00-035-2140
Structural Component Air Support
Used on acft model c130. ec/o support 1 ea p/n 337470-3, fitting 1 ea p/n 337331-4, bushing 1 ea p/n 348349, washer 1 ea p/n MS20002C8, fitting 1 ea p/n NAS516-1, nut 1 ea p/n 2752-080, bolt 1 ea p/n MS20008-10, used on ramp hinge
00-035-2152
Aircraft Window Panel
35 holes along outer edge 0.309 in. min, 0.317 in. max dia
00-035-2153
Aircraft Window Panel
Used on c-10 aircraft. glass, laminated as per ler 2-6265 fscm 98897, 35 holes along outeredge 0.309 in. min, 0.317 in. max dia
00-035-2154
Aircraft Windshield Panel
00-035-2184
Structural Aircraft Plate
Used on acft model c-130.
00-035-2370
Wing Landing Flap
Used on aircraft model t28.
00-035-2382
Structural Component Air Fitting
Bushing insert
00-035-2386
Structural Component Air Support
3.718" overall length 2.999" overall width
00-035-2387
Structural Component Air Support
3.718" overall length 2.999" overall width
00-035-2409
Structural Component Air Bracket
00-035-2410
Structural Component Air Bracket
00-035-2437
Aircraft Door
Used on model t28 acft.
00-035-2704
Structural Component Air Support
00-035-2705
Structural Component Air Support
Aluminum alloy
00-035-3012
Structural Component Air Support
30.120" overall length
00-035-3301
Structural Component Air Support
5.716" overall length
00-035-3401
Access Aircraft Door
Used on f-86 aircraft. door assembly, fuselage
00-035-3878
Aircraft Door
Used on F-100.
00-035-3881
Structural Component Air Support
2.906" overall length 0.906" overall width
00-035-4010
Aircraft Leading Edge
00-035-4031
Structural Aircraft Plate
2.250" overall length 1.688" overall width 0.188" material thickness
00-035-4032
Structural Aircraft Plate
2.250" overall length 1.688" overall width 0.188" material thickness
00-035-4034
Aircraft Fairing
00-035-4044
Aircraft Fairing
00-035-4463
Aircraft Window Panel
19.188" overall length 8.844" overall width shade 2082
00-035-4464
Aircraft Window Panel
Used on c-123 cargo airplane. 19.188" overall length 8.844" overall width 3.688 in. corner radius
00-035-5677
Structural Component Air Bracket
00-036-8254
Aircraft Skin
00-036-8255
Aircraft Skin
00-036-8258
Fuselage Aircraft Panel
Aluminum alloy, left hand
00-036-8267
Structural Component Air Fitting
11.720" overall length 3.700" overall width
00-036-8279
Structural Component Air Fitting
00-037-0893
Structural Aircraft Plate
Aluminum alloy 7075-T73511, mcdonnel material specification mms 158
00-037-0954
Cowling
29.812" overall length
00-037-1082
Exhaust Pipe
Used on acft model c-118.
00-037-1186
Attachment Molded Tank Flange
Used on t-33 aircraft. 0.270" hole diameter
00-037-1189
Attachment Molded Tank Flange
00-037-1492
Exhaust Pipe
Used on hu-16 aircraft.
00-037-1495
Exhaust Pipe
Used on HU-16. steel, corrosion resistant per mil-t-8606; 2.625 in od, 0.049 in wall
00-037-1712
Structural Component Air Fitting
1.125" overall length
00-038-0844
Aircraft Elevator
00-038-0860
Aircraft Door
00-038-0863
Fuselage Aircraft Fairing
00-038-0874
Fuselage Aircraft Fairing
00-038-0876
Aircraft Door
