00-888-8190
Aircraft Window Panel
00-888-8316
Attachment Molded Tank Flange
0.280" hole diameter
00-888-8321
Attachment Molded Tank Flange
00-888-8325
Attachment Molded Tank Flange
0.281" hole diameter
00-888-8326
Attachment Molded Tank Flange
0.281" hole diameter
00-888-8328
Attachment Molded Tank Flange
0.281" hole diameter
00-888-8329
Attachment Molded Tank Flange
0.281" hole diameter
00-888-8333
Attachment Molded Tank Flange
0.281" hole diameter
00-888-8349
Bleed Air Duct Assembly
C/o: sleeves, flanges, & elbow tubes
00-888-9843
Structural Component Air Support
00-888-9850
Structural Aircraft Plate
3.625" overall length 1.580" overall width
00-888-9856
Structural Component Air Support
Used on acft model f111. steel, ams 5355, 17-4ph, 2.920 in. lg, 0.920 in. w, 0.720 in. h, 2 holes 0.312 in. dia, 1 hole 0.437 in. dia
00-888-9989
Aircraft Fairing
00-888-9990
Aircraft Fairing
00-889-1500
Aircraft Fairing
Fairing, aluminum alloy, qq-a-250/5 temper 0 composition 2024, filler, aluminum alloy, qq-a-250/5 temper T3 composition 2024
00-889-1512
Aircraft Fairing
Used on oh-58a,c hel.
00-889-9334
Aircraft Door
00-889-9340
Structural Component Air Support
Used on acft model c-5. used as fitting on slat actuator door
00-889-9345
Structural Component Air Support
Used on acft model c-5. casting, al alloy, A356-T6 per mil-a-21180; 3.200 in. lg, 0.860 in. w, 0.330 in. thk; used as fitting on slat actuator door
00-889-9347
Structural Component Air Support
Used on acft model c-5. casting per MIL21180 class x /A356-T6/
00-889-9375
Structural Component Air Support
Used on acft model c-5. steel per mil-s-18729 condition n, 4.000 in. lg, 2.000 in. w, 0.190 in. thk
00-889-9376
Structural Component Air Support
Used on acft model c-5. steel per mil-s-18729 condition n, 4.000 in. lg, 2.000 in. w, 0.375 in. thk
00-889-9427
Structural Component Air Support
Used on acft model c-5. oal alloy 7075-T651 per qq-a-250/12, T651 temper; 3.130 in. lg, 1.820 in. w, 2.080 in. h; six 0.263 in. dia mounting holes; two 0.377 in. through holes inline; used on outboard hinge, nose landing gear aft fixed fairing
00-890-0404
Access Aircraft Door
Primer surface treated
00-890-2795
Structural Component Air Support
Aluminum alloy, ww-t-700/6 6061-T6
00-890-3625
Structural Component Air Support
Used on acft model c-5. material D6ac per manufacturers spec STM05-500, heat treatment to 220-240 ksi; 9.560 in. lg, 6.040 in. o/a w, 0.670 in. o/a thk; opposite p/n 4F53811-102a
00-890-3632
Structural Component Air Support
Used on acft model c-5. material D6ac per manufacturers spec STM05-500, heat treatment to 220-240 ksi; 9.560 in. lg, 6.040 in. o/a w, 0.670 in. o/a thk; opposite p/n 4F53811-101a
00-890-3636
Structural Component Air Support
Used on acft model c-5. ial alloy 7075-T651 per qq-a-250/12; 2.880 in. o/a lg, 2.450 in. w, 0.150 in. base thk widing to 0.300 at bearing seat; contains 7 0.206 in. dia mounting holes; c/o 1 fitting
00-890-3637
Structural Component Air Support
Used on c-5 aircraft. used as fitting, hing slanted slot door fuselage station 1274.26
00-890-3638
Structural Component Air Support
Used on c-5 aircraft. used as fitting on hinge slanted slot door fuselage station 1274.26
00-890-3661
Structural Component Air Support
Used on acft model c-5. made from lockheed stock LS34695-1; 3.700 in. lg, 2.530 in. w tapering to 1.500 in. other end; 0.510 in. o/a thk, .440 in.thk from wide end in 2.090 in.; 0.810 in. w slot along center of lg, flanged upper surface with 3 circular 0.790 in. dia notches cut into flanges; 4 0.202 in. dia holes couter bored to 0.480 in.; used on troop seat tie down fitting
00-890-3700
Access Aircraft Door
00-890-3702
Aircraft Door
Core data, aluminum foil honeycomb, 8.1-5052-H39 per qq-a-250/8 cls 1
00-890-3703
Aircraft Door
Used on F-5. core data, aluminum honeycomb, 8.1-5052-H39 per qq-a-250/8 class 1
00-890-3705
Metal Molding
00-890-3718
Bell Crank
Used on c-5 aircraft. 0.565" bore diameter flat, raised face arm end hole
00-890-3911
Structural Component Air Support
Used on acft model f4. steel, 4340, cond e, mil-s-5000, 9.500 in. lg, 0.015 in. thk
00-890-3935
Structural Component Air Support
00-890-4070
Fluid Aircraft Manifold
2.577" overall length 2.225" overall width
00-890-4075
Structural Component Air Support
Used on aircraft model f111. aluminum alloy, AMSJ260
00-890-4131
Structural Component Air Bracket
C/o 1 welded tube assy, 1 gasket, 2 bushings
00-890-4138
Access Aircraft Door
00-890-4139
Fuel Aircraft Tank
Self-sealing, 50 gal capacity cell
00-890-4162
Aircraft Window Panel
00-890-4164
Access Aircraft Door
00-890-4169
Aircraft Window Panel
00-890-6164
Radome
79.485" overall length
00-890-8340
Aircraft Door
