01-044-0450
Structural Component Air Support
Used on acft model f-16.
01-044-0451
Structural Component Air Support
Used on acft model f-16. consists of casting 1 ea., pn.16S147-7
01-044-0452
Structural Component Air Support
Used for fuel sys, ctr fuselage
01-044-1715
Structural Component Air Bracket
01-044-1716
Structural Component Air Bracket
01-044-1721
Structural Aircraft Plate
2.210" overall length 1.500" overall width 0.610" material thickness
01-044-1789
Aircraft Former
Yframe assembly; c/o -43 shim 2.6 x 2 in.; p/n 16T7304-15 spar; p/n 16T7305-19
01-044-1871
Radome
Used on acft model f4e.
01-044-3250
Elevator Balance Weight
Used on acft kc-135. high density tungsten alloy fansteel no.77; 6.700 in. lg,
01-044-3251
Aircraft Window Panel
01-044-4325
Structural Component Air Support
01-044-4986
Structural Component Air Support
C/o: 1 casting, p/n 16S149-7
01-044-5055
Fluid Aircraft Manifold
45.980" overall length 3.000" overall width
01-044-6106
Aircraft Stiffener
01-044-6107
Aircraft Stiffener
01-044-6231
Structural Aircraft Plate
Used on acft model f-16a/b. consist of 1 plate, 4 bushing; eff 0001 on; nha 16M030-3
01-044-6233
Aircraft Fairing
Used on aircraft,f-106.
01-044-6237
Structural Component Air Support
Used on acft model f-16a/b usaf. alum.alloy, per.ams 4218-T6, consists of support 1 ea.pn.16P175-9, insert 2 ea.pn.MS21209F1-15; nha 16P009-1; eff 0001-on
01-044-6238
Structural Component Air Support
Used on acft model f-16a/b usaf. alum.alloy, per.ams 4218-T6, consists of support 1 ea.pn.16P175-10, insert 2 ea.pn.MS21209F1-15; eff 0001-on; nha 16P009-1
01-044-6247
Aircraft Skin
Used on kc-135 acft.
01-044-6927
Structural Component Air Support
01-044-6935
Aircraft Stringer
Used on acft model f-4.
01-044-7141
Fuel Aircraft Tank
52.330" overall length 34.500" overall width
01-044-7692
Aircraft Frame
31.620" overall length 12.040" overall width 0.063" material thickness matl:steel; MMS155CL1
01-044-7693
Aircraft Skin
30.700" overall length 11.850" overall width
01-044-7805
Structural Component Air Support
C/o: 1 support (16W350-11) & 1 bearing (MS14103-6)
01-044-9347
Aircraft Former
Frame; stock size-.063 x 12 x 20 in; finish A403; nha 16T7241-5; eff 0002 on
01-044-9348
Aircraft Former
20.000" overall length 13.000" overall width 0.063" material thickness superseding p/n 16T7241-47, i/c code ni, ecn 33179, nha p/n 16T7241-803, finish A403
01-044-9794
Structural Component Air Support
Aluminum alloy AMS4260, temper T6, 3.800 in. lg, 3.620 in. w, 2.100 in. h
01-044-9865
Aircraft Elevator
Aluminum alloy qq-a-250/5;
01-045-0351
Aircraft Speed Brake
35.794" overall length 14.750" overall width 0.080" material thickness lower speed brake door assembly
01-045-0352
Aircraft Speed Brake
35.794" overall length 14.750" overall width 0.080" material thickness lower speed brake door assembly
01-045-0366
Access Aircraft Door
Used on acft model f-16a/b usaf.
01-045-0380
Aircraft Hinge
01-045-0408
Structural Aircraft Plate
Used on acft model f-16a/b. alum alloy per qq-a-250/4-T1; 0.063 in. thick, 3.000 in. wide, 3.000 in. long; located at fuselage section 224.00; nha 16B4221-2; eff 0001 on
01-045-0409
Structural Aircraft Plate
Used on acft model f-16a/b usaf. nha 16B410-67; eff on 0004-on
01-045-0410
Structural Aircraft Plate
Eff on 0008-on; nha 16B410-77
01-045-0411
Structural Component Air Support
Used on acft model f-16a,b. nha 16H800-1
01-045-0412
Structural Component Air Support
Used on acft model f-16a,b. nha 16H800-1
01-045-0429
Aircraft Skin
Used on f-16a aircraft. c/o sealant per fms-1044-5, -25 plate 0.100X9X12, -49 skin 0.100 x 55 x 66, -53 plate .100 X5.6X5, -57 skin .100 x 55 x 66; material of skins
01-045-0878
Aircraft Former
Used on F-4. used as stiffener
01-045-0882
Aircraft Pylon
9.000" overall length 1.500" overall width 0.050" material thickness c/o relay panel/elec wiring
01-045-0883
Aircraft Pylon
9.000" overall length 1.500" overall width 0.050" material thickness c/o relay panel/elec wiring
01-045-0884
Aircraft Pylon
9.000" overall length 1.500" overall width 0.050" material thickness c/o relay panel/elec wiring
01-045-0885
Aircraft Pylon
9.000" overall length 1.500" overall width 0.050" material thickness
01-045-0886
Aircraft Pylon
9.000" overall length 1.500" overall width 0.050" material thickness c/o relay panels, elec wiring
01-045-0887
Aircraft Pylon
9.000" overall length 1.500" overall width 0.050" material thickness c/o relay panels, elec wiring
01-045-0891
Structural Component Air Bracket
01-045-0983
Structural Aircraft Plate
Used on acft model no. c-5a. aluminum 7075-T6, qq-a-250/12, 14.000 in. lg, 4.000 in. w, 0.060 in. thk
01-045-0984
Structural Aircraft Plate
Used on acft model no. c-5a. aluminum 7075-T6, qq-a-250/12, 14.000 in. lg, 4.000 in. w, 0.060 in. thk
