01-208-0457
Aircraft Floor
Used on helicopter model sh-60b.
01-208-0460
Fuel Aircraft Tank
Used on aircraft model c-130.
01-208-0690
Structural Aircraft Plate
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 2024 qq-a-250/5, T0; 0.040 in. matl thk by 5.700 in. w by 6.500 in. lg; u cross section; fitting mtg hole; left appl; w/o river holes
01-208-0691
Structural Aircraft Plate
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 2024 qq-a-250/5, to; 0.040 in. matl thk by 5.700 in. w by 6.500 in. lg; u cross section; fitting mtg hole; right appl; w/o rivet holes
01-208-0692
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 7075 qq-a-250/13, to; 0.063 in. matl thk by 6.000 in. w by 18.000 in. lg; bowed shape; u cross section, w/o rivet holes; left hand appl
01-208-0693
Structural Component Air Support
Used on 1520-00-859-2670. aluminum alloy 7049 AMS4136 T6-11; 0.156 in. matl thk by 5.750 in. lg; l cross section; leg lg 1.250 in; prebent; w/o holes
01-208-0694
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 2024 qq-a-250/5, to; 0.032 in. matl thk by 2.400 in. w by 8.000 in. lg; bow shape; l cross section; w/o holes
01-208-0695
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 2024 qq-a-200/3, T4; 0.063 in. matl thk; base flange 1.250 in. w; left flange 1.000 in. w; 12.200 in. o/a lg; l cross section; w/o rivet holes
01-208-0696
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 2024 qq-a-200/3, T4; 0.063 in. matl thk; base flange 1.250 in. w; left flange 1.000 in. w; 12.500 in. o/a lg; l cross section; w/o rivet holes
01-208-0697
Aircraft Former
01-208-0698
Aircraft Former
01-208-0699
Boom Stringer
Used on 1520-00-859-2670. 30.500" overall length 2.400" overall width 0.032" material thickness bow shape; l cross section; w/o rivet holes
01-208-0853
Access Aircraft Door
Used on acft model kc-135. nha 458-52074
01-208-0977
Aircraft Leading Edge
55.000" overall length 10.500" overall width 3.500" material thickness nha L3226021
01-208-0998
Structural Aircraft Plate
Used on c-5a aircraft. matl 2024-T3 alclad per qq-a-250/5 temper-T3; size .040X3.0X4.0; nha 4L10006
01-208-0999
Structural Aircraft Plate
81.000" overall length
01-208-1000
Structural Aircraft Plate
01-208-1001
Structural Aircraft Plate
01-208-1003
Structural Component Air Fitting
C/o 1 plate, 1 fitting, 1 bracket assy, 4 nut, 8 washer, 4 screw; part of -105b
01-208-1004
Structural Component Air Support
0.050" material thickness acrylonitrile butadiene styrene
01-208-1005
Structural Component Air Support
Used on c-5a aircraft. part of -101a beam assembly-upper, outbd pylon; nha 4P52040; opposite -110a; matl size LS10136-2407-5X2; seal assembly to a fluid tight condition per STP56-107 using STM40-111 or STM40-112 sealant
01-208-1006
Structural Component Air Support
Used on c-5a acft. bracket, indicator-indicator mechanism, cargo ramp lock
01-208-1012
Structural Aircraft Panel
01-208-1013
Structural Aircraft Panel
01-208-1014
Structural Aircraft Panel
01-208-1015
Structural Aircraft Panel
01-208-1016
Structural Aircraft Panel
01-208-1017
Structural Aircraft Panel
Liner, right hand side-forward crew station
01-208-2979
Access Aircraft Door
01-208-2980
Access Aircraft Door
Used on acft model b-1b. nuclear hardness critical item; nha L3226667-002; opposite p/n -021; used on fire extinguisher
01-208-2981
Access Aircraft Door
01-208-3187
Structural Component Air Bracket
01-208-3206
Structural Aircraft Plate
Used on 1520-00-859-2670. type/model designation:uh-1d magnesium alloy uns M11914 qq-m-56 alloy AZ91c T6; 21.550 in. o/a lg; right appl; w/o holes, supp: floor plate assy
01-208-3207
Structural Aircraft Plate
Used on 1520-00-859-2670. type/model designation:uh-1d magnesium alloy uns M11914 qq-m-56 alloy AZ91c T6; 21.550 in. o/a lg; left appl; w/o holes
01-208-3208
Structural Aircraft Plate
Nha L3226009
01-208-3209
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 2024 qq-a-250/5, T3; 0.025 in. matl thk by 3.000 in. w by 5.000 in. lg; v cross section; w/o rivet holes
01-208-3210
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 2024 qq-a-250/5, T4; 0.063 in. matl thk; base flange 1.0000 in. lg; left flange 0.750 in. lg; 13.000 in. lg o/a; l cross section; w/o holes; right appl
01-208-3211
Structural Component Air Support
01-208-3212
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy; w/ bushing; w/o holes; left appl
01-208-3213
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy; w/ bushing; w/o holes; right appl
01-208-3214
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy; w/ bushing; w/o holes; left appl
01-208-3215
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy; w/ bushing; w/o holes; right appl
01-208-3216
Structural Component Air Support
Used on acft model b-1b. al alloy bar 2024-T851 per qq-a-225/6; stock size 4.750 in. lg, 2.750 in. w, 2.250 in. thk; opposite p/n -003; nha L5351642-002; located yn 232.50
01-208-3229
Structural Aircraft Panel
01-208-3230
Structural Aircraft Panel
Used on c-5a aircraft. matl size LS32738a; part of -519b floor assembly-flight station
01-208-3231
Structural Aircraft Panel
Used on acft model b-1b. consist of 1 panel, 2 stiffener, 1 spacer, 2 gang channel; opposite p/n -012; located at YN232.500 to YN265.250; nha L3226011
01-208-3232
Structural Aircraft Panel
Used on acft model b-1b. consist of 1 panel, 2 stiffener, 1 spacer, 3 gang channel; opposite p/n -011; nha L3226011; located at YN232.500 to YN265.250
01-208-3239
Aircraft Floor
01-208-3243
Rudder Rib
Used on 1520-00-859-2670. 43.500" overall length 2.500" overall width 0.040" material thickness v cross section; w/o rivet holes
