01-166-1203
Structural Component Air Support
Used on f-5 acft. location-lower horizontal stabilizer, output quadrant, fuselage station 475.000; matl-magnesium casting AZ91c-T6 per qq-m-56
01-166-1204
Structural Component Air Support
Used on c-5a acft. matl cast per ams 5355; includes bearing MS21240-06C11; opposite to p/n 4F54537-102; used as bracket, pivot-limit switch, side aft cargo door
01-166-1206
Structural Component Air Support
Used on kc-135 aircraft. opposite -1; material-7075-T6 extr per qq-a-277; altered bac 1519.87 x 1.60; used on control tab, elevator
01-166-1207
Structural Component Air Support
Used on b1-b aircraft.
01-166-1208
Structural Component Air Support
Used on b1-b aircraft.
01-166-1210
Structural Component Air Support
Used on acft model b-1b.
01-166-1213
Structural Component Air Support
Used on acft model b-1b. c/o plate 1 ea p/n L5338385-003, tube 1 ea p/n L5338385-005, plate 1 ea p/n L5338385-007, used on temp sensor, fwd rh side
01-166-1215
Structural Component Air Support
Used on h-53 acft. matl al alloy, qq-a-250/11, 6061-T6; 3.750 in. lg; 2.250 in. w; 6 holes 0.500 in. dia; used as shim, pylon block used for proper fit w/p/n 2191-094-3, tank
01-166-1216
Structural Component Air Support
Used on h-53 acft. matl al alloy, qq-a-250/11, 6061-T6; 4.000 in. lg; 6 holes along lg, 0.375 in. dia; 0.920 in. w; used as lug, pylon w/shim p/n 2191-094 for proper fit with tank
01-166-1217
Structural Component Air Support
Used on h-53 acft. matl st, qq-s-766, 304 sst; 1.130 in. w; 2.000 in. lg; 0.625 in. dia; used as retainer, lanyard a part of tank assy
01-166-1266
Aircraft Tip
Nuclear hardness critical item; c/o 1 skin, 1 cover, 1 trailing edge, 1 leading edge, 1 filler, 1 closeout, 4 retainer tips
01-166-1267
Aircraft Tip
Nuclear hardness critical item; c/o 1 skin, 1 cover, 1 trailing edge, 1 leading edge, 1 filler, 1 closeout, 4 retainer tips
01-166-1279
Aircraft Door
01-166-2400
Access Aircraft Door
Used on acft model b-1b.
01-166-2477
Aircraft Fairing
10.000" overall length 6.000" overall width 0.040" material thickness
01-166-2478
Structural Component Air Support
Used on c-5 acft. matl al alloy, qq-a-250/4, 2024-T3; matl size 0.040 by 3.000 by 6.000 in. lg; includes bracket p/n 4P33117-703a
01-166-2479
Structural Component Air Support
Used on acft model b52g. used on arc-190 mount
01-166-2480
Structural Component Air Support
Used on acft model b52. c/o 86 component parts
01-166-2485
Structural Component Air Support
Used on f-15 acft. function-actuator, support; location-canopy lock
01-166-2486
Structural Component Air Support
Used on f-15 acft. function-actuator support; location-ejection seat; matl-7075-T7351 aluminum alloy per mms-159 cond T7351; dim.-4.650 in. lg, 4.620 in. w, 1.250 in. thk; supercedes 68A311242-2006
01-166-2487
Structural Component Air Support
Used on f-15 acft. location-forward fuselage section
01-166-2488
Structural Component Air Support
Used on f-15 acft. function-actuator support, left side; location-ejection seat; matl-aluminum alloy, 7075-T7351, per mms-159 cond T7351; dim.-4.650 in. lg, 4.500 in. w, 1.250 in. thk
01-166-2489
Structural Component Air Support
Used on f-15 acft. function-actuator support, left hand; location-ejection seat; matl-7075-T7351 aluminum alloy per mms-159 cond T7351; dim.-4.650 in. lg, 4.620 in. w, 1.250 in. thk; supercedes 68A311242-2005
01-166-2490
Structural Component Air Support
Used on f-15 acft. location-ejection seat; function-actuator support, right hand; matl-aluminum alloy, 7075-T7351, per mms-159 cond T7351; dim.-4.650 in. lg, 4.500 in. w, 1.250 in. thk
01-166-2495
Aircraft Former
24.000" overall length 3.000" overall width 0.040" material thickness finish f-10.10; nha 5-85653-1/-52
01-166-2497
Longeron
Used on F-15. supercedes 68A312025-2005
01-166-2499
Longeron
Used on F-15. supercedes 68A312019-2055
01-166-2500
Airfoil Rib
22.240" overall length
01-166-2501
Airfoil Rib
22.240" overall length
01-166-3286
Access Aircraft Door
Used on av-8b acft.
01-166-3287
Access Aircraft Door
Used on av-8b acft.
01-166-3331
Fluid Aircraft Manifold
8.790" overall length
01-166-3459
Fluid Aircraft Manifold
Used on aircraft, hornet f/a-18.
01-166-4173
Structural Component Air Support
Used on c-5 acft. matl al alloy, qq-a-250/13, 7075-0 clad; used on fwd fairing assy, pylon
01-166-4174
Structural Component Air Support
Used on acft model f-16. unalloyed commercially pure titanium bar forging per mil-t-9047 comp. 1
01-166-4175
Structural Component Air Support
Used on acft model b-1b. c/o duct 1 ea p/n L5338303-003, flange 1 ea p/n L5338303-005, used on avionics return air, rh, located at yf 263.00
01-166-4176
Structural Component Air Support
Used on acft model f-111.
01-166-4274
Fluid Aircraft Manifold
42.040" overall length
01-166-4275
Fluid Aircraft Manifold
42.040" overall length
01-166-4276
Fluid Aircraft Manifold
8.860" overall length
01-166-4558
Access Aircraft Door
Used on aircraft model f-18.
01-166-4559
Access Aircraft Door
01-166-4880
Aircraft Fairing
Used on aircraft,model sh-60b.
01-166-4906
Fuel Aircraft Tank
Used on model sh-60b acft.
01-166-5014
Attachment Molded Tank Flange
Used on aircraft model fd-18.
01-166-5015
Attachment Molded Tank Flange
Used on model f-18 acft.
01-166-5369
Filler Opening Cap
3a thread class 1.380" outside diameter anodize surface treated unf thread series
01-166-7260
Aircraft Door
