01-234-3470
Stabilizer Aircraft Fairing
Used on aircraft model f-18. laminated kevlar 49 per mms-525, type 2; cognizant service:navy;
01-234-3480
Structural Aircraft Panel
Used on aircraft model f-18.
01-234-3481
Structural Aircraft Panel
Used on aircraft model f-18.
01-234-3482
Structural Aircraft Panel
Used on aircraft model f-18.
01-234-3483
Structural Aircraft Panel
Used on aircraft model f-18.
01-234-3484
Structural Aircraft Panel
Used on aircraft model f-18.
01-234-3485
Structural Aircraft Panel
Used on aircraft model f-18.
01-234-3486
Structural Aircraft Panel
Used on aircraft model f-18.
01-234-4081
Structural Aircraft Plate
Used on F-15.
01-234-4082
Structural Aircraft Plate
01-234-4083
Structural Aircraft Plate
Used on C-130.
01-234-4084
Structural Aircraft Plate
Used on F-15.
01-234-4085
Structural Aircraft Plate
Used on F-15.
01-234-4087
Structural Aircraft Plate
Used on F-15.
01-234-4090
Structural Component Air Support
Used on f-15 acft. p/o inboard shear beam-empennage support beam; fuselage station 712.310 to 791.650
01-234-4107
Aircraft Former
9.000" overall length 8.000" overall width 0.040" material thickness opposite p/n -38l
01-234-4108
Aircraft Former
01-234-4109
Aircraft Former
01-234-4110
Aircraft Former
01-234-4112
Aircraft Skin
Used on F-15.
01-234-4113
Aircraft Stringer
01-234-4114
Aircraft Stringer
01-234-4130
Aircraft Door
Includes mounted antenna S65-8282-34, antenna diplexer sspd-113-14
01-234-4537
Structural Component Air Bracket
Used on sentry f22 aircraft.
01-234-4626
Structural Component Air Support
01-234-4641
Aircraft Skin
01-234-4896
Structural Aircraft Plate
Type/model designation:fms-1, fms-2, fms-3, fms-4 aluminum alloy 6061-T6 qq-a-250/11, matl 0.250 in. thk by 0.625 in. w by 1.578 in. lg
01-234-4897
Structural Aircraft Plate
Type/model designation:fms-1, fms-2, fms-3, fms-4 aluminum alloy 6061-T6 qq-a-250/11, matl 0.250 in. thk by 0.812 in. w by 1.734 in. lg.
01-234-4898
Structural Aircraft Plate
Aluminum alloy 7075-T7351 mms-159 cond-T7351; 2.000 in. thk by 3.125 in. w by 6.000 in. lg
01-234-4899
Structural Component Air Support
Titanium
01-234-4900
Structural Component Air Support
Titanium
01-234-4901
Structural Component Air Support
Titanium
01-234-4902
Structural Component Air Support
Titanium
01-234-4903
Structural Component Air Support
Aluminium alloy 7050-T73651 mms 1420; 4.500 in. thk by 4.250 in. w 12.900 in. lg; bushing 4M139C12-61 3120-01-194-9052
01-234-4904
Structural Component Air Support
Aluminium alloy 7075-T73651 mms-1420; 4.500 in. thk by 4.250 in. w by 12.900 in. lg; bushing 4M139C12-61 3120-01-194-9052
01-234-4905
Structural Component Air Support
Consists of 1 support r/n 76301 75A124322-2001b aluminum 7050-T73651 mms 1420 4.00 x 5.50 x 22.50
01-234-4906
Structural Component Air Support
Cconsists of 4 support r/n 76301 75A124322-2002 -2002a -2002b -2002c 4.000 in. by 5.50 in. by 22.50 in. aluminum 7050-T73651 MMS1420; 1 bearing M81936-1-12; 1 bearing ST4M123-8; 1 fitting NAS516-1
01-234-4907
Structural Component Air Support
Cconsists of 1 support r/n 76301 75A124332-2003 aluminum 7050-T73651 MMS1420; 3.000 in. by 3.500 in. by 14.000; 1 bearing MS27645-3a; 1 bearing M81936-1-5; 1 bearing ST4M123-8; 1 fitting NAS516-1a
01-234-4908
Structural Component Air Support
Gconsists of 1 support r/n 76301 75A124332-2004 aluminum 7050-T73651 MMS1420; 3.000 in. by 3.500 in. by 14.000 in.; 1 bearing MS27645-3a; 1 bearing M81936-1-5; 1 bearing ST4M123-8; 1 fitting NAS516-1a
01-234-4909
Structural Component Air Support
Consists of 1 support r/n 76301 75A124342-2001 6al-4v 2.75 in. by 3.50 in. by 6.75 in.; 1 support 6al-4v 76301 75A124342-2001a 3.000 in. by 3.500 in. by 6.750 in. mil-t-9046 TY3 cond annealed; 75B120056-2001 bushing 9M187-81 ring retaining 2 each; 2 bushings p/n 75B120056-2003
01-234-4910
Structural Component Air Support
6al-4v mil-t-9046 cond anld; 2 holes 0.1900 in. dia plus 0.0030 in. 0.500 in. dia porm 0.03 0.01 in. by 0.060 in. c-bore; 1 hole 0.250 in. plus 0.006 in. 0.500 in. dia porm 0.03 in. 0.01 in. by 0.060 in. c-bore; 2.883 in. c to c distance between bottom holes; 2.975 in. c to c distance between holes on side; 0.188 in. thk
01-234-4911
Structural Component Air Support
Consists of 1 support r/n 76301 75A124342-2002 6al-4v 2.75 in. by 3.50 in. by 6.75 in.; 1 support -2002a 6al-4v mil-t-9046 TY3 cond anlg 3.000 in. by 3.500 in. by 6.750 in.; 75B120056-2001 bushing 2; 2 9M187-81 rings; 75B120056-2003/2001 2 bushings ea; 75B120056-9001 1 bushing
01-234-4912
Structural Component Air Support
Consists of 1 support r/n 76301 75A124352-2003 aluminum 7050-T73651 MMS1420 4.500 in. by 5.000 in. by 11.000 in; 1 bearing ST4M123-8; 2 bushings ST4M139CP12-28; 1 pin NAS561C10-22
01-234-4913
Structural Component Air Support
Al aly 2024-0 qq-a-250/5; 0.100 in. thk; 7.82 in. wide; 12.75 in. lg
01-234-4926
Structural Aircraft Panel
35.391" overall length 17.500" overall width
01-234-4927
Structural Aircraft Panel
35.391" overall length 12.000" overall width
01-234-4928
Structural Aircraft Panel
35.391" overall length 12.000" overall width
01-234-4939
Aircraft Former
Used on aircraft f-18. 47.141" overall length 15.250" overall width 2.500" material thickness
01-234-4943
Aircraft Skin
66.000" overall length 7.000" overall width
01-234-4944
Aircraft Skin
82.000" overall length 7.000" overall width
