Metal Moldings

151 part numbers
50-430015-1081 NSN 1680-00-034-5936
  • specific length issue form
  • aluminum alloy, comp 2024, t4 special features
  • aluminum alloy, comp 2024, t4 material
  • prime and paint per bs20686a, fscm 70898 surface treatment
  • fuselage sect., acft fsc application data
5113649 NSN 1680-00-122-5102
  • c-47 end application
762439 NSN 1680-00-473-9779 Cross Reference: 762439-9
  • f-104g end application
1514020-28-793 NSN 1680-00-482-4645
  • aluminum alloy material
  • aluminum alloy material
  • incl hook strip to assure positive fastening supplementary features
  • used on rh windshield, 02a acft fsc application data
371665-1 NSN 1680-00-611-7041
  • rolled fabrication method
  • 73.380 inches length
  • specific length issue form
  • aluminum alloy material
  • aluminum alloy material
4W71033-102A NSN 1680-01-116-6984
  • extruded fabrication method
  • 28.000 inches length
  • 1.359 inches attachment feature width
  • 15.400 inches attachment feature height
  • 0.080 inches exposure width
1330W10P005 NSN 1680-01-150-9162
  • aluminum material
  • aluminum alloy material
  • indicator, elect p/n 8dj215wba1, 6620011297247 fsc application data
39-8892-5 NSN 1680-01-162-6705
  • 2.000 inches length
  • specific length issue form
  • aluminum alloy material
  • trailing edge fairing, b-52 acft fsc application data
39-8892-503 NSN 1680-01-162-7648
  • 2.300 inches length
  • specific length issue form
  • aluminum alloy material
  • trailing edge, fairing, b-52 acft fsc application data
39-8892-801 NSN 1680-01-162-7649
  • 1.700 inches length
  • specific length issue form
  • aluminum alloy material
  • trailing edge fairing, b-52 acft fsc application data
39-8892-802 NSN 1680-01-162-7650
  • 1.900 inches length
  • specific length issue form
  • aluminum alloy material
  • trailing edge fairing, b-52 acft fsc application data
65-5998-10383AW NSN 1680-01-221-9286 Cross Reference: 65-5998-383AW
  • aircraft model e-3a special features
65-2497-20 NSN 1680-01-273-3149
40235003 NSN 1680-01-315-9712
  • extruded fabrication method
  • 5.472 inches length
  • 5.035 inches attachment feature width
  • 2.158 inches material accommodated thickness
  • screw mounting method
40235001 NSN 1680-01-324-0753
  • extruded fabrication method
  • 5.730 inches length
  • 5.255 inches attachment feature width
  • 1.996 inches material accommodated thickness
  • screw mounting method
40235002 NSN 1680-01-324-5187
  • extruded fabrication method
  • 5.730 inches length
  • 5.255 inches attachment feature width
  • 1.996 inches material accommodated thickness
  • screw mounting method
75A320902-2037 NSN 1680-01-331-2054
65-6180-15 NSN 1680-01-331-6768
  • extruded fabrication method
  • e-3 aircraft end application
  • sheet metal screw mounting method
  • specific length issue form
  • trim, pan installation special features
65-6180-7 NSN 1680-01-331-6769
  • extruded fabrication method
  • e-3 aircraft end application
  • sheet metal screw mounting method
  • specific length issue form
  • trim, pan installation special features
1207668-102 NSN 1680-01-334-5074
  • s-3b aircraft end application
  • any acceptable mounting method
1612566-105H48 NSN 1680-01-336-4360
1612566-106H48 NSN 1680-01-336-4361
501450-513 NSN 1680-01-338-9177
70205-40032 NSN 1680-01-341-7683
70207-24001-111 NSN 1680-01-349-6704
  • material thk. 0.015 special features
  • aluminum alloy material
  • aluminum alloy material