Ballscrew Assemblies

130 part numbers
4C95016-129E NSN 1680-00-003-0866 Cross Reference: 5901-129E
  • supp criticality code justification
4C95016-127E NSN 1680-00-003-0867 Cross Reference: 5901-127E
  • supp criticality code justification
4C95016-135D NSN 1680-00-008-3929 Cross Reference: 5901-135D
  • supp criticality code justification
4C95016-133D NSN 1680-00-008-3930 Cross Reference: 5901-133D
  • supp criticality code justification
4C95016-131D NSN 1680-00-008-3931 Cross Reference: 5901-131D
  • supp criticality code justification
4C95016-125E NSN 1680-00-008-3932 Cross Reference: 5901-125E
  • supp criticality code justification
R532M28-111 NSN 1680-00-076-3982
  • t.o. 8d1-8-204-3, figure 4 special features
104021-01 NSN 1680-00-098-2366 Cross Reference: 562L, 562L1, 94512-01
  • t.o. 16g3-2-3-13, figure 5 special features
457EA8 NSN 1680-00-135-5397
  • t.o. 16a1-13-16-3 special features
5702702 NSN 1680-00-195-7103 Cross Reference: 200913701-10
  • trailing edge flap system end application
  • supp criticality code justification
  • aircraft accessory equipment fsc application data
200913704-10 NSN 1680-00-249-7137 Cross Reference: 5702705, C5A27915
  • trailing edge flap system end application
  • supp criticality code justification
  • aircraft accessory equipment fsc application data
200913702-10 NSN 1680-00-252-0149 Cross Reference: 5702703, C5A27913
  • trailing edge flap system end application
  • supp criticality code justification
  • aircraft accessory equipment fsc application data
31126-01 NSN 1680-00-347-0394
  • nc-313h and nty-33a aircraft end application
550FV NSN 1680-00-373-5619 Cross Reference: 25-69143-1
  • t.o. 16g3-2-55-3 special features
C5A27916 NSN 1680-00-400-3744 Cross Reference: 200913700-10, 570270-1
  • supp criticality code justification
  • trailing edge flap system fsc application data
4344D1-1 NSN 1680-00-402-6201
  • c-130 aircraft end application
4344D1-2 NSN 1680-00-402-6202
  • c-130 aircraft end application
4C95016-121C NSN 1680-00-412-2739 Cross Reference: 5901-121C
  • supp criticality code justification
4C95016-122D NSN 1680-00-412-2740 Cross Reference: 5901-122D
  • supp criticality code justification
R532M28-41 NSN 1680-00-450-0572 Cross Reference: 32-62015-41
  • t.o. 8d1-8-204-3 special features
200913703-10 Manufacturers Suggested Name - Jackscrew Assembly NSN 1680-00-456-7568 Cross Reference: 5702704, C5A27914
  • trailing edge flap system end application
  • supp criticality code justification
  • aircraft accessory equipment fsc application data
4C95016-123E NSN 1680-00-499-0034 Cross Reference: 5901-123E
  • supp criticality code justification
  • source control dwg no. 4c95016-123e reference number differentiating characteristics
51550-4 NSN 1680-00-575-1595 Cross Reference: 669312-6
  • t.o. 8d1-8-116-3/4 special features
00194-501 NSN 1680-00-601-1806 Cross Reference: 00194
  • t.o. 16g3-2-42-3 fsc application data
00165-501 NSN 1680-00-603-6394 Cross Reference: 10-987-14
  • t.o. 16g3-2-42-3 fsc application data