Aviation Rod End Clevis

57 part numbers
MS21253-4RL NSN 1640-00-068-2016 Cross Reference: MS21253
  • 3a rod connection thread class
  • right-hand rod connection thread direction
  • between 0.745 inches and 0.750 inches shank length
  • between 0.189 inches and 0.195 inches shank diameter
  • between 0.745 inches and 0.760 inches overall width
204-011-179-1 NSN 1640-00-157-7846 Cross Reference: 204-011-179-001
  • 3b rod connection thread class
  • right-hand rod connection thread direction
  • 1.500 inches rod connection thread length
  • between 1.940 inches and 2.000 inches shank diameter
  • between 2.950 inches and 2.960 inches overall width
10052646 Rod End (inavy): Clevis NSN 1640-01-481-6392
  • agav criticality code justification
5HP41804-105 NSN 1640-01-487-9367
5HP41804-107 NSN 1640-01-487-9370
70400-26638-102 NSN 1640-01-505-0757 Cross Reference: 70400-26638
70400-26638-103 NSN 1640-01-505-0758 Cross Reference: 70400-26638
414C3409-2 NSN 1640-01-510-3922
  • 1520-01-088-3669: t.m.1520-240-23p end application
MBEU148651 Inavy-fork End NSN 1640-01-515-5314
  • 2b rod end thread class
  • right-hand rod end thread direction
  • 0.375 inches rod end thread length
  • 0.782 inches shank length
  • 0.189 inches hole diameter
66-11872-2 NSN 1640-01-517-8700
  • boeing 707 end application
  • clevis style designator
66-11872-1 NSN 1640-01-517-8701
  • boeing 707 end application
  • clevis style designator
66-10235-3 NSN 1640-01-517-8704
  • boeing 707 end application
  • clevis style designator
BM53-1761-0163 NSN 1640-01-521-4485
  • 2a thread class
  • right-hand thread direction
  • 0.462 inches shank thread length
  • 0.281 inches hole diameter
  • 0.400 inches shank diameter
385035-1 NSN 1640-01-522-1158
3352973-1 NSN 1640-01-525-1387
  • hercules c130j aircraft end application
901-060-767-102 Aft Nacelle Door Clevis-strut NSN 1640-01-530-2588
  • v22 aircraft end application
  • feat criticality code justification
  • aluminum alloy material
2805142-1 NSN 1640-01-531-4082
61340-00 Clevis NSN 1640-01-531-6963
  • piper cub aircraft end application
901-031-723-137 (inavy) Clevis Assembly NSN 1640-01-532-2816
  • mv-22 aircraft end application
  • feat criticality code justification
70400-02255-101 NSN 1640-01-535-4151 Cross Reference: 70400-02255
  • uh60-m,-152-0014 end application
B94815-001 Aircraft Tailstock Assembly; Inavy: Tailstock Assy NSN 1640-01-538-6110
  • 0.825 inches hole diameter
  • round hole shape
  • titanium alloy material
14-1136-001 NSN 1640-01-539-5807
1536019-103 NSN 1640-01-540-6216
A02S8133-201 Support Latch (inavy) Clevis NSN 1640-01-547-1636
  • h46 platform assembly end application
10221-00 NSN 1640-01-548-7832
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