Cessna: 210E; Cracked Main Gear Saddles; ATA 3211

Cessna: 210E; Cracked Main Gear Saddles; ATA 3211

The submitter states, “(I) replaced both main landing gear saddles (P/N 1241423-1 and -2) at annual inspection.
Both were found to have hair line cracks in the radius above the inboard U-bolt hole by using the dye-penetrant inspection method.”

Part Total Time: 1,400.0 hours.

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