Model 208; Caravan I; Nose Landing Gear Strut Failure; ATA 3222

Model 208; Caravan I; Nose Landing Gear Strut Failure; ATA 3222

Extracted From:    AC No. 43-16A
    ALERT NO. 309
    April 2004

The aircraft was having recurring shimmy problems, which led to the strut being disassembled for inspection.

During the inspection, the technician discovered the lower plug was separated from the metering pin assembly (P/N 2643018-1). This caused the strut to lose the dampening effect.

Part total time: 11,642 hours.

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