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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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