Service difficulty report · Gust Lock · Cessna 208

Difficulty date
July 12, 2014
Submitted
August 22, 2014
Operation
General aviation
Aircraft
N188SF
Make and model
Cessna 208
Aircraft serial
208000551
Aircraft time
230 hours
Part
Gust Lock
Part number
ATRL1020
Condition
Damaged
Location
Rudder
Part time
230 hours, 1 cycles
Stage of operation
CL
How discovered
O
Nature of condition
F
Precautionary procedure
A

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

RUDDER GUST LOCK TUBE ASSY SHEARED IN FLIGHT AND CAUSED A MALFUNCTION IN THE FLIGHT CONTROL/RUDDER SYS. PILOT STATED HE HAD TO USE EXCESSIVE FORCE TO MOVE THE YOKE AFT OF ITS NEUTRAL POSITION. UPON LANDING THE ACFT, THE AIRCRAFT WAS INSPECTED AND THE RUDDER GUST LOCK TUBE ASSY WAS FOUND TO BE BROKEN AND SEVERELY CORRODED. IT IS SUSPECTED THAT FATIGUE CORROSION CAUSED THIS FAILURE, DUE TO THE FACT THAT THE ACFT HAD BEEN OPERATING AS A "SEA PLANE", IN A SALT WATER LADEN ENVIRONMENT. IT IS INTERESTING TO NOTE THE ACFT IS PRACTICALLY BRAND NEW AND ONLY HAS APPROXIMATELY 230.2 TOTAL AIRFRAME HOURS TSN. THIS OFFICE RECOMMENDS FOR THE FAA TO MANDATE A "ONE TIME" INSPECTION OF THIS ACFT PART FOR CORROSION, IN AN EMERGENCY AD ACTION, THEN HAVE THIS PART BE INSPECTED ON A REGULAR BASIS AS PART OF A RECURRING AD EVERY 100 HOURS. THIS OFFICE ALSO RECOMMENDS THE MFG INCORPORATE A "REOCCURRING VISUAL CORROSION INSPECTION" OF THE TUBE ASSY, AT THE 100 HOUR INSPECTION INTERVAL. THE AD ACTION WOULD BE THE PREFERRED METHOD TO ENSURE A HIGHER LEVEL OF SAFETY.

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