Service difficulty report · Bolt · Piper PA28RT201

Difficulty date
September 17, 2011
Submitted
October 4, 2011
Operation
General aviation
Aircraft
N82821
Make and model
Piper PA28RT201
Aircraft serial
28R8118014
Aircraft time
4,190 hours
Engine
Lyc IO360C1C6
Engine time
4,190 hours
Propeller
Mcauly 2D34C215
Part
Bolt
Part number
AN440A
Condition
Failed
Location
Mlg
Part time
4,190 hours
Stage of operation
TX
How discovered
O
Nature of condition
O
Precautionary procedure
O

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

What was found

AFTER LANDING, WHILE TURNING, LT WING SAGGED. CONTINUED TAXI, LT MLG COLLAPSED. BOLT HOLDING REAR TRUNNION FRACTURED AT THE HEAD DUE TO CORROSION. ALL THE LOAD WAS TRANSFERRED TO THE FRONT TRUNNION WHICH FRACTURED AT THE END OF THE MACHINED MAIN TRUNNION STUB DUE TO OVERSTRESS, CAUSING THE RETENTION BOLT (AN4-20A) TO FAIL IN TENSION ALLOWING THE WING TO DROP OVER THE LANDING GEAR ASSY. THE GEAR STRUT PIERCED THE UPPER WING SKIN. THE BOLT HEAD REMAINED IN THE TRUNNION SLEEVE (67502-00) WHICH WAS FOUND IN THE WELL BEHIND THE REAR SPAR. THERE IS SEVERE CORROSION ON THE SHAFT OF THE BOLT FOR SEVERAL INCHES FROM THE HEAD. THE BOLT SHAFT, APPROX 1.5 INCHES FROM THE HEAD END WAS BENT AT 90 DEGREES TO THE THREAD END SHAFT APPARENTLY WHEN THE WING DROPPED OVER THE GEAR. THE RT SIDE BOLT WAS REMOVED AND HAD NO EVIDENCE OF SUCH SEVERE CORROSION. THE ANNUAL INSPECTION FOR THIS BOLT IS TO CHECK FOR THE PRESENCE OF THE HEAD. THERE IS NO REQUIREMENT TO CHECK THE TORQUE ON THE BOLT DURING THE ANNUAL INSPECTION.

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