Service difficulty report · Steering Sys · Piper PA11

Difficulty date
September 14, 2010
Submitted
January 4, 2011
Operation
General aviation
Make and model
Piper PA11
Aircraft time
2,910 hours
Engine
Cont C9012F
Propeller
Mcauly 1B90CM
Part
Steering Sys
Part number
750330
Condition
Misinstalled
Location
Rudder Assy
Stage of operation
IN
How discovered
V
Nature of condition
O
Precautionary procedure
K

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

What was found

DURING INSP OF THE RUDDER ASSY. WHILE ACFT WAS DISASSEMBLED FOR O/H, IT WAS FOUND THAT DURING PREVIOUS REPLACEMENT OF ACFT FABRIC, BOLTS ATTACHING THE RUDDER STEERING ARM CASTING TO THE RUDDER ASSY HAD BEEN REMOVED TO FACILITATE THE INSTALLATION OF THE NEW FABRIC. WHEN THE NEW FABRIC WAS INSTALLED IT COVERED THE ATTACHMENT BOLT HOLES. BECAUSE THE BOLT HOLES WERE COVERED UP, THE ATTACHMENT BOLTS WERE NOT REINSTALLED. THE STEERING ARM IS AN ALUMINUM CASTING. IT FEATURES A .7500 INCH ROUND ATTACHMENT SHANK WHICH IS INSTALLED INTO THE 4130 STEEL RUDDER SPAR. CORROSION, CAUSED BY THE CONTACT OF DISSIMILAR METALS, FROZE THE PART IN PLACE. THIS RESULTED IN THE ARM NOT COMING LOOSE. ACFT APPEARS TO HAVE BEEN IN SERVICE WITHOUT THE BOLTS INSTALLED FOR APPROX 20 YEARS. AT THIS POINT, WE ARE AWAITING RECEIPT OF THE LOG BOOKS FROM OWNER TO REVIEW MX HISTORY. THE USE OF THIS PART AND THE WAY IT IS ATTACHED TO THIS ACFT IS THE SAME THROUGHOUT THE MFG SERIES ACFT THAT ARE FABRIC COVERED. IT IS STRONGLY RECOMMENDED THAT ACFT BE INSPECTED FOR THIS UNSAFE CONDITION.

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