Service difficulty report · Control Cable · Piper PA28R201

Difficulty date
March 1, 2006
Submitted
April 18, 2006
Operation
General aviation
Aircraft
N963PA
Make and model
Piper PA28R201
Aircraft serial
2844023
Engine
Lyc IO360A1A
Part
Control Cable
Part number
62701100
Condition
Frayed
Location
Fuselage
Part time
5,350 hours
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

WHILE CONDUCTING AN ANNUAL INSPECTION PRIOR TO PLACING THE AIRCRAFT ONLINE AFTER PURCHASING IT FROM A LOCAL OPERATOR THE RT FWD RUDDER CABLE WAS FOUND TO BE BADLY WORN AND FRAYED. THE LOCATION OF THE FRAYING WAS JUST UNDER THE CENTER CONSOLE FOR THE STABALATOR TRIM AND JUST AS IT EXITED IN TO THE INSPECTION AREA UNDER THE REAR SEATS AT THE FORWARD PULLEY. THIS IS A KNOWN AREA OF WEAR FOR ALL PA 28, 34, AND 44 MODEL AIRCRAFT. RESEARCH OF THE MAINTENANCE RECORDS SHOWED THAT THE PREVIOUS OWNERS HAD FAILED TO COMPLY WITH SB WHICH REQUIRES REPETITIVE INSPECTIONS OF ALL FLIGHT CONTROL CABLES. THIS SB WAS APPLICABLE TO THIS AIRCRAFT. (K)

More about the Piper PA-28R-201