Piper PA-32R Safety Record

a loss of engine power due to the ingestion of foreign object(s) into the meshing of the gears, causing a malfunction of the magneto idler gear and failure of maintenance personnel to detect the signs of imminent failure during a mandatory oil filter examination to be performed at the time of an oil change, annual inspection, or engine overhaul. Contributing factors were unsuitable terrain for the forced landing, high crosswind weather conditions, and a parked vehicle in the landing area.

the loss of engine power for undetermined reasons during the approach and the inadvertent stall that occurred during the forced landing. Factors relating to this accident were the low airspeed, the uphill terrain, and the fence.

The failure of the pilot to maintain minimum flying airspeed, (Vso) during takeoff following a partial loss of engine power resulting in the aircraft stalling, an uncontrolled descent, and collision with trees. A factor in the accident was the failure of the right-hand magneto condenser and the pilot's operation of the aircraft in excess of its maximum gross takeoff weight.

The loss of engine power due to the failure of maintenance personnel to properly torque a connecting rod bolt during an engine overhaul, and the subsequent disconnection of the connecting rod bolt and connecting rod.

fatigue failure of the #2 cylinder fuel injection line in an area where the line was previously damaged, which resulted in an in-flight engine compartment fire and a forced landing. Related factors were: the previous damage of the fuel injector line, and the lack of suitable terrain for the forced landing.

the pilot's incomplete preflight of the airplane's stabilizer and rudder trim settings for takeoff, his failure to correct for the high pitch during the initial climb, his failure to recover from the bounced landing, and the inadvertent stall. Factors relating to this accident were the improper stabilizer and rudder trim settings.

The pilot's improper in-flight planning/decision, which resulted in a heavy load of airframe ice, an inability to maintain altitude, and a subsequent emergency landing. Factors relating to the accident were: the adverse weather (icing) condition, which was slightly worse than forecast; and loss of airspeed indication due to ice.

A FAILURE IN THE AIRCRAFT ELECTRICAL SYSTEM, AND THE PILOT'S FAILURE (OR INABILITY) TO EXTEND THE LANDING GEAR WITH THE EMERGENCY EXTENSION SYSTEM. A FACTOR RELATING TO THE ACCIDENT WAS: THE PILOT'S DECISION TO CONTINUE THE FLIGHT WITH A KNOWN DEFICIENCY.

THE PILOT'S IMPROPER DECISION TO CONTINUE FLIGHT INTO ICING CONDITIONS AFTER THE CONDITIONS WERE FIRST ENCOUNTERED. A FACTOR RELATED TO THE ACCIDENT WAS THE TREES CONTACTED DURING THE LANDING ROLL.

THE IMPROPER USE OF THE FUEL SELECTOR BY THE PILOT-IN-COMMAND BY SWITCHING TO AN EMPTY FUEL TANK. CONTRIBUTING TO THE ACCIDENT WAS THE PILOT'S FAILURE TO SWITCH BACK TO A TANK WITH FUEL.

LOSS OF ENGINE POWER DURING THE DOWNWIND LEG FOR UNDETERMINED REASONS, POOR IN-FLIGHT PLANNING/DECISION BY THE DUAL STUDENT, AND INADEQUATE SUPERVISION BY THE PILOT-IN-COMMAND (CFI).

THE UNKNOWN PILOTS IMPROPER USE OF THE THROTTLES WHICH RESULTED IN THE OVERBOOSTING OF THE ENGINE. CONTRIBUTING TO THE ACCIDENT WAS THE MAINTENANCE PERSONNEL IMPROPER MAINTENANCE IN ADJUSTING THE TURBOCHARGER WASTEGATE AND THE OIL LEAKING FROM THE ENGINE AFTER THE CATASTROPHIC FAILURE WHICH RESTRICTED THE PILOT'S VISUAL OUTLOOK.

THE PIC'S POOR PREFLIGHT PLANNING AND THE PIC'S AND FLIGHT INSTRUCTOR/PASSENGER'S FAILURE TO USE THE EMERGENCY CHECKLIST. THE LOSS OF ENGINE POWER DUE TO FUEL STARVATION WAS A FACTOR IN THE ACCIDENT.

THE PILOT'S FAILURE TO COMPENSATE FOR WIND CONDITIONS AND MAINTAIN DIRECTIONAL CONTROL. FACTORS INCLUDED: THE PILOT ALLOWING THE AIRPLANE TO LIFT OFF PREMATURELY, AND GUSTY CROSSWINDS.

WAS THE FAILURE OF THE FUEL SERVO DIAPHRAGM STEM WHICH RESULTED IN A FUEL INTERRUPTION TO THE ENGINE. HIGH OBSTRUCTIONS AND UTILITY POLE IN THE FORCED LANDING AREA WERE FACTORS CONTRIBUTING TO THE ACCIDENT.

FAILURE OF THE PILOT TO ATTAIN ADEQUATE AIRSPEED, WHICH RESULTED IN A STALL. FACTORS RELATED TO THE ACCIDENT WERE THE CROSSWIND, THE PILOT'S INADEQUATE COMPENSATION FOR THE WIND AND FAILURE TO MAINTAIN PROPER ALIGNMENT WITH THE RUNWAY, AND HIGH OBSTRUCTIONS.