Piper PA-32R Safety Record

FAILURE OF THE PILOT TO MAINTAIN PROPER ALIGNMENT DURING THE LANDING ROLL, EXCESSIVE RUDDER INPUT, AND LOSS OF DIRECTIONAL CONTROL RESULTING IN THE COLLAPSE OF THE RIGHT MAIN LANDING GEAR.

FATIGUE FAILURE OF THE THROTTLE CABLE. FACTORS RELATED TO THE ACCIDENT WERE: DARKNESS AND OBJECTS (FENCE AND UTILITY POLES) IN THE EMERGENCY LANDING AREA.

UNDETERMINED MECHANICAL FAILURE(S) THAT RESULTED IN LOSS OF ENGINE POWER, SMOKE IN THE COCKPIT, AND A SUBSEQUENT EMERGENCY DESCENT FOR A FORCED LANDING (DITCHING) AT SEA. THE LACK OF SUITABLE TERRAIN FOR A FORCED LANDING WAS A RELATED FACTOR.

FAILURE OF THE PILOT IN COMMAND TO ATTAIN ADEQUATE AIRSPEED PRIOR TO LIFTOFF DURING AN ATTEMPTED TAKEOFF. THE PILOT THEN LOST CONTROL OF THE AIRPLANE IN FLIGHT. THE PILOT ALSO DELAYED IN HIS DECISION TO ABORT THE TAKEOFF.

INITIATION OF VFR FLIGHT INTO ADVERSE WEATHER AND INSTRUMENT METEOROLOGIAL CONDITIONS. FACTORS WHICH CONTRIBUTED TO THE ACCIDENT WERE THE ADVERSE WEATHER CONDITIONS AND THE PILOT'S SELF-INDUCED PRESSURE TO MAINTAIN CURRENCY.

A LOSS OF AIRCRAFT CONTROL FOR AN UNKNOWN REASON, WHILE EN ROUTE IN INSTRUMENT METEOROLOGICAL CONDITIONS (IMC) ON A DARK NIGHT, AND THE PILOT EXCEEDING THE DESIGN STRESS LIMITS OF THE AIRCRAFT WHILE ATTEMPTING TO RECOVER FROM UNCONTROLLED FLIGHT. FACTORS RELATED TO THE ACCIDENT WERE: PILOT FATIGUE AND PROBABLE SPATIAL DISORIENTATION OF THE PILOT AND/OR AN INSTRUMENT MALFUNCTION.

THE FAILURE OF THE LEFT INTERMEDIATE EXHAUST PIPE, IN-FLIGHT ENGINE FIRE AND SMOKE IN THE COCKPIT, RESULTING IN IMPAIRMENT OF THE PILOT AND HIS SUBSEQUENT LOSS OF CONTROL.

FLIGHT INTO KNOWN ADVERSE WEATHER CONDITIONS BY THE PILOT AND STRUCTURAL (WING) ICING. FACTORS RELATED TO THE ACCIDENT WERE: THE ADVERSE WEATHER CONDITIONS AND THE PILOT'S OVERCONFIDENCE IN THE AIRCRAFT'S ABILITY.

IMPROPER INSTALLATION BY MAINTENANCE PERSONNEL AND FATIGUE FAILURE AND LEAKAGE OF THE LEFT INTERMEDIATE EXHAUST PIPE, WHICH RESULTED IN AN IN-FLIGHT FIRE IN THE ENGINE COMPARTMENT. CONTRIBUTING FACTORS WERE: INADEQUATE SERVICE BULLETIN PROVIDED BY THE MANUFACTURER AND INSUFFICIENT STANDARDS PROVIDED BY THE (FAA) AIRWORTHINESS DIRECTIVE.

FAILURE OF THE PILOT TO MAINTAIN PROPER ALTITUDE AND CLEARANCE FROM TREES WHILE DEPARTING FROM THE AIRPORT. FACTORS RELATED TO THE ACCIDENT WERE: THE PILOT'S INADEQUATE PREFLIGHT PLANNING/PREPARATION, HIS ALLOWING THE AIRCRAFT WEIGHT AND BALANCE TO BE EXCEEDED, DARKNESS, AND THE PILOT'S LACK OF FAMILIARITY WITH THE AIRPORT.

FAILURE OF THE PILOT TO MAINTAIN PROPER AIRSPEED AND ALTITUDE ON AN ILS FINAL APPROACH, WHICH ALLOWED THE AIRCRAFT TO DESCEND BELOW THE GLIDE PATH AND COLLIDE WITH APPROACH LIGHTING. FACTORS RELATED TO THE ACCIDENT WERE: DARKNESS, ADVERSE WEATHER CONDITIONS, THE PILOT'S DECISION TO FLY IN KNOWN ADVERSE WEATHER (ICING) CONDITIONS, AND STRUCTURAL ICING.

IMPROPER PLANNING/DECISION BY THE PILOT. FACTORS RELATED TO THE ACCIDENT WERE: THE PILOT'S LACK OF FAMILIARITY WITH THE AIRCRAFT, HIS FAILURE TO USE THE RECOMMENDED FLAP EXTENSION, HIS FAILURE TO MAINTAIN AN AIRSPEED ABOVE THE AUTOMATIC GEAR EXTENSION SPEED OR USE THE OVERRIDE FEATURE, WHICH ALLOWED THE GEAR TO EXTEND (PRECLUDING THE ABILITY TO CLIMB), AND THE POWER LINE.

THE PILOT'S DECISION TO CONTINUE THE TAXI DURING DARK NIGHT CONDITIONS WITHOUT TAXIWAY LIGHTS, AN OPERABLE LANDING LIGHT OR, ASSISTANCE FROM AIRPORT PERSONNEL.

INADEQUATE PREFLIGHT BY THE PILOT, WHICH RESULTED IN FUEL EXHAUSTION, DUE TO AN INADEQUATE SUPPLY OF FUEL. FACTORS RELATED TO THE ACCIDENT WERE: FALSE FUEL GAGE INDICATIONS AND TREES IN THE EMERGENCY LANDING AREA.