19991213042439A

Accident · Substantial damage

FAA accident report · Piper PA-32RT-300T · Ft Lauderdale, FL · December 13, 1999

Date
December 13, 1999 · 15:06 local
Place
Ft Lauderdale, FL
Phase of flight
Climb
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N21312
NTSB investigation
NTSBMIA00LA049
Reported as
Piper PA32RT300T
Reported engine
Lycoming TIO540S1AD
Fatal injuries
0
Pilot’s flight hours
723 total222 in this make and model113 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-23)A/c departed runway 27L and impacted several pine trees, before coming to rest in about 12 ft of water. The a/c was substantially damaged. (.4)at about 150 feet AGL, during takeoff climb, the flight experienced a partial engine power loss due to an intermittently operative right-hand magneto condenser. The pilot stated the airplane stalled and collided with trees, eventually coming to rest partially submerged in a marina basin. Disassembly examination of the core engine and all fuel components revealed no mechanical abnormalities. Bench testing and disassembly examination of the right-hand magneto condenser revealed no damage attributable to the submersion and a short to ground that would have rendered the magneto inoperative. Using the pilot's estimate of fuel aboard, the occupant's weights, and the faa's estimate of the baggage and cargo aboard, computations revealed the aircraft was about 272 pounds over maximum gross takeoff weight. The pilot was not bfr current, nor was the conversion to a three-bladed propeller properly documented in the maintenance records.

As the FAA filed it

(-23)A/C DEPARTED RUNWAY 27L AND IMPACTED SEVERAL PINE TREES, BEFORE COMING TO REST IN ABOUT 12 FT OF WATER. THE A/C WAS SUBSTANTIALLY DAMAGED. (.4)AT ABOUT 150 FEET AGL, DURING TAKEOFF CLIMB, THE FLIGHT EXPERIENCED A PARTIAL ENGINE POWER LOSS DUE TO AN INTERMITTENTLY OPERATIVE RIGHT-HAND MAGNETO CONDENSER. THE PILOT STATED THE AIRPLANE STALLED AND COLLIDED WITH TREES, EVENTUALLY COMING TO REST PARTIALLY SUBMERGED IN A MARINA BASIN. DISASSEMBLY EXAMINATION OF THE CORE ENGINE AND ALL FUEL COMPONENTS REVEALED NO MECHANICAL ABNORMALITIES. BENCH TESTING AND DISASSEMBLY EXAMINATION OF THE RIGHT-HAND MAGNETO CONDENSER REVEALED NO DAMAGE ATTRIBUTABLE TO THE SUBMERSION AND A SHORT TO GROUND THAT WOULD HAVE RENDERED THE MAGNETO INOPERATIVE. USING THE PILOT'S ESTIMATE OF FUEL ABOARD, THE OCCUPANT'S WEIGHTS, AND THE FAA'S ESTIMATE OF THE BAGGAGE AND CARGO ABOARD, COMPUTATIONS REVEALED THE AIRCRAFT WAS ABOUT 272 POUNDS OVER MAXIMUM GROSS TAKEOFF WEIGHT. THE PILOT WAS NOT BFR CURRENT, NOR WAS THE CONVERSION TO A THREE-BLADED PROPELLER PROPERLY DOCUMENTED IN THE MAINTENANCE RECORDS.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.

Other reports on N21312 · 1

Matched to the same aircraft by N-number and date.