20021031032249A

Accident · Destroyed

FAA accident report · Beech F33A · Fernandina Beac, FL · October 31, 2002

Date
October 31, 2002 · 14:50 local
Place
Fernandina Beac, FL
Airport
Fernandina Beach Municipal
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N3122K
NTSB investigation
NTSBATL03LA012
Reported as
Beech F33A
People aboard
1
Fatal injuries
1

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) During test flight, after maintenance, for the replacement of both magnetos and a stand-by alternator, the engine lost power at approximately 2500 feet MSL. Pilot attempted to restore engine power, but was unsuccessful. Pilot then attempted to return to airport, however crash landed short of runway 22 in wooded area. Upon impact aircraft caught fire, the second pilot escaped and pulled the pilot from the aircraft to safety. The second pilot received minor injuries was treated and released, the pilot received serious injury and died from heart failure while undergoing treatment. FAA on scene investigator found no evidence of in-flight fire. Subsequent inspection of propeller blades indicated that the engine was not producing power at time of impact. During engine inspection, no discrepancies were found, that could be used to determine the loss of power. No fuel was found at the fuel distribution unit. Upon request of the NTSB, the engine has been sent to Continental motors for further investigation under supervision of NTSB.

As the FAA filed it

(-23) DURING TEST FLIGHT, AFTER MAINTENANCE, FOR THE REPLACEMENT OF BOTH MAGNETOS AND A STAND-BY ALTERNATOR, THE ENGINE LOST POWER AT APPROXIMATELY 2500 FEET MSL. PILOT ATTEMPTED TO RESTORE ENGINE POWER, BUT WAS UNSUCCESSFUL. PILOT THEN ATTEMPTED TO RETURN TO AIRPORT, HOWEVER CRASH LANDED SHORT OF RUNWAY 22 IN WOODED AREA. UPON IMPACT AIRCRAFT CAUGHT FIRE, THE SECOND PILOT ESCAPED AND PULLED THE PILOT FROM THE AIRCRAFT TO SAFETY. THE SECOND PILOT RECEIVED MINOR INJURIES WAS TREATED AND RELEASED, THE PILOT RECEIVED SERIOUS INJURY AND DIED FROM HEART FAILURE WHILE UNDERGOING TREATMENT. FAA ON SCENE INVESTIGATOR FOUND NO EVIDENCE OF IN-FLIGHT FIRE. SUBSEQUENT INSPECTION OF PROPELLER BLADES INDICATED THAT THE ENGINE WAS NOT PRODUCING POWER AT TIME OF IMPACT. DURING ENGINE INSPECTION, NO DISCREPANCIES WERE FOUND, THAT COULD BE USED TO DETERMINE THE LOSS OF POWER. NO FUEL WAS FOUND AT THE FUEL DISTRIBUTION UNIT. UPON REQUEST OF THE NTSB, THE ENGINE HAS BEEN SENT TO CONTINENTAL MOTORS FOR FURTHER INVESTIGATION UNDER SUPERVISION OF NTSB.

NTSB investigation

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