20050413007889A

Accident · Substantial damage

FAA accident report · Cessna 337B · Ocala, FL · April 13, 2005

Date
April 13, 2005 · 14:30 local
Place
Ocala, FL
Airport
Ocala Municipal-Jim Taylor Field
Phase of flight
To Aborted (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N463DA
NTSB investigation
NTSBMIA05CA092
Reported as
Cessna 337B
People aboard
1
Fatal injuries
0
Pilot’s flight hours
11,621 total1,200 in this make and model16 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) Pilot aborted takeoff and crashed at end of departure runway, because the pilot stated that he had a rear engine failure. There was substantial damage to the aircraft and no injuries to the single occupant the PIC. Two witnesses stated that the rear engine was not running during taxi before takeoff. One witness on the recovery crew stated that the rear engine was not warm to the touch directly after the accident. FAA preliminary investigation revealed that the rear engine operated normally five minutes iaw the aircraft flight manual. The rear engine tachometer was not functioning during the engine run, witnessed by the FAA.

As the FAA filed it

(-23) PILOT ABORTED TAKEOFF AND CRASHED AT END OF DEPARTURE RUNWAY, BECAUSE THE PILOT STATED THAT HE HAD A REAR ENGINE FAILURE. THERE WAS SUBSTANTIAL DAMAGE TO THE AIRCRAFT AND NO INJURIES TO THE SINGLE OCCUPANT THE PIC. TWO WITNESSES STATED THAT THE REAR ENGINE WAS NOT RUNNING DURING TAXI BEFORE TAKEOFF. ONE WITNESS ON THE RECOVERY CREW STATED THAT THE REAR ENGINE WAS NOT WARM TO THE TOUCH DIRECTLY AFTER THE ACCIDENT. FAA PRELIMINARY INVESTIGATION REVEALED THAT THE REAR ENGINE OPERATED NORMALLY FIVE MINUTES IAW THE AIRCRAFT FLIGHT MANUAL. THE REAR ENGINE TACHOMETER WAS NOT FUNCTIONING DURING THE ENGINE RUN, WITNESSED BY THE FAA.

NTSB investigation

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