20140815017869A

Accident · Destroyed

FAA accident report · Cessna 414 · Bowie, TX · August 15, 2014

Date
August 15, 2014 · 15:30 local
Place
Bowie, TX
Phase of flight
Landing: Approach
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N127BC
NTSB investigation
NTSBCEN14FA438
Reported as
Cessna 414
Reported engine
Continental TSIO-520-NB
People aboard
2
Fatal injuries
2
Other injuries
0
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
1,200 total15 in this make and model15 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.

Pilot had purchased aircraft two weeks proir to accident flight. Pilot had obtained ground and flight instruction to transition from his CE-310 to accident aircraft (CE-414). Witness states aircraft entered pattern on a l/h base leg direction and dove slightly to lose altitude. Aircraft pulled up but power was not applied. Aircraft entered a stall/spin, doing 3 l/h rotations prior to impact in a slight nose down flat attitude. Post accident fire consumed entire fuselage.

Investigation found engine throttles at idle, evidence of rotation found on the propellers and turbo-charger impellers. Fuel selector valves set to main. Field teardown of engines found no obvious sign of inflight shutdown or engine problems. At this time no mechanical explanation can be found for the accident

As the FAA filed it

PILOT HAD PURCHASED AIRCRAFT TWO WEEKS PROIR TO ACCIDENT FLIGHT. PILOT HAD OBTAINED GROUND AND FLIGHT INSTRUCTION TO TRANSITION FROM HIS CE-310 TO ACCIDENT AIRCRAFT (CE-414). WITNESS STATES AIRCRAFT ENTERED PATTERN ON A L/H BASE LEG DIRECTION AND DOVE SLIGHTLY TO LOSE ALTITUDE. AIRCRAFT PULLED UP BUT POWER WAS NOT APPLIED. AIRCRAFT ENTERED A STALL/SPIN, DOING 3 L/H ROTATIONS PRIOR TO IMPACT IN A SLIGHT NOSE DOWN FLAT ATTITUDE. POST ACCIDENT FIRE CONSUMED ENTIRE FUSELAGE.

INVESTIGATION FOUND ENGINE THROTTLES AT IDLE, EVIDENCE OF ROTATION FOUND ON THE PROPELLERS AND TURBO-CHARGER IMPELLERS. FUEL SELECTOR VALVES SET TO MAIN. FIELD TEARDOWN OF ENGINES FOUND NO OBVIOUS SIGN OF INFLIGHT SHUTDOWN OR ENGINE PROBLEMS. AT THIS TIME NO MECHANICAL EXPLANATION CAN BE FOUND FOR THE ACCIDENT

NTSB investigation

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