20100902050149A

Accident · Destroyed

FAA accident report · Beech 65 · Redwood City, CA · September 2, 2010

Date
September 2, 2010 · 11:51 local
Place
Redwood City, CA
Airport
San Carlos
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N832B
NTSB investigation
NTSBWPR10FA448
Reported as
Beech 65
Reported engine
Lycoming GSO&IGSO-480
People aboard
3
Fatal injuries
3
Other injuries
0
Pilot’s certificate
Commercial pilot
Pilot’s flight hours
12,004 total0 in this make and model0 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.

The aircraft departed San Carlos Airport (ksql) for south county (E16). On the departure leg out of ksql witnesses observed the aircraft going through a series of pitch oscillations. Ten seconds later the aircraft was observed exhibiting longitudinal instability. The aircraft then began a roll to the right followed by an application of left rudder. The aircraft was still observed to have a positive rate of climb although now rotating to the left on the vertical axis. The left yawing moment stopped as the aircraft began to roll to the right in a nose high attitude. The roll continued to the right as it entered a steep descending turn. The aircraft impacted a lagoon north of the airport and sank in about twelve feet of water.

As the FAA filed it

THE AIRCRAFT DEPARTED SAN CARLOS AIRPORT (KSQL) FOR SOUTH COUNTY (E16). ON THE DEPARTURE LEG OUT OF KSQL WITNESSES OBSERVED THE AIRCRAFT GOING THROUGH A SERIES OF PITCH OSCILLATIONS. TEN SECONDS LATER THE AIRCRAFT WAS OBSERVED EXHIBITING LONGITUDINAL INSTABILITY. THE AIRCRAFT THEN BEGAN A ROLL TO THE RIGHT FOLLOWED BY AN APPLICATION OF LEFT RUDDER. THE AIRCRAFT WAS STILL OBSERVED TO HAVE A POSITIVE RATE OF CLIMB ALTHOUGH NOW ROTATING TO THE LEFT ON THE VERTICAL AXIS. THE LEFT YAWING MOMENT STOPPED AS THE AIRCRAFT BEGAN TO ROLL TO THE RIGHT IN A NOSE HIGH ATTITUDE. THE ROLL CONTINUED TO THE RIGHT AS IT ENTERED A STEEP DESCENDING TURN. THE AIRCRAFT IMPACTED A LAGOON NORTH OF THE AIRPORT AND SANK IN ABOUT TWELVE FEET OF WATER.

NTSB investigation

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