20120702014939A

Accident · Substantial damage

FAA accident report · Dehavilland BEAVER DHC-2 · Rudyard Bay, AK · July 2, 2012

Date
July 2, 2012 · 15:15 local
Place
Rudyard Bay, AK
Phase of flight
Takeoff: Departure Roll
Operating rules
Air taxi and commuter (Part 135)
Operator
TQ0A
Damage
Substantial damage
Aircraft
N1018A
NTSB investigation
NTSBANC12CA060
Reported as
Dehavilland Beaver DHC-2
Reported engine
Pratt & Whitney R-985 series
People aboard
6
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Airline transport, flight instructor
Pilot’s flight hours
5,925 total110 in this make and model110 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.

Condition:calm water and light wind. Pilot planned to start the take-off run opposite the direction he intended to take off, do a step turn to the left to the intended departure direction and take off. In the step turn the rate of turn increased to more than what the pilot anticipated. The pilot lost control as the turn tightened, resulting in an excessive capsizing tendency of the aircraft, causing the right wing to contact the water resulting in substantial damage to the right wing.

As the FAA filed it

CONDITION:CALM WATER AND LIGHT WIND. PILOT PLANNED TO START THE TAKE-OFF RUN OPPOSITE THE DIRECTION HE INTENDED TO TAKE OFF, DO A STEP TURN TO THE LEFT TO THE INTENDED DEPARTURE DIRECTION AND TAKE OFF. IN THE STEP TURN THE RATE OF TURN INCREASED TO MORE THAN WHAT THE PILOT ANTICIPATED. THE PILOT LOST CONTROL AS THE TURN TIGHTENED, RESULTING IN AN EXCESSIVE CAPSIZING TENDENCY OF THE AIRCRAFT, CAUSING THE RIGHT WING TO CONTACT THE WATER RESULTING IN SUBSTANTIAL DAMAGE TO THE RIGHT WING.

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 N1018A · 2

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