20100808042109A

Accident · Substantial damage

FAA accident report · Stinson 108-3 · Bridgeport, CA · August 8, 2010

Date
August 8, 2010 · 10:17 local
Place
Bridgeport, CA
Airport
Bryant Field
Phase of flight
Landing: Rollout
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N230SS
NTSB investigation
NTSBWPR10CA391
Reported as
Stinson 108-3
Reported engine
Continental O-470R
People aboard
3
Fatal injuries
0
Other injuries
1
Pilot’s certificate
Airline transport
Pilot’s flight hours
3,300 total300 in this make and model30 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 pilot stated that he performed a wheel landing and after touchdown he applied slight nose forward pressure on the yoke to pin the mains. A second or two later the right wing lifted rapidly which he tried to counteract with right aileron. The input of aileron was ineffective and full power was applied for a go-around. Even with power, right aileron and right rudder, the pilot could not regain control of the aircraft. The power was reduced; however, brakes were not applied in fear of a nose-over. The aircraft exited the runway to the left, and went through a fence at about a 45 degree angle and entered a ditch. The nose spun around to the right abruptly and the aircraft settled back into the ditch.

As the FAA filed it

THE PILOT STATED THAT HE PERFORMED A WHEEL LANDING AND AFTER TOUCHDOWN HE APPLIED SLIGHT NOSE FORWARD PRESSURE ON THE YOKE TO PIN THE MAINS. A SECOND OR TWO LATER THE RIGHT WING LIFTED RAPIDLY WHICH HE TRIED TO COUNTERACT WITH RIGHT AILERON. THE INPUT OF AILERON WAS INEFFECTIVE AND FULL POWER WAS APPLIED FOR A GO-AROUND. EVEN WITH POWER, RIGHT AILERON AND RIGHT RUDDER, THE PILOT COULD NOT REGAIN CONTROL OF THE AIRCRAFT. THE POWER WAS REDUCED; HOWEVER, BRAKES WERE NOT APPLIED IN FEAR OF A NOSE-OVER. THE AIRCRAFT EXITED THE RUNWAY TO THE LEFT, AND WENT THROUGH A FENCE AT ABOUT A 45 DEGREE ANGLE AND ENTERED A DITCH. THE NOSE SPUN AROUND TO THE RIGHT ABRUPTLY AND THE AIRCRAFT SETTLED BACK INTO THE DITCH.

NTSB investigation

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