20100115028109A

Accident · Destroyed

FAA accident report · Steele Samu RV-4 · Picayune, MS · January 15, 2010

Date
January 15, 2010 · 16:45 local
Place
Picayune, MS
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N107SS
NTSB investigation
NTSBERA10LA120
Reported as
Steele Samu RV-4
Reported engine
Lycoming 0-320 series
People aboard
2
Fatal injuries
2
Other injuries
0
Pilot’s certificate
Private pilot
Pilot’s flight hours
1,859 total100 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/a&p/owner, was working on the auto pilot, on the day of the accident. The pilot took a passenger for the test flight, of the auto pilot. A witness observed the plane 1,600 feet from the end of the runway, doing a flyby at about 50 feet AGL. The aircraft came to rest 1,630 feet from the end of the runway, in a nose down attitude and with evidence of a spin to the left. Weight and balance information showed that the aircraft was 267 lbs over the recommended gross weight and 389 lbs over the acrobatic gross weight. The center of gravity (CG) calculations showed the CG was 0.27 behind the design CG and 1.77 behind the aerobatic CG limit.

As the FAA filed it

THE PILOT/A&P/OWNER, WAS WORKING ON THE AUTO PILOT, ON THE DAY OF THE ACCIDENT. THE PILOT TOOK A PASSENGER FOR THE TEST FLIGHT, OF THE AUTO PILOT. A WITNESS OBSERVED THE PLANE 1,600 FEET FROM THE END OF THE RUNWAY, DOING A FLYBY AT ABOUT 50 FEET AGL. THE AIRCRAFT CAME TO REST 1,630 FEET FROM THE END OF THE RUNWAY, IN A NOSE DOWN ATTITUDE AND WITH EVIDENCE OF A SPIN TO THE LEFT. WEIGHT AND BALANCE INFORMATION SHOWED THAT THE AIRCRAFT WAS 267 LBS OVER THE RECOMMENDED GROSS WEIGHT AND 389 LBS OVER THE ACROBATIC GROSS WEIGHT. THE CENTER OF GRAVITY (CG) CALCULATIONS SHOWED THE CG WAS 0.27 BEHIND THE DESIGN CG AND 1.77 BEHIND THE AEROBATIC CG LIMIT.

NTSB investigation

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