20170731015659A

Accident · Substantial damage

FAA accident report · Chapman Robert E T-BIRD II (TIERRA) · Potosi, MO · July 31, 2017

Date
July 31, 2017 · 08:35 local
Place
Potosi, MO
Airport
Washington County Apt
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N204BC
NTSB investigation
NTSBCEN17LA293
Reported as
Chapman Robert E T-BIRD II (Tierra)
Reported engine
ROTAX 582
People aboard
1
Fatal injuries
0
Other injuries
1
Pilot’s certificate
Private pilot

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.

On July 31, 2017 at approximately 0835 central daylight time the pilot performed a normal takeoff from Washington county airport (8WC) near Potosi, MO. This was the pilot's first flight in this airplane make and model. After climbing to approximately 100 150 feet above the airport elevation witnesses saw the aircraft begin a steeply banked turn to the right along with an abrupt steep nose-down change in pitch attitude. The airplane descended rapidly and struck the ground approximately 500 feet beyond the departure end of runway 02 in a pasture approximately 50 feet below the airport elevation.

The aircraft wreckage was inspected. Control cable continuity was established along with adequate fuel and engine compression. The required condition inspection was current at the time of the incident.

The pilot sustained injuries of a broken ankle requiring surgery, a back injury requiring surgery, abrasions and contusions.

The pilot suggested the possibility of a take-off and departure stall. The pilot stated that the airplane seemed to be wallowing just prior to making an uncommanded right turn along with an abrupt drop in pitch attitude. The pilot also states that in response he applied full opposite aileron and rudder with no response from the aircraft, further validating take-off and departure stall.

Multiple major modifications had been made to the aircraft including change to the size and shape of the aileron airfoil, addition of flaps, addition of flap controls, and modification to a tricycle gear of original design. None of these modifications had been adequately flight tested in accordance with the special airworthiness certificate and issued operating limitations.

As the FAA filed it

ON JULY 31, 2017 AT APPROXIMATELY 0835 CENTRAL DAYLIGHT TIME THE PILOT PERFORMED A NORMAL TAKEOFF FROM WASHINGTON COUNTY AIRPORT (8WC) NEAR POTOSI, MO. THIS WAS THE PILOT'S FIRST FLIGHT IN THIS AIRPLANE MAKE AND MODEL. AFTER CLIMBING TO APPROXIMATELY 100 150 FEET ABOVE THE AIRPORT ELEVATION WITNESSES SAW THE AIRCRAFT BEGIN A STEEPLY BANKED TURN TO THE RIGHT ALONG WITH AN ABRUPT STEEP NOSE-DOWN CHANGE IN PITCH ATTITUDE. THE AIRPLANE DESCENDED RAPIDLY AND STRUCK THE GROUND APPROXIMATELY 500 FEET BEYOND THE DEPARTURE END OF RUNWAY 02 IN A PASTURE APPROXIMATELY 50 FEET BELOW THE AIRPORT ELEVATION.

THE AIRCRAFT WRECKAGE WAS INSPECTED. CONTROL CABLE CONTINUITY WAS ESTABLISHED ALONG WITH ADEQUATE FUEL AND ENGINE COMPRESSION. THE REQUIRED CONDITION INSPECTION WAS CURRENT AT THE TIME OF THE INCIDENT.

THE PILOT SUSTAINED INJURIES OF A BROKEN ANKLE REQUIRING SURGERY, A BACK INJURY REQUIRING SURGERY, ABRASIONS AND CONTUSIONS.

THE PILOT SUGGESTED THE POSSIBILITY OF A TAKE-OFF AND DEPARTURE STALL. THE PILOT STATED THAT THE AIRPLANE SEEMED TO BE WALLOWING JUST PRIOR TO MAKING AN UNCOMMANDED RIGHT TURN ALONG WITH AN ABRUPT DROP IN PITCH ATTITUDE. THE PILOT ALSO STATES THAT IN RESPONSE HE APPLIED FULL OPPOSITE AILERON AND RUDDER WITH NO RESPONSE FROM THE AIRCRAFT, FURTHER VALIDATING TAKE-OFF AND DEPARTURE STALL.

MULTIPLE MAJOR MODIFICATIONS HAD BEEN MADE TO THE AIRCRAFT INCLUDING CHANGE TO THE SIZE AND SHAPE OF THE AILERON AIRFOIL, ADDITION OF FLAPS, ADDITION OF FLAP CONTROLS, AND MODIFICATION TO A TRICYCLE GEAR OF ORIGINAL DESIGN. NONE OF THESE MODIFICATIONS HAD BEEN ADEQUATELY FLIGHT TESTED IN ACCORDANCE WITH THE SPECIAL AIRWORTHINESS CERTIFICATE AND ISSUED OPERATING LIMITATIONS.

NTSB investigation

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