20170607006889A

Accident · Substantial damage

FAA accident report · Mckenna SD-1A · Juneau, WI · June 7, 2017

Date
June 7, 2017 · 09:00 local
Place
Juneau, WI
Airport
Dodge County Airport
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N31313
NTSB investigation
NTSBCEN17LA224
Reported as
Mckenna SD-1A
Reported engine
Continental C85 series
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Private pilot
Pilot’s flight hours
390 total1 in this make and model7 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.

Owner purchased an experimental aircraft with the wings, ailerons, flaps, horizontal stab, elevators and rudder removed. The owner reinstalled all parts. An A&P performed a condition inspection. The owner conducted a test flight and on climb he had to keep the left aileron in the full down position to keep the aircraft level. His speed was 70 mph . Owner continued flight at 500 ft AGL in the airport pattern. Upon landing, he bounced on the first attempt and tried to flare but lost control to the right, ground looping into grass tearing off the left landing gear from the engine mount and causing substantial damage to the engine mount.

On inspection, flight control continuity was confirmed. Ailerons, flaps and rudder lined up and looked to be rigged properly. The wing angle of incidence could not be determined.

As the FAA filed it

OWNER PURCHASED AN EXPERIMENTAL AIRCRAFT WITH THE WINGS, AILERONS, FLAPS, HORIZONTAL STAB, ELEVATORS AND RUDDER REMOVED. THE OWNER REINSTALLED ALL PARTS. AN A&P PERFORMED A CONDITION INSPECTION. THE OWNER CONDUCTED A TEST FLIGHT AND ON CLIMB HE HAD TO KEEP THE LEFT AILERON IN THE FULL DOWN POSITION TO KEEP THE AIRCRAFT LEVEL. HIS SPEED WAS 70 MPH . OWNER CONTINUED FLIGHT AT 500 FT AGL IN THE AIRPORT PATTERN. UPON LANDING, HE BOUNCED ON THE FIRST ATTEMPT AND TRIED TO FLARE BUT LOST CONTROL TO THE RIGHT, GROUND LOOPING INTO GRASS TEARING OFF THE LEFT LANDING GEAR FROM THE ENGINE MOUNT AND CAUSING SUBSTANTIAL DAMAGE TO THE ENGINE MOUNT.

ON INSPECTION, FLIGHT CONTROL CONTINUITY WAS CONFIRMED. AILERONS, FLAPS AND RUDDER LINED UP AND LOOKED TO BE RIGGED PROPERLY. THE WING ANGLE OF INCIDENCE COULD NOT BE DETERMINED.

NTSB investigation

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