20200511003469A

Accident · Destroyed

FAA accident report · Schempp-Hirth VENTUS 2CT · Stuarts Draft, VA · May 11, 2020

Date
May 11, 2020 · 15:10 local
Place
Stuarts Draft, VA
Phase of flight
Descent
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N514TW
NTSB investigation
NTSBERA20CA178
Reported as
Schempp-Hirth Ventus 2CT
Reported engine
NONE NONE
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Airline transport, flight instructor
Pilot’s flight hours
18,000 total142 in this make and model81 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.

Pilot departed (2VA3) in merlin, VA. Upon crossing a ridge line into waynesboro, VA at approx 8000 ft MSL the pilot was unable to gain lift and began losing altitude. After deciding on a suitable landing site engine start attempt was made. Prior to getting the engine to start the aircraft contacted the ground right wing down causing partial separation from fuselage and spar damage. The tail boom also broke free from the aircraft during the landing and subsequent ground loop. Recommended minimum engine start alttitude is 984 ft AGL at 95-100 km/h iaw aircraft flight manual emergency procedures.

As the FAA filed it

PILOT DEPARTED (2VA3) IN MERLIN, VA. UPON CROSSING A RIDGE LINE INTO WAYNESBORO, VA AT APPROX 8000 FT MSL THE PILOT WAS UNABLE TO GAIN LIFT AND BEGAN LOSING ALTITUDE. AFTER DECIDING ON A SUITABLE LANDING SITE ENGINE START ATTEMPT WAS MADE. PRIOR TO GETTING THE ENGINE TO START THE AIRCRAFT CONTACTED THE GROUND RIGHT WING DOWN CAUSING PARTIAL SEPARATION FROM FUSELAGE AND SPAR DAMAGE. THE TAIL BOOM ALSO BROKE FREE FROM THE AIRCRAFT DURING THE LANDING AND SUBSEQUENT GROUND LOOP. RECOMMENDED MINIMUM ENGINE START ALTTITUDE IS 984 FT AGL AT 95-100 KM/H IAW AIRCRAFT FLIGHT MANUAL EMERGENCY PROCEDURES.

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 N514TW · 1

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