20101021052019A

Accident · Substantial damage

FAA accident report · Cirrus Desi SR20 · Sanford, FL · October 21, 2010

Date
October 21, 2010 · 11:30 local
Place
Sanford, FL
Airport
Orlando Sanford International
Phase of flight
Landing: Touchdown
Operating rules
Pilot school (Part 141)
Damage
Substantial damage
Aircraft
N495DA
NTSB investigation
NTSBERA11CA030
Reported as
Cirrus Desi SR20
Reported engine
Continental IO-360-ES
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Student
Pilot’s flight hours
66 total65 in this make and model41 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.

This office responded to an aircraft accident at the Orlando- Sanford airport involving a Cirrus SR-20 airplane. During our interview with the pilot, he stated that he was cleared to land on runway 27C. He also remembered the wind at 8 knots. On short final was reading 75 indicated airspeed, the aircraft touched down and bounced back up in the air about 5 feet. He then flared a second time and the results were the same he again bounced, at that point the student decided to abort the 3rd landing attempt an do a go around. Approximately 20-30 feet altitude had 80 knots still low for flaps the airplane began turning & yawing left. He tried to correct and couldn't. it then descended left into the grass left wing low. The aircraft sustained substantial damage, it appears the aircraft as it hit the embankment caused the propeller to drive into the ground,dislodge the engine subsequenty almost somersaulting the aircraft spinning it completely around impailing it into the ground and then sliding on the edge of the grass. Debris and witness statements depict the same scenario. During inspection found the brs system to be intact, the lanyard straps became exposed but the system never fired and was disarmed by aerosim. The air bag deployed as required. The left gear pushed through the wing causing the wing to break at the cord line. As stated the engine mounts broke free causing the engine to roll several times. The vertical tail/rudder hinges had torn causing the rudder hinges to elongate due to impact.

As the FAA filed it

THIS OFFICE RESPONDED TO AN AIRCRAFT ACCIDENT AT THE ORLANDO- SANFORD AIRPORT INVOLVING A CIRRUS SR-20 AIRPLANE. DURING OUR INTERVIEW WITH THE PILOT, HE STATED THAT HE WAS CLEARED TO LAND ON RUNWAY 27C. HE ALSO REMEMBERED THE WIND AT 8 KNOTS. ON SHORT FINAL WAS READING 75 INDICATED AIRSPEED, THE AIRCRAFT TOUCHED DOWN AND BOUNCED BACK UP IN THE AIR ABOUT 5 FEET. HE THEN FLARED A SECOND TIME AND THE RESULTS WERE THE SAME HE AGAIN BOUNCED, AT THAT POINT THE STUDENT DECIDED TO ABORT THE 3RD LANDING ATTEMPT AN DO A GO AROUND. APPROXIMATELY 20-30 FEET ALTITUDE HAD 80 KNOTS STILL LOW FOR FLAPS THE AIRPLANE BEGAN TURNING & YAWING LEFT. HE TRIED TO CORRECT AND COULDN'T. IT THEN DESCENDED LEFT INTO THE GRASS LEFT WING LOW. THE AIRCRAFT SUSTAINED SUBSTANTIAL DAMAGE, IT APPEARS THE AIRCRAFT AS IT HIT THE EMBANKMENT CAUSED THE PROPELLER TO DRIVE INTO THE GROUND,DISLODGE THE ENGINE SUBSEQUENTY ALMOST SOMERSAULTING THE AIRCRAFT SPINNING IT COMPLETELY AROUND IMPAILING IT INTO THE GROUND AND THEN SLIDING ON THE EDGE OF THE GRASS. DEBRIS AND WITNESS STATEMENTS DEPICT THE SAME SCENARIO. DURING INSPECTION FOUND THE BRS SYSTEM TO BE INTACT, THE LANYARD STRAPS BECAME EXPOSED BUT THE SYSTEM NEVER FIRED AND WAS DISARMED BY AEROSIM. THE AIR BAG DEPLOYED AS REQUIRED. THE LEFT GEAR PUSHED THROUGH THE WING CAUSING THE WING TO BREAK AT THE CORD LINE. AS STATED THE ENGINE MOUNTS BROKE FREE CAUSING THE ENGINE TO ROLL SEVERAL TIMES. THE VERTICAL TAIL/RUDDER HINGES HAD TORN CAUSING THE RUDDER HINGES TO ELONGATE DUE TO IMPACT.

NTSB investigation

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