20100818045149A

Accident · Substantial damage

FAA accident report · Schweizer 269C-1 · Titusville, FL · August 18, 2010

Date
August 18, 2010 · 13:45 local
Place
Titusville, FL
Phase of flight
Landing: Approach
Operating rules
Pilot school (Part 141)
Operator
HIAS
Damage
Substantial damage
Aircraft
N1542D
NTSB investigation
NTSBERA10CA432
Reported as
Schweizer 269C-1
Reported engine
Lycoming HIO-360 series
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Commercial pilot, flight instructor
Pilot’s flight hours
503 total456 in this make and model190 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.

Student was practicing 180 degree autorotations from 600 feet alt and began to rapidly build rotor RPM. CFI was distracted by tach and did not realize the loss of altitude. At 200' CFI took control and leveld aircraft. At 100' CFI began flaring to build up RPM, but aircrfat continue to descend until the tail rotor came in contact with the terrain. Immediately the aircraft lunged forward and impact the front of the skids into the ground, causing the tail boom to rise while the main rotor blades drooped, severing the tail boom in two locations and causing the aircraft to roll violantly to the left through a entire roll and resting on its leftside.

As the FAA filed it

STUDENT WAS PRACTICING 180 DEGREE AUTOROTATIONS FROM 600 FEET ALT AND BEGAN TO RAPIDLY BUILD ROTOR RPM. CFI WAS DISTRACTED BY TACH AND DID NOT REALIZE THE LOSS OF ALTITUDE. AT 200' CFI TOOK CONTROL AND LEVELD AIRCRAFT. AT 100' CFI BEGAN FLARING TO BUILD UP RPM, BUT AIRCRFAT CONTINUE TO DESCEND UNTIL THE TAIL ROTOR CAME IN CONTACT WITH THE TERRAIN. IMMEDIATELY THE AIRCRAFT LUNGED FORWARD AND IMPACT THE FRONT OF THE SKIDS INTO THE GROUND, CAUSING THE TAIL BOOM TO RISE WHILE THE MAIN ROTOR BLADES DROOPED, SEVERING THE TAIL BOOM IN TWO LOCATIONS AND CAUSING THE AIRCRAFT TO ROLL VIOLANTLY TO THE LEFT THROUGH A ENTIRE ROLL AND RESTING ON ITS LEFTSIDE.

NTSB investigation

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