20110410006759A

Accident · Substantial damage

FAA accident report · Robinson Helicopter R22 · Marlboro, MA · April 10, 2011

Date
April 10, 2011 · 10:00 local
Place
Marlboro, MA
Airport
Marlboro Airport
Phase of flight
Hover/Holding
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N791SH
NTSB investigation
NTSBERA11CA235
Reported as
Robinson Helicopter R22
Reported engine
Lycoming O-360 series
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Private pilot
Pilot’s flight hours
250 total29 in this make and model15 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.

The student, an airplane rated private pilot, was on his fourth solo flight. This was his first solo flight with the fuel tanks full, resulting in a center of gravity within limits, but near the aft limits. The student lightened the load on the helicopter skids twice in order to "feel" the balance and adjust the control inputs. The student then lifted the aircraft into a hover, and started to drift aft, tail low. The stinger and tailrotor struck the surface and the aircraft started to yaw significantly to the right. The helicopter proceeded around about 360 degrees until the student reduced collective, landing back on the ramp area. Damage was visually evident to the tail rotor blades, stinger and lower vertical stabilizer.

As the FAA filed it

THE STUDENT, AN AIRPLANE RATED PRIVATE PILOT, WAS ON HIS FOURTH SOLO FLIGHT. THIS WAS HIS FIRST SOLO FLIGHT WITH THE FUEL TANKS FULL, RESULTING IN A CENTER OF GRAVITY WITHIN LIMITS, BUT NEAR THE AFT LIMITS. THE STUDENT LIGHTENED THE LOAD ON THE HELICOPTER SKIDS TWICE IN ORDER TO "FEEL" THE BALANCE AND ADJUST THE CONTROL INPUTS. THE STUDENT THEN LIFTED THE AIRCRAFT INTO A HOVER, AND STARTED TO DRIFT AFT, TAIL LOW. THE STINGER AND TAILROTOR STRUCK THE SURFACE AND THE AIRCRAFT STARTED TO YAW SIGNIFICANTLY TO THE RIGHT. THE HELICOPTER PROCEEDED AROUND ABOUT 360 DEGREES UNTIL THE STUDENT REDUCED COLLECTIVE, LANDING BACK ON THE RAMP AREA. DAMAGE WAS VISUALLY EVIDENT TO THE TAIL ROTOR BLADES, STINGER AND LOWER VERTICAL STABILIZER.

NTSB investigation

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