20121106028159A

Accident · Substantial damage

FAA accident report · Robinson Helicopter R44 II · Bryan, TX · November 6, 2012

Date
November 6, 2012 · 17:00 local
Place
Bryan, TX
Phase of flight
Hover/Holding
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N131AA
NTSB investigation
NTSBCEN13CA053
Reported as
Robinson Helicopter R44 II
Reported engine
Lycoming IO-540-AE1A5
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Commercial pilot, flight instructor
Pilot’s flight hours
4,001 total31 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.

Student pilot was on second solo flight of the day. When the collective was applied the helicopter became light on the skids and started to hover the helicopter rolled right, the student corrected with a left cyclic movement which caused left skid to contact the ground. The helicopter rolled back to the right rolling on to its side and contacting the ground with substantial damage done to the helicopter. Transmission and gear box, blades were completely detached from helicopter. Left skid was also broke and detached from airframe. There were no mechanical irregularities with helicopter at time of accident according to pilot.

1. A/c heading at time of accident was 308 degrees

2. A/c rolled approximately 12 feet to the right.

3. A/c position after accident was on it's right side still heading approximately 308 degrees.

As the FAA filed it

STUDENT PILOT WAS ON SECOND SOLO FLIGHT OF THE DAY. WHEN THE COLLECTIVE WAS APPLIED THE HELICOPTER BECAME LIGHT ON THE SKIDS AND STARTED TO HOVER THE HELICOPTER ROLLED RIGHT, THE STUDENT CORRECTED WITH A LEFT CYCLIC MOVEMENT WHICH CAUSED LEFT SKID TO CONTACT THE GROUND. THE HELICOPTER ROLLED BACK TO THE RIGHT ROLLING ON TO ITS SIDE AND CONTACTING THE GROUND WITH SUBSTANTIAL DAMAGE DONE TO THE HELICOPTER. TRANSMISSION AND GEAR BOX, BLADES WERE COMPLETELY DETACHED FROM HELICOPTER. LEFT SKID WAS ALSO BROKE AND DETACHED FROM AIRFRAME. THERE WERE NO MECHANICAL IRREGULARITIES WITH HELICOPTER AT TIME OF ACCIDENT ACCORDING TO PILOT.

1. A/C HEADING AT TIME OF ACCIDENT WAS 308 DEGREES

2. A/C ROLLED APPROXIMATELY 12 FEET TO THE RIGHT.

3. A/C POSITION AFTER ACCIDENT WAS ON IT'S RIGHT SIDE STILL HEADING APPROXIMATELY 308 DEGREES.

NTSB investigation

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