20060608012339A

Accident · Minor damage

FAA accident report · Hiller FH-1100 · Navarre Beach, FL · June 8, 2006

Date
June 8, 2006 · 12:32 local
Place
Navarre Beach, FL
Phase of flight
Pwr On Vertical Ldng/Rtrcrft
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N4035G
NTSB investigation
NTSBMIA06LA126
Reported as
Hiller FH1100
People aboard
2
Fatal injuries
0

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.

(-23) On June 8, 2006, at 1230 CDT, the pilot in command of N4035G, an FH-1100 helicopter departed from a private heliport at Navarre Beach Florida on a personal flight. Shortly after takeoff, the pilot heard a loud bang and felt a slight shudder in the airframe. He initiated an immediate descent and prior to landing discovered he had lost directional control, at which time he reduced power to idle and performed an autorotational landing to the Beach. One of the tail rotor blades departed the aircraft in flight and could not be located. The resulting out of balance condition caused the remainder of the tail rotor and the ninety degree gearbox to come off of its mounts and remained suspended from the tail by the control cable. The aircraft was landed successfully with no further damage. Investigation continues to determine cause of tail rotor failure.

As the FAA filed it

(-23) ON JUNE 8, 2006, AT 1230 CDT, THE PILOT IN COMMAND OF N4035G, AN FH-1100 HELICOPTER DEPARTED FROM A PRIVATE HELIPORT AT NAVARRE BEACH FLORIDA ON A PERSONAL FLIGHT. SHORTLY AFTER TAKEOFF, THE PILOT HEARD A LOUD BANG AND FELT A SLIGHT SHUDDER IN THE AIRFRAME. HE INITIATED AN IMMEDIATE DESCENT AND PRIOR TO LANDING DISCOVERED HE HAD LOST DIRECTIONAL CONTROL, AT WHICH TIME HE REDUCED POWER TO IDLE AND PERFORMED AN AUTOROTATIONAL LANDING TO THE BEACH. ONE OF THE TAIL ROTOR BLADES DEPARTED THE AIRCRAFT IN FLIGHT AND COULD NOT BE LOCATED. THE RESULTING OUT OF BALANCE CONDITION CAUSED THE REMAINDER OF THE TAIL ROTOR AND THE NINETY DEGREE GEARBOX TO COME OFF OF ITS MOUNTS AND REMAINED SUSPENDED FROM THE TAIL BY THE CONTROL CABLE. THE AIRCRAFT WAS LANDED SUCCESSFULLY WITH NO FURTHER DAMAGE. INVESTIGATION CONTINUES TO DETERMINE CAUSE OF TAIL ROTOR FAILURE.

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 N4035G · 2

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