20070905824179A

Accident · Substantial damage

FAA accident report · Bell 206B · Lakeland, FL · September 5, 2007

Date
September 5, 2007 · 15:05 local
Place
Lakeland, FL
Airport
Lakeland Linder Regional
Phase of flight
Pwr On Vertical Ldng/Rtrcrft
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N267MW
NTSB investigation
NTSBMIA07LA148
Reported as
Bell 206B
People aboard
4
Fatal injuries
0
Pilot’s flight hours
6,414 total2,117 in this make and model90 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.

(-23) Pilot reported that just prior to touchdown, fifteen to twenty feet above the ground, the aircraft lost tail rotor effectiveness and spun around several times. He said he executed a hovering autorotation and landed the aircraft resulting in a hard landing. Examination of the aircraft revealed a bent forward cross tube, a bent aft cross tube, and structural damage to the fuselage in the area of the left aft cross tube attach point. No injuries were reported by the pilot or passengers. Further examination of the aircraft revealed a failure of the aft tail rotor driveshaft segment. The bond between the shaft and the forward attach flange had failed. Turning the rotor system through by hand showed continuity within the tail rotor system. But, when pressure was induced by turning the main rotor and holding the tail rotor, a loud bang was heard as the bond would intermittently fail. Tail rotor shaft assembly was sent to Bell helicopters by the NTSB.

As the FAA filed it

(-23) PILOT REPORTED THAT JUST PRIOR TO TOUCHDOWN, FIFTEEN TO TWENTY FEET ABOVE THE GROUND, THE AIRCRAFT LOST TAIL ROTOR EFFECTIVENESS AND SPUN AROUND SEVERAL TIMES. HE SAID HE EXECUTED A HOVERING AUTOROTATION AND LANDED THE AIRCRAFT RESULTING IN A HARD LANDING. EXAMINATION OF THE AIRCRAFT REVEALED A BENT FORWARD CROSS TUBE, A BENT AFT CROSS TUBE, AND STRUCTURAL DAMAGE TO THE FUSELAGE IN THE AREA OF THE LEFT AFT CROSS TUBE ATTACH POINT. NO INJURIES WERE REPORTED BY THE PILOT OR PASSENGERS. FURTHER EXAMINATION OF THE AIRCRAFT REVEALED A FAILURE OF THE AFT TAIL ROTOR DRIVESHAFT SEGMENT. THE BOND BETWEEN THE SHAFT AND THE FORWARD ATTACH FLANGE HAD FAILED. TURNING THE ROTOR SYSTEM THROUGH BY HAND SHOWED CONTINUITY WITHIN THE TAIL ROTOR SYSTEM. BUT, WHEN PRESSURE WAS INDUCED BY TURNING THE MAIN ROTOR AND HOLDING THE TAIL ROTOR, A LOUD BANG WAS HEARD AS THE BOND WOULD INTERMITTENTLY FAIL. TAIL ROTOR SHAFT ASSEMBLY WAS SENT TO BELL HELICOPTERS BY THE NTSB.

NTSB investigation

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