20160326024449A

Accident · Substantial damage

FAA accident report · Enstrom F280 · Sodus, NY · March 26, 2016

Date
March 26, 2016 · 10:45 local
Place
Sodus, NY
Airport
Williamson-Sodus
Phase of flight
Landing: Rollout
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N5698Y
NTSB investigation
NTSBGAA16CA163
Reported as
Enstrom F280
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Commercial pilot, flight instructor
Pilot’s flight hours
3,847 total151 in this make and model44 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 flight instructor reported that he asked the pilot receiving instruction to demonstrate a run-on landing on the sod between the runway and taxiway. He reported that as the helicopter touched down at about 25 miles per hour (21.72 knots), the pilot lowered the collective to the full down position while the helicopter was still moving forward with considerable momentum. The helicopter began to "lurch forward" and the nose of the helicopter started to lower. The flight instructor then came on the flight controls, but the helicopter had progressed to an "extreme nose low attitude," and he applied aft cyclic to prevent the main rotor blades from impacting terrain. The main rotor blades instead impacted and separated the tailboom. The fuselage continued moving forward and the nose impacted terrain and then settled back on the skids. The helicopter sustained substantial damage to the fuselage, main rotor system, tailboom, and tail rotor system.

As the FAA filed it

THE FLIGHT INSTRUCTOR REPORTED THAT HE ASKED THE PILOT RECEIVING INSTRUCTION TO DEMONSTRATE A RUN-ON LANDING ON THE SOD BETWEEN THE RUNWAY AND TAXIWAY. HE REPORTED THAT AS THE HELICOPTER TOUCHED DOWN AT ABOUT 25 MILES PER HOUR (21.72 KNOTS), THE PILOT LOWERED THE COLLECTIVE TO THE FULL DOWN POSITION WHILE THE HELICOPTER WAS STILL MOVING FORWARD WITH CONSIDERABLE MOMENTUM. THE HELICOPTER BEGAN TO "LURCH FORWARD" AND THE NOSE OF THE HELICOPTER STARTED TO LOWER. THE FLIGHT INSTRUCTOR THEN CAME ON THE FLIGHT CONTROLS, BUT THE HELICOPTER HAD PROGRESSED TO AN "EXTREME NOSE LOW ATTITUDE," AND HE APPLIED AFT CYCLIC TO PREVENT THE MAIN ROTOR BLADES FROM IMPACTING TERRAIN. THE MAIN ROTOR BLADES INSTEAD IMPACTED AND SEPARATED THE TAILBOOM. THE FUSELAGE CONTINUED MOVING FORWARD AND THE NOSE IMPACTED TERRAIN AND THEN SETTLED BACK ON THE SKIDS. THE HELICOPTER SUSTAINED SUBSTANTIAL DAMAGE TO THE FUSELAGE, MAIN ROTOR SYSTEM, TAILBOOM, AND TAIL ROTOR SYSTEM.

NTSB investigation

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