20180613007719A

Accident · Substantial damage

FAA accident report · Schweizer 269C · North Las Vegas, NV · June 13, 2018

Date
June 13, 2018 · 10:59 local
Place
North Las Vegas, NV
Phase of flight
Run-Up Area
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N557DC
NTSB investigation
NTSBWPR18LA170
Reported as
Schweizer 269C
Reported engine
Lycoming HIO-360 series
People aboard
1
Fatal injuries
0
Other injuries
1
Pilot’s certificates
Commercial pilot, private pilot
Pilot’s flight hours
75 total72 in this make and model4 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.

On June 13, 2018 at approximately 1146 PST, at North Las Vegas airport (kvgt), a 1993 Schweizer 269C sustained substantial damage due to ground resonance.

The aircraft was parked on the south ramp in a marked helicopter pad where the pilot was preparing to lift into a hover. The pilot stated the helicopter began to vibrate prior to becoming light on the skids. As the vibrations increased, the pilot lowered the collective and rolled off the throttle.

The pilot reported that the vibrations became even more severe for approximately 20 to 40 seconds until the rotor blades came to a stop due to substantial damage caused by the vibrations.

An inspection of the four landing gear dampers and the only undamged rotor oleo elastomeric damper, all tested within allowed tolerances.

As the FAA filed it

ON JUNE 13, 2018 AT APPROXIMATELY 1146 PST, AT NORTH LAS VEGAS AIRPORT (KVGT), A 1993 SCHWEIZER 269C SUSTAINED SUBSTANTIAL DAMAGE DUE TO GROUND RESONANCE.

THE AIRCRAFT WAS PARKED ON THE SOUTH RAMP IN A MARKED HELICOPTER PAD WHERE THE PILOT WAS PREPARING TO LIFT INTO A HOVER. THE PILOT STATED THE HELICOPTER BEGAN TO VIBRATE PRIOR TO BECOMING LIGHT ON THE SKIDS. AS THE VIBRATIONS INCREASED, THE PILOT LOWERED THE COLLECTIVE AND ROLLED OFF THE THROTTLE.

THE PILOT REPORTED THAT THE VIBRATIONS BECAME EVEN MORE SEVERE FOR APPROXIMATELY 20 TO 40 SECONDS UNTIL THE ROTOR BLADES CAME TO A STOP DUE TO SUBSTANTIAL DAMAGE CAUSED BY THE VIBRATIONS.

AN INSPECTION OF THE FOUR LANDING GEAR DAMPERS AND THE ONLY UNDAMGED ROTOR OLEO ELASTOMERIC DAMPER, ALL TESTED WITHIN ALLOWED TOLERANCES.

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 N557DC · 3

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