20080527838579A

Accident · Substantial damage

FAA accident report · Scwzer 269C · Gardendale, AL · May 27, 2008

Date
May 27, 2008 · 11:00 local
Place
Gardendale, AL
Airport
Parker Field
Phase of flight
Pwr On Vertical Ldng/Rtrcrft
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N368HF
NTSB investigation
NTSBNYC08CA195
Reported as
Scwzer 269C
Fatal injuries
0
Pilot’s flight hours
2,100 total150 in this make and model30 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)The pilot in command (flight instructor) stated that when he attempted to land the helicopter from a hover, the helicopter encountered what he identified as ground resonance. The pilot stated that he rolled the throttle off immediately. This improper action caused the ground resonance to intensify resulting in substantial damage to the airframe, tailboom skid landing gear, main and tail rotor blades and sudden stoppage to the engine, transmission and drive train. The occupants egressed through the right cabin entrance door. A small fire broke out as a result of engine oil on the hot exhaust. One occupant received minor cuts to the right arm and hand requiring stitches.

As the FAA filed it

(-23)THE PILOT IN COMMAND (FLIGHT INSTRUCTOR) STATED THAT WHEN HE ATTEMPTED TO LAND THE HELICOPTER FROM A HOVER, THE HELICOPTER ENCOUNTERED WHAT HE IDENTIFIED AS GROUND RESONANCE. THE PILOT STATED THAT HE ROLLED THE THROTTLE OFF IMMEDIATELY. THIS IMPROPER ACTION CAUSED THE GROUND RESONANCE TO INTENSIFY RESULTING IN SUBSTANTIAL DAMAGE TO THE AIRFRAME, TAILBOOM SKID LANDING GEAR, MAIN AND TAIL ROTOR BLADES AND SUDDEN STOPPAGE TO THE ENGINE, TRANSMISSION AND DRIVE TRAIN. THE OCCUPANTS EGRESSED THROUGH THE RIGHT CABIN ENTRANCE DOOR. A SMALL FIRE BROKE OUT AS A RESULT OF ENGINE OIL ON THE HOT EXHAUST. ONE OCCUPANT RECEIVED MINOR CUTS TO THE RIGHT ARM AND HAND REQUIRING STITCHES.

NTSB investigation

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