20040616012659A

Accident · Substantial damage

FAA accident report · Amtr ROTORWAY162F · Hood River, OR · June 16, 2004

Date
June 16, 2004 · 11:30 local
Place
Hood River, OR
Airport
Hood River Airport
Phase of flight
Pwr Off Vert Land/Autorotate
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N717CS
NTSB investigation
NTSBSEA04CA107
Reported as
Amtr ROTORWAY162F
Reported engine
AMTRRW ROTWY162
People aboard
1
Fatal injuries
0
Pilot’s flight hours
6,500 total185 in this make and model88 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 elected to accomplish autorotation landing in a field due to low RPM and warning light. At touchdown the aircraft slowly rotated towards the nose and the main rotor blade made ground contact just to the left and forward of the ship. The aircraft slowly rolled over on its left side. There were no injuried to the pilot. Aircraft damage included a broken windshield, dented tail boom, broken left stabilizer, and damaged rotor blades. Investigation revealed that aircraft lost power due to fuel starvation. Pilot miscalculated fuel burn in that he didn't take into consideration the fuel burn required for a hotter than normal day.

As the FAA filed it

(-23) PILOT ELECTED TO ACCOMPLISH AUTOROTATION LANDING IN A FIELD DUE TO LOW RPM AND WARNING LIGHT. AT TOUCHDOWN THE AIRCRAFT SLOWLY ROTATED TOWARDS THE NOSE AND THE MAIN ROTOR BLADE MADE GROUND CONTACT JUST TO THE LEFT AND FORWARD OF THE SHIP. THE AIRCRAFT SLOWLY ROLLED OVER ON ITS LEFT SIDE. THERE WERE NO INJURIED TO THE PILOT. AIRCRAFT DAMAGE INCLUDED A BROKEN WINDSHIELD, DENTED TAIL BOOM, BROKEN LEFT STABILIZER, AND DAMAGED ROTOR BLADES. INVESTIGATION REVEALED THAT AIRCRAFT LOST POWER DUE TO FUEL STARVATION. PILOT MISCALCULATED FUEL BURN IN THAT HE DIDN'T TAKE INTO CONSIDERATION THE FUEL BURN REQUIRED FOR A HOTTER THAN NORMAL DAY.

NTSB investigation

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