20071108826399A

Accident · Substantial damage

FAA accident report · Hughes 269C · Baker City, OR · November 8, 2007

Date
November 8, 2007 · 13:00 local
Place
Baker City, OR
Airport
Baker City Municipal
Phase of flight
Climb
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N381MC
NTSB investigation
NTSBSEA08FA022
Reported as
Hughes 269C
Reported engine
Lycoming HIO360D1A
People aboard
1
Fatal injuries
1
Pilot’s flight hours
2,071 total62 in this make and model27 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) Experienced fixed wing pilot in training as a student in rotorcraft helicopter on a solo flight was observed by eyewitnesses to depart the airport to the north. Between about 800-1500 feet above the ground, the witnesses described the helicopter falling tail first to the ground. Post crash investigation found evidence of the helicopter impacting the ground from a vertical descent, left skid first, slightly tail low. The main rotor and the tail rotor appeared to have not been rotating. Inspection of the engine oil filter showed evidence of copper. The last oil change was noted to be 8.6 hours before the accident flight with no copper noted. Maintenance records showed no evidence of abnormal engine operation. The engine will be examined by a team of investigators on December 13, 2007.

As the FAA filed it

(-23) EXPERIENCED FIXED WING PILOT IN TRAINING AS A STUDENT IN ROTORCRAFT HELICOPTER ON A SOLO FLIGHT WAS OBSERVED BY EYEWITNESSES TO DEPART THE AIRPORT TO THE NORTH. BETWEEN ABOUT 800-1500 FEET ABOVE THE GROUND, THE WITNESSES DESCRIBED THE HELICOPTER FALLING TAIL FIRST TO THE GROUND. POST CRASH INVESTIGATION FOUND EVIDENCE OF THE HELICOPTER IMPACTING THE GROUND FROM A VERTICAL DESCENT, LEFT SKID FIRST, SLIGHTLY TAIL LOW. THE MAIN ROTOR AND THE TAIL ROTOR APPEARED TO HAVE NOT BEEN ROTATING. INSPECTION OF THE ENGINE OIL FILTER SHOWED EVIDENCE OF COPPER. THE LAST OIL CHANGE WAS NOTED TO BE 8.6 HOURS BEFORE THE ACCIDENT FLIGHT WITH NO COPPER NOTED. MAINTENANCE RECORDS SHOWED NO EVIDENCE OF ABNORMAL ENGINE OPERATION. THE ENGINE WILL BE EXAMINED BY A TEAM OF INVESTIGATORS ON DECEMBER 13, 2007.

NTSB investigation

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