20090805012919A

Accident · Substantial damage

FAA accident report · Luscom 8A · Eatonville, WA · August 5, 2009

Date
August 5, 2009 · 20:30 local
Place
Eatonville, WA
Phase of flight
Cruise/Level Flight
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N28425
NTSB investigation
NTSBWPR09LA390
Reported as
Luscom 8A
Reported engine
Continental A65*
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s flight hours
107 total107 in this make and model50 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 reports that after approximately 1 hour flight time the aircraft started having problems. He stated that the engine stopped and would not re-start. He managed to glide the aircraft down and into a field. Upon touchdown the aircraft slid approximately 50 feet at which time the main landing gear collapsed. The external part of the main landing gear, propeller, engine, and wing tip areas were damaged in the crash however the aircraft hull appears to be intact. The pilot and passenger were examined by fire and rescue with the passenger being transported to a hospital due to a non-life threatening head injury. Examination of the crash site indicates fuel remained in the right tank with the fuel from the left tank most likely drained as a result of accident damage. Both left and right fuel tank valves were in the "on" or "open" position. Inspection of the aircraft and engine maintenance records indicate that the aircraft, engine and propeller were current. Examination of the wreckage confirm that the aircraft was well maintained. The owner/pilot had access to a hangar for aircraft storage. The aircraft certificate of airworthiness and registration were valid.

As the FAA filed it

(-23) THE PILOT REPORTS THAT AFTER APPROXIMATELY 1 HOUR FLIGHT TIME THE AIRCRAFT STARTED HAVING PROBLEMS. HE STATED THAT THE ENGINE STOPPED AND WOULD NOT RE-START. HE MANAGED TO GLIDE THE AIRCRAFT DOWN AND INTO A FIELD. UPON TOUCHDOWN THE AIRCRAFT SLID APPROXIMATELY 50 FEET AT WHICH TIME THE MAIN LANDING GEAR COLLAPSED. THE EXTERNAL PART OF THE MAIN LANDING GEAR, PROPELLER, ENGINE, AND WING TIP AREAS WERE DAMAGED IN THE CRASH HOWEVER THE AIRCRAFT HULL APPEARS TO BE INTACT. THE PILOT AND PASSENGER WERE EXAMINED BY FIRE AND RESCUE WITH THE PASSENGER BEING TRANSPORTED TO A HOSPITAL DUE TO A NON-LIFE THREATENING HEAD INJURY. EXAMINATION OF THE CRASH SITE INDICATES FUEL REMAINED IN THE RIGHT TANK WITH THE FUEL FROM THE LEFT TANK MOST LIKELY DRAINED AS A RESULT OF ACCIDENT DAMAGE. BOTH LEFT AND RIGHT FUEL TANK VALVES WERE IN THE "ON" OR "OPEN" POSITION. INSPECTION OF THE AIRCRAFT AND ENGINE MAINTENANCE RECORDS INDICATE THAT THE AIRCRAFT, ENGINE AND PROPELLER WERE CURRENT. EXAMINATION OF THE WRECKAGE CONFIRM THAT THE AIRCRAFT WAS WELL MAINTAINED. THE OWNER/PILOT HAD ACCESS TO A HANGAR FOR AIRCRAFT STORAGE. THE AIRCRAFT CERTIFICATE OF AIRWORTHINESS AND REGISTRATION WERE VALID.

NTSB investigation

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