20100831045969A

Accident · Substantial damage

FAA accident report · Bird CK · Eagles Mere, PA · August 31, 2010

Date
August 31, 2010 · 10:30 local
Place
Eagles Mere, PA
Airport
Eagles Mere Airport
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N765N
NTSB investigation
NTSBERA10LA458
Reported as
Bird CK
Reported engine
KINNER B-54
People aboard
1
Fatal injuries
0
Other injuries
1
Pilot’s certificate
Private pilot
Pilot’s flight hours
1,500 total3 in this make and model80 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.

During take off climb at 200 feet AGL the pilot experienced an engine failure. A forced, on airport, landing was made. Before touching down, the aircraft entered a full stall, at 25 feet AGL, resulting in hard landing damage to the landing gear, engine, propeller and wings. During landing roll further damage was caused to the aft fuselage, tail wheel and elevators from contact with a fence post. A post accident examination revealed large sheets of randolph 802 sealant had collected in the main fuel tank sump area. The loose sealant was large enough to restrict fuel flow into the firewall fuel system strainer, resulting in fuel starvation.

As the FAA filed it

DURING TAKE OFF CLIMB AT 200 FEET AGL THE PILOT EXPERIENCED AN ENGINE FAILURE. A FORCED, ON AIRPORT, LANDING WAS MADE. BEFORE TOUCHING DOWN, THE AIRCRAFT ENTERED A FULL STALL, AT 25 FEET AGL, RESULTING IN HARD LANDING DAMAGE TO THE LANDING GEAR, ENGINE, PROPELLER AND WINGS. DURING LANDING ROLL FURTHER DAMAGE WAS CAUSED TO THE AFT FUSELAGE, TAIL WHEEL AND ELEVATORS FROM CONTACT WITH A FENCE POST. A POST ACCIDENT EXAMINATION REVEALED LARGE SHEETS OF RANDOLPH 802 SEALANT HAD COLLECTED IN THE MAIN FUEL TANK SUMP AREA. THE LOOSE SEALANT WAS LARGE ENOUGH TO RESTRICT FUEL FLOW INTO THE FIREWALL FUEL SYSTEM STRAINER, RESULTING IN FUEL STARVATION.

NTSB investigation

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