20010506008929A

Accident · Substantial damage

FAA accident report · Bbavia 11AC · Brewer, ME · May 6, 2001

Date
May 6, 2001 · 13:45 local
Place
Brewer, ME
Airport
Brewer Airport
Phase of flight
Forced/Precautionary Landing
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N9267E
NTSB investigation
NTSBNYC01LA118
Reported as
Bbavia 11AC
Reported engine
Lycoming O235*
Fatal injuries
0
Pilot’s flight hours
147 total30 in this make and model22 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)Aircraft was taking off from rumway 19 when at 200-250 feet the engine quit. Pilot proceeded to push the nose over and slip the aircraft. At approximately 50 feet the aircraft stalled and impacted the turf runway. Upon impacting the runway the aircraft spun around 180 degrees facing the opposite direction of take-off. Pilot was removed from aircraft by witnesses at airport. Pilot received minor injuries and was transported by local EMS to hospital and released. The aircraft was destroyed. Inspection of the aircraft at the accident site revealed there was no evidence of fuel in the forward tank. There was no sign of fuel spillage or odor of fuel at the crash site. The aircraft fuel system remained intact after the crash. All other engine functions were normal. (.4) the pilot stated that during preflight, he saw fuel in both the forward and aft fuel tanks. He hand-propped the engine, and after startup, conducted two engine runups, then took off. During the climb, between 150 feet and 200 feet of altitude, the engine and propeller stopped running. The pilot attempted to slip the airplane back onto the grass runway; however, it sta lled, then impacted the ground and spun around, about 180 degrees. The fuel system was not compromised. The forward fuel tank was empty, and the aft fuel tank contained an unknown quantity of fuel. Small amounts of fuel were also found in the gascolator and carburetor. During climbs, fuel could only be drawn from the forward tank.

As the FAA filed it

(-23)AIRCRAFT WAS TAKING OFF FROM RUMWAY 19 WHEN AT 200-250 FEET THE ENGINE QUIT. PILOT PROCEEDED TO PUSH THE NOSE OVER AND SLIP THE AIRCRAFT. AT APPROXIMATELY 50 FEET THE AIRCRAFT STALLED AND IMPACTED THE TURF RUNWAY. UPON IMPACTING THE RUNWAY THE AIRCRAFT SPUN AROUND 180 DEGREES FACING THE OPPOSITE DIRECTION OF TAKE-OFF. PILOT WAS REMOVED FROM AIRCRAFT BY WITNESSES AT AIRPORT. PILOT RECEIVED MINOR INJURIES AND WAS TRANSPORTED BY LOCAL EMS TO HOSPITAL AND RELEASED. THE AIRCRAFT WAS DESTROYED. INSPECTION OF THE AIRCRAFT AT THE ACCIDENT SITE REVEALED THERE WAS NO EVIDENCE OF FUEL IN THE FORWARD TANK. THERE WAS NO SIGN OF FUEL SPILLAGE OR ODOR OF FUEL AT THE CRASH SITE. THE AIRCRAFT FUEL SYSTEM REMAINED INTACT AFTER THE CRASH. ALL OTHER ENGINE FUNCTIONS WERE NORMAL. (.4) THE PILOT STATED THAT DURING PREFLIGHT, HE SAW FUEL IN BOTH THE FORWARD AND AFT FUEL TANKS. HE HAND-PROPPED THE ENGINE, AND AFTER STARTUP, CONDUCTED TWO ENGINE RUNUPS, THEN TOOK OFF. DURING THE CLIMB, BETWEEN 150 FEET AND 200 FEET OF ALTITUDE, THE ENGINE AND PROPELLER STOPPED RUNNING. THE PILOT ATTEMPTED TO SLIP THE AIRPLANE BACK ONTO THE GRASS RUNWAY; HOWEVER, IT STA LLED, THEN IMPACTED THE GROUND AND SPUN AROUND, ABOUT 180 DEGREES. THE FUEL SYSTEM WAS NOT COMPROMISED. THE FORWARD FUEL TANK WAS EMPTY, AND THE AFT FUEL TANK CONTAINED AN UNKNOWN QUANTITY OF FUEL. SMALL AMOUNTS OF FUEL WERE ALSO FOUND IN THE GASCOLATOR AND CARBURETOR. DURING CLIMBS, FUEL COULD ONLY BE DRAWN FROM THE FORWARD TANK.

NTSB investigation

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