What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
Aircraft crashed on takeoff into water approximately 200 yards from departure end of runway 5.
Aircraft appeared to have cartwheeled damaging both wings and lower engine cowl. Aircraft came to rest on a mud bank partially submerged at high tide (sea water).
Aircraft was destroyed during the recovery effort remaining completely submerged in sea water for approximately two days during the recovery.
After recovery, inspection revealed left fuel tank ruptured and empty, right fuel tank ½ full, aux tank in aft baggage compartment full. Damage to both wings includes wing spar damage approximately three feet in from each wing tip (not including tip caps). Due to damage to the airframe during recovery, flight control continuity was not possible.
There was approximately fifteen pounds of oil, tools, and a variety of miscellaneous equipment found in the rear baggage compartment.
Engine inspection revealed the following; engine was torn off during recovery effort therefore engine control continuity was not possible. All upper spark plugs were removed to verify compression via thumb pressure over spark plug hole. Number three and four cylinders were noted to have no compression. Removed all valve covers and noted that number four cylinder exhaust valve was stuck in the open position. No anomalies were noted on the number three cylinder and remaining valve train.
Propeller turned freely and the magneto impulse coupling could be heard clicking but no spark verified due to water intrusion.
Interview with the pilot and passengers revealed that he had recently fueled the aircraft to full on all three tanks (wings and aux, oct. 10, 2016 at X60) and had the intent of flying to new hampshire on the accident date. Pilot and passengers stated that they had in total approximately twenty pounds of personal items on board the aircraft.
After interviewing the pilot and passengers, they stated that the engine seemed to be running fine but the aircraft would not climb above 100 feet. All statements and evidence are consistent with an overloaded aircraft and stall.
Aircraft maintenance documents were not made available to the FAA.
Pilot was unable to produce an airman certificate on the day of the accident, investigation revealed that the pilots airman certificate was revoked in 1997, and the last third class medical on record is in 2009.
As the FAA filed it
AIRCRAFT CRASHED ON TAKEOFF INTO WATER APPROXIMATELY 200 YARDS FROM DEPARTURE END OF RUNWAY 5.
AIRCRAFT APPEARED TO HAVE CARTWHEELED DAMAGING BOTH WINGS AND LOWER ENGINE COWL. AIRCRAFT CAME TO REST ON A MUD BANK PARTIALLY SUBMERGED AT HIGH TIDE (SEA WATER).
AIRCRAFT WAS DESTROYED DURING THE RECOVERY EFFORT REMAINING COMPLETELY SUBMERGED IN SEA WATER FOR APPROXIMATELY TWO DAYS DURING THE RECOVERY.
AFTER RECOVERY, INSPECTION REVEALED LEFT FUEL TANK RUPTURED AND EMPTY, RIGHT FUEL TANK ½ FULL, AUX TANK IN AFT BAGGAGE COMPARTMENT FULL. DAMAGE TO BOTH WINGS INCLUDES WING SPAR DAMAGE APPROXIMATELY THREE FEET IN FROM EACH WING TIP (NOT INCLUDING TIP CAPS). DUE TO DAMAGE TO THE AIRFRAME DURING RECOVERY, FLIGHT CONTROL CONTINUITY WAS NOT POSSIBLE.
THERE WAS APPROXIMATELY FIFTEEN POUNDS OF OIL, TOOLS, AND A VARIETY OF MISCELLANEOUS EQUIPMENT FOUND IN THE REAR BAGGAGE COMPARTMENT.
ENGINE INSPECTION REVEALED THE FOLLOWING; ENGINE WAS TORN OFF DURING RECOVERY EFFORT THEREFORE ENGINE CONTROL CONTINUITY WAS NOT POSSIBLE. ALL UPPER SPARK PLUGS WERE REMOVED TO VERIFY COMPRESSION VIA THUMB PRESSURE OVER SPARK PLUG HOLE. NUMBER THREE AND FOUR CYLINDERS WERE NOTED TO HAVE NO COMPRESSION. REMOVED ALL VALVE COVERS AND NOTED THAT NUMBER FOUR CYLINDER EXHAUST VALVE WAS STUCK IN THE OPEN POSITION. NO ANOMALIES WERE NOTED ON THE NUMBER THREE CYLINDER AND REMAINING VALVE TRAIN.
PROPELLER TURNED FREELY AND THE MAGNETO IMPULSE COUPLING COULD BE HEARD CLICKING BUT NO SPARK VERIFIED DUE TO WATER INTRUSION.
INTERVIEW WITH THE PILOT AND PASSENGERS REVEALED THAT HE HAD RECENTLY FUELED THE AIRCRAFT TO FULL ON ALL THREE TANKS (WINGS AND AUX, OCT. 10, 2016 AT X60) AND HAD THE INTENT OF FLYING TO NEW HAMPSHIRE ON THE ACCIDENT DATE. PILOT AND PASSENGERS STATED THAT THEY HAD IN TOTAL APPROXIMATELY TWENTY POUNDS OF PERSONAL ITEMS ON BOARD THE AIRCRAFT.
AFTER INTERVIEWING THE PILOT AND PASSENGERS, THEY STATED THAT THE ENGINE SEEMED TO BE RUNNING FINE BUT THE AIRCRAFT WOULD NOT CLIMB ABOVE 100 FEET. ALL STATEMENTS AND EVIDENCE ARE CONSISTENT WITH AN OVERLOADED AIRCRAFT AND STALL.
AIRCRAFT MAINTENANCE DOCUMENTS WERE NOT MADE AVAILABLE TO THE FAA.
PILOT WAS UNABLE TO PRODUCE AN AIRMAN CERTIFICATE ON THE DAY OF THE ACCIDENT, INVESTIGATION REVEALED THAT THE PILOTS AIRMAN CERTIFICATE WAS REVOKED IN 1997, AND THE LAST THIRD CLASS MEDICAL ON RECORD IS IN 2009.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.
Other reports on N1827Y · 2
Matched to the same aircraft by N-number and date.