20101011052009A

Accident · Substantial damage

FAA accident report · Grumman G-164 · Michigan, ND · October 11, 2010

Date
October 11, 2010 · 14:00 local
Place
Michigan, ND
Phase of flight
Takeoff: Rotation
Operating rules
Agricultural (Part 137)
Damage
Substantial damage
Aircraft
N554Y
NTSB investigation
NTSBCEN11CA071
Reported as
Grumman G-164
Reported engine
Pratt & Whitney R-985 series
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s flight hours
0 total0 in this make and model0 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.

Airman stated that in his attempt to take off on his easterly runway the aircraft seemed to be low on power but that all engine instruments were normal. He decided to attempt the takeoff anyway. He stated that he realized to late that the aircraft probably wouldn't stay in the air if it made it into the air so he pulled the dump handle. The aircraft dumpedabout 40 or so gallons of the 150 gallon load and became airborn approximately 300 feet shortof the runway end. The aircraft climbed out of ground effect and then lost all power. The airman stated that he then shoved the nose over hard and struck the overrun area of the strip hard smashing the engine, propeller, and damaging the right main gear. As the aircraft started to loose energy it flipped side for side and came to a rest, inverted, in the swamp approximately 30 yards to right and 100 yards past the end of the runway, in 16 inches of swamp water. The aircraft has substantial damage. There were no injuries reported. Subsequent investigation of the aircraft and engine: it was determined that at least one cylinder was dead and possibly a second. At the time of the inspection the right magneto was also found inoperative. Fuel colllected from the aircraft appeared normal.

As the FAA filed it

AIRMAN STATED THAT IN HIS ATTEMPT TO TAKE OFF ON HIS EASTERLY RUNWAY THE AIRCRAFT SEEMED TO BE LOW ON POWER BUT THAT ALL ENGINE INSTRUMENTS WERE NORMAL. HE DECIDED TO ATTEMPT THE TAKEOFF ANYWAY. HE STATED THAT HE REALIZED TO LATE THAT THE AIRCRAFT PROBABLY WOULDN'T STAY IN THE AIR IF IT MADE IT INTO THE AIR SO HE PULLED THE DUMP HANDLE. THE AIRCRAFT DUMPEDABOUT 40 OR SO GALLONS OF THE 150 GALLON LOAD AND BECAME AIRBORN APPROXIMATELY 300 FEET SHORTOF THE RUNWAY END. THE AIRCRAFT CLIMBED OUT OF GROUND EFFECT AND THEN LOST ALL POWER. THE AIRMAN STATED THAT HE THEN SHOVED THE NOSE OVER HARD AND STRUCK THE OVERRUN AREA OF THE STRIP HARD SMASHING THE ENGINE, PROPELLER, AND DAMAGING THE RIGHT MAIN GEAR.AS THE AIRCRAFT STARTED TO LOOSE ENERGY IT FLIPPED SIDE FOR SIDE AND CAME TO A REST, INVERTED, IN THE SWAMP APPROXIMATELY 30 YARDS TO RIGHT AND 100 YARDS PAST THE END OF THE RUNWAY, IN 16 INCHES OF SWAMP WATER.THE AIRCRAFT HAS SUBSTANTIAL DAMAGE. THERE WERE NO INJURIES REPORTED. SUBSEQUENT INVESTIGATION OF THE AIRCRAFT AND ENGINE: IT WAS DETERMINED THAT AT LEAST ONE CYLINDER WAS DEAD AND POSSIBLY A SECOND. AT THE TIME OF THE INSPECTION THE RIGHT MAGNETO WAS ALSO FOUND INOPERATIVE. FUEL COLLLECTED FROM THE AIRCRAFT APPEARED NORMAL.

NTSB investigation

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