20200312000699A

Accident · Destroyed

FAA accident report · Piper PA-28-181 · Danvers, MA · March 12, 2020

Date
March 12, 2020 · 16:22 local
Place
Danvers, MA
Airport
Beverly Municipal
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N656ST
NTSB investigation
NTSBERA20LA126
Reported as
Piper PA-28-181
Reported engine
Lycoming O-360-A4M
People aboard
1
Fatal injuries
0
Other injuries
1
Pilot’s certificate
Student
Pilot’s flight hours
38 total38 in this make and model16 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.

N656ST was conducting touch-and-go landings on runway 16. During the 5th takeoff, the pilot heard and felt a reduction of power from the engine at approximately 400-500? MSL. The pilot stated the RPM was at 2400RPM and was decreasing. The pilot requested runway 27 for landing. Based on airport surveillance video, N656ST touched down with approximately 275? Of runway remaining. The aircraft departed the end of the runway into a grass area and became airborne once again when the aircraft encountered a 15? Cliff off the end of runway 27. The aircraft came to rest about 5? Off the ground in a tree approximately 500? From the departure end of runway 27 and 100? North of the runway centerline. The right wing of the aircraft separated from the fuselage and was pinned vertically between the tree and the fuselage. The pilot sustained minor cuts to his right hand. The weather at the time of the incident was reported as winds from 120 degrees at 5 knots, 10 statute miles visibility, scattered clouds at 6,500?, overcast at 7,900?, and a temperature of 7 degrees celsius with a dewpoint of 1 degree celsius. The aircraft had an estimated 35 gallons of fuel on board at the time of the accident with approximately 18 gallons of fuel recovered from the left fuel tank. Most of the fuel remaining in the right tank leaked out when the fuel lines were severed during the accident sequence. There was a substantial amount of fuel visible in the snow under the aircraft. The propeller sustained damage only from impact with the tree and the damage indicated the propeller was not rotating at the time of impact.

As the FAA filed it

N656ST WAS CONDUCTING TOUCH-AND-GO LANDINGS ON RUNWAY 16. DURING THE 5TH TAKEOFF, THE PILOT HEARD AND FELT A REDUCTION OF POWER FROM THE ENGINE AT APPROXIMATELY 400-500? MSL. THE PILOT STATED THE RPM WAS AT 2400RPM AND WAS DECREASING. THE PILOT REQUESTED RUNWAY 27 FOR LANDING. BASED ON AIRPORT SURVEILLANCE VIDEO, N656ST TOUCHED DOWN WITH APPROXIMATELY 275? OF RUNWAY REMAINING. THE AIRCRAFT DEPARTED THE END OF THE RUNWAY INTO A GRASS AREA AND BECAME AIRBORNE ONCE AGAIN WHEN THE AIRCRAFT ENCOUNTERED A 15? CLIFF OFF THE END OF RUNWAY 27. THE AIRCRAFT CAME TO REST ABOUT 5? OFF THE GROUND IN A TREE APPROXIMATELY 500? FROM THE DEPARTURE END OF RUNWAY 27 AND 100? NORTH OF THE RUNWAY CENTERLINE. THE RIGHT WING OF THE AIRCRAFT SEPARATED FROM THE FUSELAGE AND WAS PINNED VERTICALLY BETWEEN THE TREE AND THE FUSELAGE. THE PILOT SUSTAINED MINOR CUTS TO HIS RIGHT HAND. THE WEATHER AT THE TIME OF THE INCIDENT WAS REPORTED AS WINDS FROM 120 DEGREES AT 5 KNOTS, 10 STATUTE MILES VISIBILITY, SCATTERED CLOUDS AT 6,500?, OVERCAST AT 7,900?, AND A TEMPERATURE OF 7 DEGREES CELSIUS WITH A DEWPOINT OF 1 DEGREE CELSIUS. THE AIRCRAFT HAD AN ESTIMATED 35 GALLONS OF FUEL ON BOARD AT THE TIME OF THE ACCIDENT WITH APPROXIMATELY 18 GALLONS OF FUEL RECOVERED FROM THE LEFT FUEL TANK. MOST OF THE FUEL REMAINING IN THE RIGHT TANK LEAKED OUT WHEN THE FUEL LINES WERE SEVERED DURING THE ACCIDENT SEQUENCE. THERE WAS A SUBSTANTIAL AMOUNT OF FUEL VISIBLE IN THE SNOW UNDER THE AIRCRAFT. THE PROPELLER SUSTAINED DAMAGE ONLY FROM IMPACT WITH THE TREE AND THE DAMAGE INDICATED THE PROPELLER WAS NOT ROTATING AT THE TIME OF IMPACT.

NTSB investigation

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