20160804018369A

Accident · Substantial damage

FAA accident report · Gordon Gilchrist PA14 EXP · Sparta, MI · August 4, 2016

Date
August 4, 2016 · 20:20 local
Place
Sparta, MI
Airport
Paul C. Miller-Sparta
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N18PG
NTSB investigation
NTSBCEN16LA305
Reported as
Gordon Gilchrist PA14 EXP
Reported engine
Aerosport O-375-A1A
People aboard
2
Fatal injuries
0
Other injuries
2
Pilot’s certificate
Private pilot
Pilot’s flight hours
900 total46 in this make and model46 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.

On August 4, 2016 about 2020 eastern daylight time, an experimental amateur built PA-14EXP amphibious aircraft, N18PH, sustained substantial damage when it struck the Sparta Michigan airport perimeter fence and nosed over during a forced landing. The pilot stated the accident occurred following a loss of engine power during initial climb after takeoff from runway 25. The pilot and passenger received minor injuries. The airplane was registered to and operated by the pilot under the provisions of 14 code of federal regulations part 91 as a personal flight. Visual meteorological conditions prevailed for the flight.

As the FAA filed it

ON AUGUST 4, 2016 ABOUT 2020 EASTERN DAYLIGHT TIME, AN EXPERIMENTAL AMATEUR BUILT PA-14EXP AMPHIBIOUS AIRCRAFT, N18PH, SUSTAINED SUBSTANTIAL DAMAGE WHEN IT STRUCK THE SPARTA MICHIGAN AIRPORT PERIMETER FENCE AND NOSED OVER DURING A FORCED LANDING. THE PILOT STATED THE ACCIDENT OCCURRED FOLLOWING A LOSS OF ENGINE POWER DURING INITIAL CLIMB AFTER TAKEOFF FROM RUNWAY 25. THE PILOT AND PASSENGER RECEIVED MINOR INJURIES. THE AIRPLANE WAS REGISTERED TO AND OPERATED BY THE PILOT UNDER THE PROVISIONS OF 14 CODE OF FEDERAL REGULATIONS PART 91 AS A PERSONAL FLIGHT. VISUAL METEOROLOGICAL CONDITIONS PREVAILED FOR THE FLIGHT.

NTSB investigation

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