20200425006109A

Accident · Substantial damage

FAA accident report · Piper PA-28-151 · East Hampton, NY · April 25, 2020

Date
April 25, 2020 · 13:15 local
Place
East Hampton, NY
Airport
East Hampton
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N33005
NTSB investigation
NTSBERA20LA163
Reported as
Piper PA-28-151
Reported engine
Lycoming 0-320 series
People aboard
3
Fatal injuries
0
Other injuries
0

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 April 25, at approximately 1315L, 1715Z, a single engine aircraft, PA-28-151, N33005 departed rwy 28 at East Hampton, new york (hto). VFR conditions were reported and shortly after takeoff, at approximately 400 feet, pilot felt the engine vibration, turned around and landed rwy 10. Aircraft landed long and went through a fence and sustained substantial damage. There were 3 people on board (pilot and 2 passengers). No injuries were reported.

Visual inspection summary: opened top engine cowling no visual damaged noted. No oil or fuel leaks were noted. Engine oil on dipstick showed correct level and was clean. Visually inspected engine throttle, mixture and carburetor heat controls were intact and showed correct movement. No binding. Sumped left and right fuel tanks showed no FOD or water contamination. Fuel strainer showed no FOD or water. Opened fuel tank caps. Both tanks showed fuel just below tabs. Mechanic pulled prop through all four-compression strokes were evident with prop spring back. Owner attempted to started engine but noticed that the fuel selector was in the off position, selector was then turned on, boost pump switched on to prime engine. Engine started. Idle at 1200 RPM increased engine power to 1500 RPM. Engine ran normal no vibration or sputtering was noted. After about 5 to 8 minutes engine was shut down. Opened engine cowling no oil or fuel leakage were noted.

Based on the interview conducted with the pilot, she did not show lack of knowledge in the areas of operations and followed the aircraft manufacture's procedures

Reported weather was analyzed and carburetor icing does not appear to be the cause of the accident.

As the FAA filed it

ON APRIL 25, AT APPROXIMATELY 1315L, 1715Z, A SINGLE ENGINE AIRCRAFT, PA-28-151, N33005 DEPARTED RWY 28 AT EAST HAMPTON, NEW YORK (HTO). VFR CONDITIONS WERE REPORTED AND SHORTLY AFTER TAKEOFF, AT APPROXIMATELY 400 FEET, PILOT FELT THE ENGINE VIBRATION, TURNED AROUND AND LANDED RWY 10. AIRCRAFT LANDED LONG AND WENT THROUGH A FENCE AND SUSTAINED SUBSTANTIAL DAMAGE. THERE WERE 3 PEOPLE ON BOARD (PILOT AND 2 PASSENGERS). NO INJURIES WERE REPORTED.

VISUAL INSPECTION SUMMARY: OPENED TOP ENGINE COWLING NO VISUAL DAMAGED NOTED. NO OIL OR FUEL LEAKS WERE NOTED. ENGINE OIL ON DIPSTICK SHOWED CORRECT LEVEL AND WAS CLEAN. VISUALLY INSPECTED ENGINE THROTTLE, MIXTURE AND CARBURETOR HEAT CONTROLS WERE INTACT AND SHOWED CORRECT MOVEMENT. NO BINDING. SUMPED LEFT AND RIGHT FUEL TANKS SHOWED NO FOD OR WATER CONTAMINATION. FUEL STRAINER SHOWED NO FOD OR WATER. OPENED FUEL TANK CAPS. BOTH TANKS SHOWED FUEL JUST BELOW TABS. MECHANIC PULLED PROP THROUGH ALL FOUR-COMPRESSION STROKES WERE EVIDENT WITH PROP SPRING BACK. OWNER ATTEMPTED TO STARTED ENGINE BUT NOTICED THAT THE FUEL SELECTOR WAS IN THE OFF POSITION, SELECTOR WAS THEN TURNED ON, BOOST PUMP SWITCHED ON TO PRIME ENGINE. ENGINE STARTED. IDLE AT 1200 RPM INCREASED ENGINE POWER TO 1500 RPM. ENGINE RAN NORMAL NO VIBRATION OR SPUTTERING WAS NOTED. AFTER ABOUT 5 TO 8 MINUTES ENGINE WAS SHUT DOWN. OPENED ENGINE COWLING NO OIL OR FUEL LEAKAGE WERE NOTED.

BASED ON THE INTERVIEW CONDUCTED WITH THE PILOT, SHE DID NOT SHOW LACK OF KNOWLEDGE IN THE AREAS OF OPERATIONS AND FOLLOWED THE AIRCRAFT MANUFACTURE'S PROCEDURES

REPORTED WEATHER WAS ANALYZED AND CARBURETOR ICING DOES NOT APPEAR TO BE THE CAUSE OF THE ACCIDENT.

NTSB investigation

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