20121012026649A

Accident · Substantial damage

FAA accident report · Piper PA-28-140 · Allentown, PA · October 12, 2012

Date
October 12, 2012 · 18:35 local
Place
Allentown, PA
Airport
Lehigh Valley International
Phase of flight
Takeoff: Climb Out
Operating rules
Pilot school (Part 141)
Operator
GU7A
Damage
Substantial damage
Aircraft
N15037
NTSB investigation
NTSBERA13LA025
Reported as
Piper PA-28-140
Reported engine
Lycoming 0-320 series
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Commercial pilot, flight instructor, private pilot
Pilot’s flight hours
1,106 total500 in this make and model200 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 October 12, 2012, about 1835 eastern daylight time, a Piper PA-28-140, N15037, operated by ace pilot training inc., was substantially damaged during a forced landing in a corn field following a partial loss of engine power during initial climb from Lehigh Valley International Airport (abe), Allentown, Pennsylvania. The certified flight instructor (CFI) and private pilot were not injured. The instructional flight was conducted under the provisions of 14 code of federal regulations part 91. Visual meteorological conditions prevailed and no flight plan was filed for the planned local flight. The CFI stated that the airplane was fueled to 36 gallons prior to the flight. The engine start-up, taxi, and run-up were normal. While departing from runway 31, about 200 feet above ground level, the CFI noticed that the throttle lever did not appear to be completely forward. He and the private pilot pushed the throttle lever full forward with resistance, which was followed by engine sputtering. The CFI then applied carburetor heat; however, the engine continued to sputter. He then elected to land in a corn field. During the landing, the engine firewall and right aileron were damaged. Upon examination and testing, which included engine runs and disassembly of components attached to the engine it was discovered that both magnetoes were defective. One had a loose gear and the other was missing approximately 1/3 of the teeth on a gear. Both magnetoes had been on the engine since overhauled by the manufacturer and had achieved 2,228 hours in service with no maintenance record entries showing any work being performed on them.

As the FAA filed it

ON OCTOBER 12, 2012, ABOUT 1835 EASTERN DAYLIGHT TIME, A PIPER PA-28-140, N15037, OPERATED BY ACE PILOT TRAINING INC., WAS SUBSTANTIALLY DAMAGED DURING A FORCED LANDING IN A CORN FIELD FOLLOWING A PARTIAL LOSS OF ENGINE POWER DURING INITIAL CLIMB FROM LEHIGH VALLEY INTERNATIONAL AIRPORT (ABE), ALLENTOWN, PENNSYLVANIA. THE CERTIFIED FLIGHT INSTRUCTOR (CFI) AND PRIVATE PILOT WERE NOT INJURED. THE INSTRUCTIONAL FLIGHT WAS CONDUCTED UNDER THE PROVISIONS OF 14 CODE OF FEDERAL REGULATIONS PART 91. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AND NO FLIGHT PLAN WAS FILED FOR THE PLANNED LOCAL FLIGHT. THE CFI STATED THAT THE AIRPLANE WAS FUELED TO 36 GALLONS PRIOR TO THE FLIGHT. THE ENGINE START-UP, TAXI, AND RUN-UP WERE NORMAL. WHILE DEPARTING FROM RUNWAY 31, ABOUT 200 FEET ABOVE GROUND LEVEL, THE CFI NOTICED THAT THE THROTTLE LEVER DID NOT APPEAR TO BE COMPLETELY FORWARD. HE AND THE PRIVATE PILOT PUSHED THE THROTTLE LEVER FULL FORWARD WITH RESISTANCE, WHICH WAS FOLLOWED BY ENGINE SPUTTERING. THE CFI THEN APPLIED CARBURETOR HEAT; HOWEVER, THE ENGINE CONTINUED TO SPUTTER. HE THEN ELECTED TO LAND IN A CORN FIELD. DURING THE LANDING, THE ENGINE FIREWALL AND RIGHT AILERON WERE DAMAGED. UPON EXAMINATION AND TESTING, WHICH INCLUDED ENGINE RUNS AND DISASSEMBLY OF COMPONENTS ATTACHED TO THE ENGINE IT WAS DISCOVERED THAT BOTH MAGNETOES WERE DEFECTIVE. ONE HAD A LOOSE GEAR AND THE OTHER WAS MISSING APPROXIMATELY 1/3 OF THE TEETH ON A GEAR. BOTH MAGNETOES HAD BEEN ON THE ENGINE SINCE OVERHAULED BY THE MANUFACTURER AND HAD ACHIEVED 2,228 HOURS IN SERVICE WITH NO MAINTENANCE RECORD ENTRIES SHOWING ANY WORK BEING PERFORMED ON THEM.

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 N15037 · 1

Matched to the same aircraft by N-number and date.