20161007019939I

Incident · Minor damage

FAA incident report · Piper PA-28-151 · Lebanon, TN · October 7, 2016

Date
October 7, 2016 · 12:00 local
Place
Lebanon, TN
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N33575
Reported as
Piper PA-28-151
Reported engine
Lycoming 0-320 series
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Private pilot
Pilot’s flight hours
103 total65 in this make and model49 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.

The pilot claimed to have completed a satisfactory runup prior to departing Lebanon municipal airport (M54). He stated that once his aircraft reached approximately 1,200 feet MSL during the climbout, the engine began to sputter. He conducted the emergency checklist for his situation, verifying that the fuel primer, power setting, fuel mixture setting, and magnetos were all okay. He determined that the engine was not producing enough power to continue climbing so he committed to landing in a field just slightly to the west of his climbout heading and less than 1 NM from the end of the runway he had just departed from. He successfully landed without causing injury to himself, the sole occupant of the aircraft, and with only very minor damage to the aircraft. The FAA inspectors who investigated this incident found that the air inlet hose that connects the air filter to the carburetor heat box had collapsed, restricting airflow to the engine, and causing the power loss the pilot had previously experienced. All appropriate aircraft inspections had been performed on the aircraft and properly documented prior to the incident. The pilot was properly certificated and current at the time of the incident.

As the FAA filed it

THE PILOT CLAIMED TO HAVE COMPLETED A SATISFACTORY RUNUP PRIOR TO DEPARTING LEBANON MUNICIPAL AIRPORT (M54). HE STATED THAT ONCE HIS AIRCRAFT REACHED APPROXIMATELY 1,200 FEET MSL DURING THE CLIMBOUT, THE ENGINE BEGAN TO SPUTTER. HE CONDUCTED THE EMERGENCY CHECKLIST FOR HIS SITUATION, VERIFYING THAT THE FUEL PRIMER, POWER SETTING, FUEL MIXTURE SETTING, AND MAGNETOS WERE ALL OKAY. HE DETERMINED THAT THE ENGINE WAS NOT PRODUCING ENOUGH POWER TO CONTINUE CLIMBING SO HE COMMITTED TO LANDING IN A FIELD JUST SLIGHTLY TO THE WEST OF HIS CLIMBOUT HEADING AND LESS THAN 1 NM FROM THE END OF THE RUNWAY HE HAD JUST DEPARTED FROM. HE SUCCESSFULLY LANDED WITHOUT CAUSING INJURY TO HIMSELF, THE SOLE OCCUPANT OF THE AIRCRAFT, AND WITH ONLY VERY MINOR DAMAGE TO THE AIRCRAFT. THE FAA INSPECTORS WHO INVESTIGATED THIS INCIDENT FOUND THAT THE AIR INLET HOSE THAT CONNECTS THE AIR FILTER TO THE CARBURETOR HEAT BOX HAD COLLAPSED, RESTRICTING AIRFLOW TO THE ENGINE, AND CAUSING THE POWER LOSS THE PILOT HAD PREVIOUSLY EXPERIENCED. ALL APPROPRIATE AIRCRAFT INSPECTIONS HAD BEEN PERFORMED ON THE AIRCRAFT AND PROPERLY DOCUMENTED PRIOR TO THE INCIDENT. THE PILOT WAS PROPERLY CERTIFICATED AND CURRENT AT THE TIME OF THE INCIDENT.