19930519014459A

Accident · Substantial damage

FAA accident report · Piper PA-25-235 · Mexico, MO · May 19, 1993

Date
May 19, 1993 · 15:20 local
Place
Mexico, MO
Damage
Substantial damage
Aircraft
N8787L
NTSB investigation
NTSBCHI93LA175
Reported as
Piper PA25235
Fatal 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.

(-4)The pilot reported a partial loss of engine power during a spray run. He briefly applied carburetor heat, pumped the throttle and leaned the mixture, but was unable to restore sufficient power to maintain altitude. He landed the airplane in a soft, fallow field and nosed over. The engine was removed from the airframe. During the removal and subsequent preparation of the engine for a test run in a different airframe, some water was noted in the fuel gascolator, oil was seen in the left magneto, a broken high tension lead was replaced, and a different carburetor air box was fitted. The engine started and ran normally, except for a slight roughness at full rated power.

As the FAA filed it

(-4)THE PILOT REPORTED A PARTIAL LOSS OF ENGINE POWER DURING A SPRAY RUN. HE BRIEFLY APPLIED CARBURETOR HEAT, PUMPED THE THROTTLE AND LEANED THE MIXTURE, BUT WAS UNABLE TO RESTORE SUFFICIENT POWER TO MAINTAIN ALTITUDE. HE LANDED THE AIRPLANE IN A SOFT, FALLOW FIELD AND NOSED OVER. THE ENGINE WAS REMOVED FROM THE AIRFRAME. DURING THE REMOVAL AND SUBSEQUENT PREPARATION OF THE ENGINE FOR A TEST RUN IN A DIFFERENT AIRFRAME, SOME WATER WAS NOTED IN THE FUEL GASCOLATOR, OIL WAS SEEN IN THE LEFT MAGNETO, A BROKEN HIGH TENSION LEAD WAS REPLACED, AND A DIFFERENT CARBURETOR AIR BOX WAS FITTED. THE ENGINE STARTED AND RAN NORMALLY, EXCEPT FOR A SLIGHT ROUGHNESS AT FULL RATED POWER.

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 N8787L · 3

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