What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) On July 21, 2008 at approximately 1438 CDT, N57601, a 1975 Piper pawnee brave, PA-36-285-300, operated by betrand spraying LLC (J3GG) made an emergency landing in a field approximately 3/4 of a statute mile southeast of the dirt runway belonging to bertrand spraying LLC. There were no injuries. The sole occupant and pilot privacy data omitted, commercial airman privacy data omitted, stated he lost power shortly after takeoff and made an emergency landing in the field and the aircraft hit very hard. The pilot stated the manifold pressure was between 23-24 hg when it is normally 26 hg. He adamantly maintains he had full throttle during the takeoff. The aircraft was substantially damaged as the right main landing gear separated from the fuselage and the left main gear collapsed. The engine was positioned downward at a nearly 90 degree angle due to impact with the ground. The pilot stated approximately one week prior to the accident, the engine ran rugh and the spark plugs were removed to clean excessive carbon. The plugs were reinstalled and the engine performed normally.
As the FAA filed it
(-23) ON JULY 21, 2008 AT APPROXIMATELY 1438 CDT, N57601, A 1975 PIPER PAWNEE BRAVE, PA-36-285-300, OPERATED BY BETRAND SPRAYING LLC (J3GG) MADE AN EMERGENCY LANDING IN A FIELD APPROXIMATELY 3/4 OF A STATUTE MILE SOUTHEAST OF THE DIRT RUNWAY BELONGING TO BERTRAND SPRAYING LLC. THERE WERE NO INJURIES. THE SOLE OCCUPANT AND PILOT ^PRIVACY DATA OMITTED^, COMMERCIAL AIRMAN ^PRIVACY DATA OMITTED^, STATED HE LOST POWER SHORTLY AFTER TAKEOFF AND MADE AN EMERGENCY LANDING IN THE FIELD AND THE AIRCRAFT HIT VERY HARD. THE PILOT STATED THE MANIFOLD PRESSURE WAS BETWEEN 23-24 HG WHEN IT IS NORMALLY 26 HG. HE ADAMANTLY MAINTAINS HE HAD FULL THROTTLE DURING THE TAKEOFF. THE AIRCRAFT WAS SUBSTANTIALLY DAMAGED AS THE RIGHT MAIN LANDING GEAR SEPARATED FROM THE FUSELAGE AND THE LEFT MAIN GEAR COLLAPSED. THE ENGINE WAS POSITIONED DOWNWARD AT A NEARLY 90 DEGREE ANGLE DUE TO IMPACT WITH THE GROUND. THE PILOT STATED APPROXIMATELY ONE WEEK PRIOR TO THE ACCIDENT, THE ENGINE RAN RUGH AND THE SPARK PLUGS WERE REMOVED TO CLEAN EXCESSIVE CARBON. THE PLUGS WERE REINSTALLED AND THE ENGINE PERFORMED NORMALLY.
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 N57601 · 1
Matched to the same aircraft by N-number and date.