What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) Pilots stated that shortly after beginning a maneuver (practicing a steep spiral) over a selected site, they noticed that the prop RPM had gone from the selected 2400 RPM to 2700 RPM. When they could not control the propeller they headed for the Enterprise airport. They immediately checked oil pressure and saw no indication of any oil pressure. They then started looking for an off field landing site and made an advisory call for emergency landing. Within seconds, the engine seized and by that time the windshield was covered with oil making it difficult to see straight ahead. They identified an open grass field and ron reynolds took control of the airplane. The gear was lowered and the flaps put to full down. Upon touch down, the airplane kept straight on roll out until the last moment when it spun 120 degrees to the right. The airplane sustained substantial damage to left and right wings, landing gear, fuselage, and propeller. There were no injuries. A preliminary inspection indicated an excessive oil leak around the front area of the engine.
As the FAA filed it
(-23) PILOTS STATED THAT SHORTLY AFTER BEGINNING A MANEUVER (PRACTICING A STEEP SPIRAL) OVER A SELECTED SITE, THEY NOTICED THAT THE PROP RPM HAD GONE FROM THE SELECTED 2400 RPM TO 2700 RPM. WHEN THEY COULD NOT CONTROL THE PROPELLER THEY HEADED FOR THE ENTERPRISE AIRPORT. THEY IMMEDIATELY CHECKED OIL PRESSURE AND SAW NO INDICATION OF ANY OIL PRESSURE. THEY THEN STARTED LOOKING FOR AN OFF FIELD LANDING SITE AND MADE AN ADVISORY CALL FOR EMERGENCY LANDING. WITHIN SECONDS, THE ENGINE SEIZED AND BY THAT TIME THE WINDSHIELD WAS COVERED WITH OIL MAKING IT DIFFICULT TO SEE STRAIGHT AHEAD. THEY IDENTIFIED AN OPEN GRASS FIELD AND RON REYNOLDS TOOK CONTROL OF THE AIRPLANE. THE GEAR WAS LOWERED AND THE FLAPS PUT TO FULL DOWN. UPON TOUCH DOWN, THE AIRPLANE KEPT STRAIGHT ON ROLL OUT UNTIL THE LAST MOMENT WHEN IT SPUN 120 DEGREES TO THE RIGHT. THE AIRPLANE SUSTAINED SUBSTANTIAL DAMAGE TO LEFT AND RIGHT WINGS, LANDING GEAR, FUSELAGE, AND PROPELLER. THERE WERE NO INJURIES. A PRELIMINARY INSPECTION INDICATED AN EXCESSIVE OIL LEAK AROUND THE FRONT AREA OF THE ENGINE.
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 N7635J · 2
Matched to the same aircraft by N-number and date.