What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
During the second leg of the day, in cruise at FL250, pilot heard a loud bang and the aircraft made an abrupt nose down pitching moment. The pilot was able to gain control after approximately 3,500 feet of altitude loss. He experienced stiff controlls, with the column further aft than normal. During the descent he slowed the aircraft at FL180 to ensure aircraft controllability for landing with flaps partially extended. He made a flatter than normal, partial flap emergency landing at kbff. Upon exiting the aircraft, he noticed the starboard side, lower half cowling had been torn off the power plant and impacted the starboard side horizontal stabilizer, causing damage to approximately 2 feet of the outer portion which was bent up at about 45 degrees, causing elevator damage, and horizontal stabilizer structural damage.
No injuries
As the FAA filed it
DURING THE SECOND LEG OF THE DAY, IN CRUISE AT FL250, PILOT HEARD A LOUD BANG AND THE AIRCRAFT MADE AN ABRUPT NOSE DOWN PITCHING MOMENT. THE PILOT WAS ABLE TO GAIN CONTROL AFTER APPROXIMATELY 3,500 FEET OF ALTITUDE LOSS. HE EXPERIENCED STIFF CONTROLLS, WITH THE COLUMN FURTHER AFT THAN NORMAL. DURING THE DESCENT HE SLOWED THE AIRCRAFT AT FL180 TO ENSURE AIRCRAFT CONTROLLABILITY FOR LANDING WITH FLAPS PARTIALLY EXTENDED. HE MADE A FLATTER THAN NORMAL, PARTIAL FLAP EMERGENCY LANDING AT KBFF. UPON EXITING THE AIRCRAFT, HE NOTICED THE STARBOARD SIDE, LOWER HALF COWLING HAD BEEN TORN OFF THE POWER PLANT AND IMPACTED THE STARBOARD SIDE HORIZONTAL STABILIZER, CAUSING DAMAGE TO APPROXIMATELY 2 FEET OF THE OUTER PORTION WHICH WAS BENT UP AT ABOUT 45 DEGREES, CAUSING ELEVATOR DAMAGE, AND HORIZONTAL STABILIZER STRUCTURAL DAMAGE.
NO INJURIES