What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
At approximately 10:50 CT aircraft departed pearland regional airport (lvj) enroute to Galveston Scholes airport (gls), 28 miles away. At approximately 17 miles away from gls, the pilot stated that he smelled smoke in the cabin and realized his engine oil pressure gauge read zero. Shortly after reporting to the gls tower his position at 5NM, the engine stopped. Pilot retracted the landing gear and flaps to increase glide speed. Pilot managed to make it to the runway. After clearing the airport perimeter fence, he extended his landing gear, but the gear didn’t have time to fully extend and the aircraft landed on runway 18 at 1103 CT with the right landing gear partially down. The left and nose were fully extended. There were no injuries and there was minor damage to the aircraft. Post accident examination of the engine revealed the engine oil filter adapter was not safety wired and was loose. The engine oil system was depleted. Engine wall above cylinder #2 just below the magneto was breeched during engine seizure.
As the FAA filed it
AT APPROXIMATELY 10:50 CT AIRCRAFT DEPARTED PEARLAND REGIONAL AIRPORT (LVJ) ENROUTE TO GALVESTON SCHOLES AIRPORT (GLS), 28 MILES AWAY. AT APPROXIMATELY 17 MILES AWAY FROM GLS, THE PILOT STATED THAT HE SMELLED SMOKE IN THE CABIN AND REALIZED HIS ENGINE OIL PRESSURE GAUGE READ ZERO. SHORTLY AFTER REPORTING TO THE GLS TOWER HIS POSITION AT 5NM, THE ENGINE STOPPED. PILOT RETRACTED THE LANDING GEAR AND FLAPS TO INCREASE GLIDE SPEED. PILOT MANAGED TO MAKE IT TO THE RUNWAY. AFTER CLEARING THE AIRPORT PERIMETER FENCE, HE EXTENDED HIS LANDING GEAR, BUT THE GEAR DIDN’T HAVE TIME TO FULLY EXTEND AND THE AIRCRAFT LANDED ON RUNWAY 18 AT 1103 CT WITH THE RIGHT LANDING GEAR PARTIALLY DOWN. THE LEFT AND NOSE WERE FULLY EXTENDED. THERE WERE NO INJURIES AND THERE WAS MINOR DAMAGE TO THE AIRCRAFT. POST ACCIDENT EXAMINATION OF THE ENGINE REVEALED THE ENGINE OIL FILTER ADAPTER WAS NOT SAFETY WIRED AND WAS LOOSE. THE ENGINE OIL SYSTEM WAS DEPLETED. ENGINE WALL ABOVE CYLINDER #2 JUST BELOW THE MAGNETO WAS BREECHED DURING ENGINE SEIZURE.
NTSB investigation
The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.