What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(.19) On March 31, 2001, about 1133 hours PST, a Stinson 108-1, N8158K, owned and operated by the pilot, experienced a total loss of engine power. The pilot made a forced landing about 3 miles northeast of the banning, CA., airport and collided with a berm. The airplane was substantially damaged, and the private pilot was seriously injured. The personal flight was performed under 14 CFR part 91. Visual meteorological conditions prevailed, and no flight plan was filed. The flight originated from banning about 1120. The pilot reported to the NTSB investigator that he had purchased the airplane a few weeks prior to the accident flight. He also stated that no vibration was felt prior to the loss of engine power. In an attempt at restoring power, he applied the carburetor heat, changed the mixture setting and repositioned the ignition key, but no engine power was restored. Thereafter, the pilot made a forced landing on the underlying rough terrain. A sheriff's deputy who responded to the accident site stated to the safety board investigator that upon arrival at the crash site he observed fuel streaming from the wing tanks of the impact-damaged airplane. (-23)on March 31, 2001, at 1115, privacy data omitted departed banning airport banning CA. Destination Redlands airport, Redlands CA. privacy data omitted Over flew the Redlands airport heading north about 5 miles turnes to enter the 45 degree entry to runway 26, and started descending from 4000 feet to 2400 feet. Also at this time privacy data omitted throttled back, and pulled carburetor heat and the engine quit. privacy data omitted Picked out a dirt road that was part of a home building site to land. Whiel he was descending he tried several times to restart the engine with no success. privacy data omitted Landed, and on roll he hit a dirt building site pad which caused the aircraft to flip over. privacy data omitted Sustained severe injuries, as a result of the accident. (.4) on March 31, 2001, about 1133 hours pacific standard time, a Stinson 108-1, N8158K, experienced a total loss of engine power during cruise flight. The pilot made a forced landing about 1.5 miles north-northeast of the Redlands Municipal Airport, Redlands, California. During the landing rollout, the airplane collided with a dirt berm. The airplane was substantially dam aged, and the private pilot was seriously injured. The personal flight was performed under 14 CFR part 91. Visual meteorological conditions prevailed, and no flight plan was filed. The flight originated from banning about 1120. The pilot reported to the national transportation safety board investigator that he had purchased the airplane a few weeks prior to the accident flight, and he was familiar with its operation. Prior to taking off on the accident flight, both of the wing fuel tanks had been filled. The pilot also stated that no vibration was felt prior to the loss of engine power. In an attempt at restoring power, he applied the carburetor heat, changed the mixture setting, and repositioned the ignition key. However, none of his actions were successful in restoring power to his airplane's engine. Thereafter, he made a forced landing on the underlying rough terrain. A deputy sheriff responded to the accident site. The sheriff reported to the safety board investigator that upon arrival he observed fuel streaming from the wing tanks of the impact-damaged airplane. The airplane was manufactured in 1946. The airplane was subsequently recovered, inspected, and partially repaired bya federal aviation administration certificated airframe and powerplant mechanic. The mechanic who performed the work verbally reported to the safety board investigator that the engine was completely torn down. No evidence of any preimpact malfunction was noted. The accessories were also examined, and no evidence of malfunction was noted. Both the carburetor finger screen and the gascolator fuel screen were observed clear. The magnetos were functional. The carburetor heat control worked. One of the propeller blades was noted bent in an aft direction indicating the crankshaft was not rotating during the impact sequence. The mechanic indicated that he could not ascertain the reason for the non-mechanical total loss of engine power.
As the FAA filed it
(.19) ON MARCH 31, 2001, ABOUT 1133 HOURS PST, A STINSON 108-1, N8158K, OWNED AND OPERATED BY THE PILOT, EXPERIENCED A TOTAL LOSS OF ENGINE POWER. THE PILOT MADE A FORCED LANDING ABOUT 3 MILES NORTHEAST OF THE BANNING, CA., AIRPORT AND COLLIDED WITH A BERM. THE AIRPLANE WAS SUBSTANTIALLY DAMAGED, AND THE PRIVATE PILOT WAS SERIOUSLY INJURED. THE PERSONAL FLIGHT WAS PERFORMED UNDER 14 CFR PART 91. VISUAL METEOROLOGICAL CONDITIONS PREVAILED, AND NO FLIGHT PLAN WAS FILED. THE FLIGHT ORIGINATED FROM BANNING ABOUT 1120. THE PILOT REPORTED TO THE NTSB INVESTIGATOR THAT HE HAD PURCHASED THE AIRPLANE A FEW WEEKS PRIOR TO THE ACCIDENT FLIGHT. HE ALSO STATED THAT NO VIBRATION WAS FELT PRIOR TO THE LOSS OF ENGINE POWER. IN AN ATTEMPT AT RESTORING POWER, HE APPLIED THE CARBURETOR HEAT, CHANGED THE MIXTURE SETTING AND REPOSITIONED THE IGNITION KEY, BUT NO ENGINE POWER WAS RESTORED. THEREAFTER, THE PILOT MADE A FORCED LANDING ON THE UNDERLYING ROUGH TERRAIN. A SHERIFF'S DEPUTY WHO RESPONDED TO THE ACCIDENT SITE STATED TO THE SAFETY BOARD INVESTIGATOR THAT UPON ARRIVAL AT THE CRASH SITE HE OBSERVED FUEL STREAMING FROM THE WING TANKS OF THE IMPACT-DAMAGED AIRPLANE. (-23)ON MARCH 31, 2001, AT 1115, ^PRIVACY DATA OMITTED^ DEPARTED BANNING AIRPORT BANNING CA. DESTINATION REDLANDS AIRPORT, REDLANDS CA. ^PRIVACY DATA O^ OVER FLEW THE REDLANDS AIRPORT HEADING NORTH ABOUT 5 MILES TURNES TO ENTER THE 45 DEGREE ENTRY TO RUNWAY 26, AND STARTED DESCENDING FROM 4000 FEET TO 2400 FEET. ALSO AT THIS TIME ^PRIVACY DATA O^ THROTTLED BACK, AND PULLED CARBURETOR HEAT AND THE ENGINE QUIT. ^PRIVACY DATA O^ PICKED OUT A DIRT ROAD THAT WAS PART OF A HOME BUILDING SITE TO LAND. WHIEL HE WAS DESCENDING HE TRIED SEVERAL TIMES TO RESTART THE ENGINE WITH NO SUCCESS. ^PRIVACY DATA O^ LANDED, AND ON ROLL HE HIT A DIRT BUILDING SITE PAD WHICH CAUSED THE AIRCRAFT TO FLIP OVER. ^PRIVACY DATA O^ SUSTAINED SEVERE INJURIES, AS A RESULT OF THE ACCIDENT. (.4) ON MARCH 31, 2001, ABOUT 1133 HOURS PACIFIC STANDARD TIME, A STINSON 108-1, N8158K, EXPERIENCED A TOTAL LOSS OF ENGINE POWER DURING CRUISE FLIGHT. THE PILOT MADE A FORCED LANDING ABOUT 1.5 MILES NORTH-NORTHEAST OF THE REDLANDS MUNICIPAL AIRPORT, REDLANDS, CALIFORNIA. DURING THE LANDING ROLLOUT, THE AIRPLANE COLLIDED WITH A DIRT BERM. THE AIRPLANE WAS SUBSTANTIALLY DAM AGED, AND THE PRIVATE PILOT WAS SERIOUSLY INJURED. THE PERSONAL FLIGHT WAS PERFORMED UNDER 14 CFR PART 91. VISUAL METEOROLOGICAL CONDITIONS PREVAILED, AND NO FLIGHT PLAN WAS FILED. THE FLIGHT ORIGINATED FROM BANNING ABOUT 1120. THE PILOT REPORTED TO THE NATIONAL TRANSPORTATION SAFETY BOARD INVESTIGATOR THAT HE HAD PURCHASED THE AIRPLANE A FEW WEEKS PRIOR TO THE ACCIDENT FLIGHT, AND HE WAS FAMILIAR WITH ITS OPERATION. PRIOR TO TAKING OFF ON THE ACCIDENT FLIGHT, BOTH OF THE WING FUEL TANKS HAD BEEN FILLED. THE PILOT ALSO STATED THAT NO VIBRATION WAS FELT PRIOR TO THE LOSS OF ENGINE POWER. IN AN ATTEMPT AT RESTORING POWER, HE APPLIED THE CARBURETOR HEAT, CHANGED THE MIXTURE SETTING, AND REPOSITIONED THE IGNITION KEY. HOWEVER, NONE OF HIS ACTIONS WERE SUCCESSFUL IN RESTORING POWER TO HIS AIRPLANE'S ENGINE. THEREAFTER, HE MADE A FORCED LANDING ON THE UNDERLYING ROUGH TERRAIN. A DEPUTY SHERIFF RESPONDED TO THE ACCIDENT SITE. THE SHERIFF REPORTED TO THE SAFETY BOARD INVESTIGATOR THAT UPON ARRIVAL HE OBSERVED FUEL STREAMING FROM THE WING TANKS OF THE IMPACT-DAMAGED AIRPLANE. THE AIRPLANE WAS MANUFACTURED IN 1946. THE AIRPLANE WAS SUBSEQUENTLY RECOVERED, INSPECTED, AND PARTIALLY REPAIRED BYA FEDERAL AVIATION ADMINISTRATION CERTIFICATED AIRFRAME AND POWERPLANT MECHANIC. THE MECHANIC WHO PERFORMED THE WORK VERBALLY REPORTED TO THE SAFETY BOARD INVESTIGATOR THAT THE ENGINE WAS COMPLETELY TORN DOWN. NO EVIDENCE OF ANY PREIMPACT MALFUNCTION WAS NOTED. THE ACCESSORIES WERE ALSO EXAMINED, AND NO EVIDENCE OF MALFUNCTION WAS NOTED. BOTH THE CARBURETOR FINGER SCREEN AND THE GASCOLATOR FUEL SCREEN WERE OBSERVED CLEAR. THE MAGNETOS WERE FUNCTIONAL. THE CARBURETOR HEAT CONTROL WORKED. ONE OF THE PROPELLER BLADES WAS NOTED BENT IN AN AFT DIRECTION INDICATING THE CRANKSHAFT WAS NOT ROTATING DURING THE IMPACT SEQUENCE. THE MECHANIC INDICATED THAT HE COULD NOT ASCERTAIN THE REASON FOR THE NON-MECHANICAL TOTAL LOSS OF ENGINE 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.