What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
Narrative: history of flight: on November 29,1995, at 1340 CDT, a Beechcraft, BE-33-F33A, N15JV, registered to valley motors, inc., impacted a telegraph wire during a forced landing after engine power failure, on final approach to destination, during a 14CFR 91 pleasure flight. Visual meteorological conditions prevailed at the time. Minor damage was sustained by the aircraft & the certificated commercial pilot & one passenger sustained no injuries, the flight originated at college station , TX November 29, 1995 at 1115 CDT. Damage to aircraft: there was minor damage to one propeller blade, upper engine cowl, left wing inboard leading edge, left flap, left land gear, upper cabin section, & leading edge vertical stabilizer fairing. Test and research: investigation revealed the boost pump drain in intake duct was obstructed, engine idle mixture was richer than manufacturer's specifications, & fuel pump pressure was higher at idle RPM than specified. Note: aircraft was not within power off glide distance from runway of final approach, forced landing touch down accomplished 1/2 mile from runway approach end. privacy data omitted This incident is closed.
As the FAA filed it
NARRATIVE: HISTORY OF FLIGHT: ON NOVEMBER 29,1995, AT 1340 CDT, A BEECHCRAFT, BE-33-F33A, N15JV, REGISTERED TO VALLEY MOTORS, INC., IMPACTED A TELEGRAPH WIRE DURING A FORCED LANDING AFTER ENGINE POWER FAILURE, ON FINAL APPROACH TO DESTINATION, DURING A 14CFR 91 PLEASURE FLIGHT. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AT THE TIME. MINOR DAMAGE WAS SUSTAINED BY THE AIRCRAFT & THE CERTIFICATED COMMERCIAL PILOT & ONE PASSENGER SUSTAINED NO INJURIES, THE FLIGHT ORIGINATED AT COLLEGE STATION , TX NOVEMBER 29, 1995 AT 1115 CDT. DAMAGE TO AIRCRAFT: THERE WAS MINOR DAMAGE TO ONE PROPELLER BLADE, UPPER ENGINE COWL, LEFT WING INBOARD LEADING EDGE, LEFT FLAP, LEFT LAND GEAR, UPPER CABIN SECTION, & LEADING EDGE VERTICAL STABILIZER FAIRING. TEST AND RESEARCH: INVESTIGATION REVEALED THE BOOST PUMP DRAIN IN INTAKE DUCT WAS OBSTRUCTED, ENGINE IDLE MIXTURE WAS RICHER THAN MANUFACTURER'S SPECIFICATIONS, & FUEL PUMP PRESSURE WAS HIGHER AT IDLE RPM THAN SPECIFIED. NOTE: AIRCRAFT WAS NOT WITHIN POWER OFF GLIDE DISTANCE FROM RUNWAY OF FINAL APPROACH, FORCED LANDING TOUCH DOWN ACCOMPLISHED 1/2 MILE FROM RUNWAY APPROACH END. ^PRIVACY DATA OMITTED^ THIS INCIDENT IS CLOSED.