What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
On 04/22/2012 at approximately 16:30 CDT an experimental, amateur- built aircraft, N80BH, make: Bumford-Royer, model: Christen Eagle II,crashed, after take-off from Pearland reginal airport (klvj), friendswood Texas. The aircraft turned to an approximate heading of 233 degrees, , hitting trees and the bank of a drainage ditch, coming to rest at the bottom of the ditch about 1/4 mile from the runway. The aircraft was properly registered and certificated for the local, CFR part 91 flight and sustained substantail damage. The pilot was properly rated for the personal flight and was seriously injured.a witness said the aircraft was taking off and had climed to about 300 to 400 feet when the witness heard a loss of engine power. Inspection of the aircraft at the accident site disclosed damage to the propeller, engine mount, firewall, both upper and lower wings and spars, right aileron, fuselage, main gear and main fuel tank. The oil filter adapter and propeller control were broken from the rear of the engine
As the FAA filed it
ON 04/22/2012 AT APPROXIMATELY 16:30 CDT AN EXPERIMENTAL, AMATEUR- BUILT AIRCRAFT, N80BH, MAKE: BUMFORD-ROYER, MODEL: CHRISTEN EAGLE II,CRASHED, AFTER TAKE-OFF FROM PEARLAND REGINAL AIRPORT (KLVJ), FRIENDSWOOD TEXAS.THE AIRCRAFT TURNED TO AN APPROXIMATE HEADING OF 233 DEGREES, , HITTING TREES AND THE BANK OF A DRAINAGE DITCH, COMING TO REST AT THE BOTTOM OF THE DITCH ABOUT 1/4 MILE FROM THE RUNWAY.THE AIRCRAFT WAS PROPERLY REGISTERED AND CERTIFICATED FOR THE LOCAL, CFR PART 91 FLIGHT AND SUSTAINED SUBSTANTAIL DAMAGE.THE PILOT WAS PROPERLY RATED FOR THE PERSONAL FLIGHT AND WAS SERIOUSLY INJURED.A WITNESS SAID THE AIRCRAFT WAS TAKING OFF AND HAD CLIMED TO ABOUT 300 TO 400 FEET WHEN THE WITNESS HEARD A LOSS OF ENGINE POWER.INSPECTION OF THE AIRCRAFT AT THE ACCIDENT SITE DISCLOSED DAMAGE TO THE PROPELLER, ENGINE MOUNT, FIREWALL, BOTH UPPER AND LOWER WINGS AND SPARS, RIGHT AILERON, FUSELAGE, MAIN GEAR AND MAIN FUEL TANK. THE OIL FILTER ADAPTER AND PROPELLER CONTROL WERE BROKEN FROM THE REAR 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 N80BH · 1
Matched to the same aircraft by N-number and date.