What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) Pilot stated that on September 18, 2005 he received an aircraft checkout from the renting FBO. The aircraft checkout flight was 1.4 hours long and ground school 30 minutes. On September 19 at approximately 0900 am the pilot and 2 passengers departed the chandler airport (chd) chandler, Arizona. Pilot stated he was approximately 150 pounds under gross weight on takeoff. Aircraft landed at Bisbee airport (P04) with no problems. Before departing the pilot added 20 gallons of avgas to the aircraft. Pilot stated that the wind was sse at 3 knots and the temperature was 73 degrees fahrenheit and the aircraft was again 150 pounds under gross weight. At approximately 1530 PST on September 19, 2005 the pilot stated the takeoff roll (as per the pilot) the aircraft never accelerated past 65 knots; the aircraft ground roll encompassed the entire runway of 5900 feet. Aircraft ran off the end of the runway, then the pilot pulled power off and applied brakes. Damage consisted of both wing leading edged, propeller, landing gear and fuselage damage. Pilot made a statement that his instructor, during check out told him that the ground run on high density airports would be longer. No additional causal factors.
As the FAA filed it
(-23) PILOT STATED THAT ON SEPTEMBER 18, 2005 HE RECEIVED AN AIRCRAFT CHECKOUT FROM THE RENTING FBO. THE AIRCRAFT CHECKOUT FLIGHT WAS 1.4 HOURS LONG AND GROUND SCHOOL 30 MINUTES. ON SEPTEMBER 19 AT APPROXIMATELY 0900 AM THE PILOT AND 2 PASSENGERS DEPARTED THE CHANDLER AIRPORT (CHD) CHANDLER, ARIZONA. PILOT STATED HE WAS APPROXIMATELY 150 POUNDS UNDER GROSS WEIGHT ON TAKEOFF. AIRCRAFT LANDED AT BISBEE AIRPORT (P04) WITH NO PROBLEMS. BEFORE DEPARTING THE PILOT ADDED 20 GALLONS OF AVGAS TO THE AIRCRAFT. PILOT STATED THAT THE WIND WAS SSE AT 3 KNOTS AND THE TEMPERATURE WAS 73 DEGREES FAHRENHEIT AND THE AIRCRAFT WAS AGAIN 150 POUNDS UNDER GROSS WEIGHT. AT APPROXIMATELY 1530 PST ON SEPTEMBER 19, 2005 THE PILOT STATED THE TAKEOFF ROLL (AS PER THE PILOT) THE AIRCRAFT NEVER ACCELERATED PAST 65 KNOTS; THE AIRCRAFT GROUND ROLL ENCOMPASSED THE ENTIRE RUNWAY OF 5900 FEET. AIRCRAFT RAN OFF THE END OF THE RUNWAY, THEN THE PILOT PULLED POWER OFF AND APPLIED BRAKES. DAMAGE CONSISTED OF BOTH WING LEADING EDGED, PROPELLER, LANDING GEAR AND FUSELAGE DAMAGE. PILOT MADE A STATEMENT THAT HIS INSTRUCTOR, DURING CHECK OUT TOLD HIM THAT THE GROUND RUN ON HIGH DENSITY AIRPORTS WOULD BE LONGER. NO ADDITIONAL CAUSAL FACTORS.
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 N5757D · 1
Matched to the same aircraft by N-number and date.