What happened
The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.
(-23) Medical certificate third class, 11/04/02. At 1720 Mr. Kern took off in N2279K from the Woodland, Washington airport. Mr. Kern reported that the aircraft engine was operating normally through out the take-off maneuver, then engine made power. Approximately 1200 feet down runway 12, the aircraft rotated, got into the air then settled down on the runway again. Mr. Kern then pulled back and rotated again, the aircraft was about 10 feet airborne, then the left wing dropped and the aircraft hit the ground 90 feet to the east of the runway. Mr. Kern informed inspector clark that he was attempting a short field take-off. The passenger and eyewitnesses said the engine sounded normal through out the take-off procedure. FAA inspector john r. clark investigated the accident and found the engine had adequate fuel and that there were no engine irregularites. The left wing spar was bent 5 five inboard of the left wingtip, the outboard 2 feet of the right wing tip was damage including the spar, the fuselage aft of the cabin was severely wrinkled, and the firewall was bent. All three landing gear legs were bent and damaged. The propeller had shown evidence that the engine was at full power.
As the FAA filed it
(-23) MEDICAL CERTIFICATE THIRD CLASS, 11/04/02. AT 1720 MR. KERN TOOK OFF IN N2279K FROM THE WOODLAND, WASHINGTON AIRPORT. MR. KERN REPORTED THAT THE AIRCRAFT ENGINE WAS OPERATING NORMALLY THROUGH OUT THE TAKE-OFF MANEUVER, THEN ENGINE MADE POWER. APPROXIMATELY 1200 FEET DOWN RUNWAY 12, THE AIRCRAFT ROTATED, GOT INTO THE AIR THEN SETTLED DOWN ON THE RUNWAY AGAIN. MR. KERN THEN PULLED BACK AND ROTATED AGAIN, THE AIRCRAFT WAS ABOUT 10 FEET AIRBORNE, THEN THE LEFT WING DROPPED AND THE AIRCRAFT HIT THE GROUND 90 FEET TO THE EAST OF THE RUNWAY. MR. KERN INFORMED INSPECTOR CLARK THAT HE WAS ATTEMPTING A SHORT FIELD TAKE-OFF. THE PASSENGER AND EYEWITNESSES SAID THE ENGINE SOUNDED NORMAL THROUGH OUT THE TAKE-OFF PROCEDURE. FAA INSPECTOR JOHN R. CLARK INVESTIGATED THE ACCIDENT AND FOUND THE ENGINE HAD ADEQUATE FUEL AND THAT THERE WERE NO ENGINE IRREGULARITES. THE LEFT WING SPAR WAS BENT 5 FIVE INBOARD OF THE LEFT WINGTIP, THE OUTBOARD 2 FEET OF THE RIGHT WING TIP WAS DAMAGE INCLUDING THE SPAR, THE FUSELAGE AFT OF THE CABIN WAS SEVERELY WRINKLED, AND THE FIREWALL WAS BENT. ALL THREE LANDING GEAR LEGS WERE BENT AND DAMAGED. THE PROPELLER HAD SHOWN EVIDENCE THAT THE ENGINE WAS AT FULL 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.
Other reports on N2279Y · 1
Matched to the same aircraft by N-number and date.