ANACORTES, WA, USA
N1755U
CESSNA 207
THE PLT STATED HE ADDED 10 DEGREES OF FLAPS ON DOWNWIND AND APPLIED FULL FLAPS ON FINAL. A RAPID RATE OF DESCENT WAS EXPERIENCED 200 YARDS FROM TOUCHDOWN. THE PILOT SAID HE ADDED POWER TO ARREST THE SINK RATE. THE ACFT COLLIDED WITH TREES ON FINAL. THE PILOT STATED THAT AFTER THE ACCIDENT, THE FLAPS WERE EXTENDED 10 DEGREES, THE FLAP ACTUATOR HANDLE WAS IN THE FULL DOWN POSITION AND THE FLAP CIRCUIT BREAKER WAS OUT. A MECHANIC WHO INSPECTED THE ACFT AFTER THE ACCIDENT REPORTED NO MECHANICAL ABNORMALITIES WERE FOUND.
Source: NTSB Aviation Accident Database
Aviation Accidents App
In-Depth Access to Aviation Accident Reports
