Incident Overview
During the takeoff roll, the pilot reported that the airspeed indicator did not exceed 65 knots. He subsequently aborted the takeoff, but the airplane continued off the end of the runway and came to rest in a parking lot.
System Examination
An airspeed calibration test was conducted, which revealed that the airspeed indicator read approximately 10 knots higher than the test equipment. Further inspection of the pitot-static system found that the pitot tube was obstructed with a "corrosion-type material."
Airspeed Indicator Bench Test
The airspeed indicator was removed from the airplane and bench tested. The bench test showed that the indicator read approximately 4–5 knots higher than the test equipment.
Previous System Check
The most recent pitot-static system check had been performed on March 14, 2001.