Narrative:

The approach was in light rain that ended on short final. The runway was wet from a previous shower. I landed approximately 1500 ft down the runway. I tested the brakes, they were ok. I deployed thrust reversers, spoilers, and I increased the braking pressure. Nearing the last taxiway, the aircraft was decelerating normally until the aircraft rolled on the painted threshold markings at which time the deceleration rate of aircraft stopped. Later we could see from the tire tracks that there was very little rubber on the painted areas as compared with unpainted surface. Preventive measures: 1) mix sand with paint to increase the braking friction on painted surfaces. 2) use maximum thrust reversers for full effectiveness. 3) use maximum brakes for minimum stopping distance. 4) land on first 1000 ft of runway. Supplemental information from acn 399852: the PIC was unable to stop on the hard surface and continued off the runway a few ft and stopped. Several factors contributed to this occurrence. 1) the wet runway surface. 2) the weight of the aircraft (minimum required fuel and no passenger) reducing braking effectiveness. 3) the possibility of hydroplaning the tires. 4) wet painted surfaces on the runway (threshold markings and numbering for runway 17L) that further decreased braking effectiveness at the end of runway 35R. To correct this occurrence a more aggressive use of reverse thrust upon touchdown and decelerating more rapidly to low speed using reverse thrust, before reaching the runway end.

Google
 

Original NASA ASRS Text

Title: A C650 FLC EXPERIENCES A RWY EXCURSION WHEN THEY FAIL TO STOP ON A WET RWY AT LNK, NE. SCENARIO DEPICTS LATE DEPLOYMENT OF SPOILERS AND THRUST REVERSERS.

Narrative: THE APCH WAS IN LIGHT RAIN THAT ENDED ON SHORT FINAL. THE RWY WAS WET FROM A PREVIOUS SHOWER. I LANDED APPROX 1500 FT DOWN THE RWY. I TESTED THE BRAKES, THEY WERE OK. I DEPLOYED THRUST REVERSERS, SPOILERS, AND I INCREASED THE BRAKING PRESSURE. NEARING THE LAST TXWY, THE ACFT WAS DECELERATING NORMALLY UNTIL THE ACFT ROLLED ON THE PAINTED THRESHOLD MARKINGS AT WHICH TIME THE DECELERATION RATE OF ACFT STOPPED. LATER WE COULD SEE FROM THE TIRE TRACKS THAT THERE WAS VERY LITTLE RUBBER ON THE PAINTED AREAS AS COMPARED WITH UNPAINTED SURFACE. PREVENTIVE MEASURES: 1) MIX SAND WITH PAINT TO INCREASE THE BRAKING FRICTION ON PAINTED SURFACES. 2) USE MAX THRUST REVERSERS FOR FULL EFFECTIVENESS. 3) USE MAX BRAKES FOR MINIMUM STOPPING DISTANCE. 4) LAND ON FIRST 1000 FT OF RWY. SUPPLEMENTAL INFO FROM ACN 399852: THE PIC WAS UNABLE TO STOP ON THE HARD SURFACE AND CONTINUED OFF THE RWY A FEW FT AND STOPPED. SEVERAL FACTORS CONTRIBUTED TO THIS OCCURRENCE. 1) THE WET RWY SURFACE. 2) THE WT OF THE ACFT (MINIMUM REQUIRED FUEL AND NO PAX) REDUCING BRAKING EFFECTIVENESS. 3) THE POSSIBILITY OF HYDROPLANING THE TIRES. 4) WET PAINTED SURFACES ON THE RWY (THRESHOLD MARKINGS AND NUMBERING FOR RWY 17L) THAT FURTHER DECREASED BRAKING EFFECTIVENESS AT THE END OF RWY 35R. TO CORRECT THIS OCCURRENCE A MORE AGGRESSIVE USE OF REVERSE THRUST UPON TOUCHDOWN AND DECELERATING MORE RAPIDLY TO LOW SPD USING REVERSE THRUST, BEFORE REACHING THE RWY END.

Data retrieved from NASA's ASRS site as of July 2007 and automatically converted to unabbreviated mixed upper/lowercase text. This report is for informational purposes with no guarantee of accuracy. See NASA's ASRS site for official report.