Narrative:

After making a normal visual approach and landing to runway 21 at lyh (while transitioning to taxi), ie, aerodynamic flight control had decayed. I armed the nosewheel steering system with the arming switch and attempted to engage the nosewheel steering engage button on the power lever. The nosewheel steering at first seemed to engage for about a half second, then I realized I had lost or never had nosewheel steering. The aircraft was by this time veering to the right towards a snow berm at the runway edge. I used all the opposite reverse available and maximum braking, but it looked like at least the right main would exit the runway. At this time I stopped and feathered both engines to prevent damage to propellers and engines while still utilizing maximum braking. The aircraft came to a stop with the nosewheel approximately 15 ft off the runway and the right mains 12 inches off with no damage to occupants or aircraft. Upon inspection the nosewheel steering engage button assembly was found to be loose. The aircraft had been sitting for a week alternately freezing and thawing which could have caused condensation to form in and around the microswitch (nosewheel steering). Additionally, by the way the aircraft pulled to the right it could have possibly had a frozen brake.

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Original NASA ASRS Text

Title: ACR FLYING AN SA227 LEAVES RWY AT LYNCHBURG, VA, WITH NOSEWHEEL STEERING PROBS.

Narrative: AFTER MAKING A NORMAL VISUAL APCH AND LNDG TO RWY 21 AT LYH (WHILE TRANSITIONING TO TAXI), IE, AERODYNAMIC FLT CTL HAD DECAYED. I ARMED THE NOSEWHEEL STEERING SYS WITH THE ARMING SWITCH AND ATTEMPTED TO ENGAGE THE NOSEWHEEL STEERING ENGAGE BUTTON ON THE PWR LEVER. THE NOSEWHEEL STEERING AT FIRST SEEMED TO ENGAGE FOR ABOUT A HALF SECOND, THEN I REALIZED I HAD LOST OR NEVER HAD NOSEWHEEL STEERING. THE ACFT WAS BY THIS TIME VEERING TO THE R TOWARDS A SNOW BERM AT THE RWY EDGE. I USED ALL THE OPPOSITE REVERSE AVAILABLE AND MAX BRAKING, BUT IT LOOKED LIKE AT LEAST THE R MAIN WOULD EXIT THE RWY. AT THIS TIME I STOPPED AND FEATHERED BOTH ENGS TO PREVENT DAMAGE TO PROPS AND ENGS WHILE STILL UTILIZING MAX BRAKING. THE ACFT CAME TO A STOP WITH THE NOSEWHEEL APPROX 15 FT OFF THE RWY AND THE R MAINS 12 INCHES OFF WITH NO DAMAGE TO OCCUPANTS OR ACFT. UPON INSPECTION THE NOSEWHEEL STEERING ENGAGE BUTTON ASSEMBLY WAS FOUND TO BE LOOSE. THE ACFT HAD BEEN SITTING FOR A WK ALTERNATELY FREEZING AND THAWING WHICH COULD HAVE CAUSED CONDENSATION TO FORM IN AND AROUND THE MICROSWITCH (NOSEWHEEL STEERING). ADDITIONALLY, BY THE WAY THE ACFT PULLED TO THE R IT COULD HAVE POSSIBLY HAD A FROZEN BRAKE.

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.