Narrative:

En route from bna airport to jqf airport; near the time stated above in cruise with the autoplt engaged; I was given permission for heading deviations 'as needed' for navigation around active thunderstorm cells. During the time I was circumnaving a cumulo nimbus cell; the aircraft entered an extreme nose down pitch altitude; excessive back pressure was applied and the autoplt disengaged. After the autoplt was disengaged; I was able to regain pitch control and retrim the aircraft from its full nose down setting. As I was returning to 13000 ft; I noticed false indications from the attitude indicator and no suction. The attitude indicator is the only primary instrument on this aircraft operated from vacuum and the 'fcs' receives pitch information from the attitude indicator. The directional gyro is slaved. Leveling back at 13000 ft I advised ZTL that I had a vacuum failure and needed to stay clear of the clouds as much as possible. I was told that there was crossing traffic at 12000 ft and that a pilot deviation of 400 ft had occurred and to call them. The flight was continued partial panel to jqf airport. Maintenance personnel were contacted to troubleshoot the duel vacuum system. Both vacuum pumps were found to be sheared at the shaft and the vacuum out indicators were inoperative. Repairs were made and the aircraft returned to service with a note on the shut down checklist to check the vacuum out indicators after engine shutdown.

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Original NASA ASRS Text

Title: CESSNA P210 PLT HAS VACUUM SYS FAIL AND ACFT HAS ALT EXCURSION.

Narrative: ENRTE FROM BNA ARPT TO JQF ARPT; NEAR THE TIME STATED ABOVE IN CRUISE WITH THE AUTOPLT ENGAGED; I WAS GIVEN PERMISSION FOR HDG DEVS 'AS NEEDED' FOR NAV AROUND ACTIVE TSTM CELLS. DURING THE TIME I WAS CIRCUMNAVING A CUMULO NIMBUS CELL; THE ACFT ENTERED AN EXTREME NOSE DOWN PITCH ALT; EXCESSIVE BACK PRESSURE WAS APPLIED AND THE AUTOPLT DISENGAGED. AFTER THE AUTOPLT WAS DISENGAGED; I WAS ABLE TO REGAIN PITCH CTL AND RETRIM THE ACFT FROM ITS FULL NOSE DOWN SETTING. AS I WAS RETURNING TO 13000 FT; I NOTICED FALSE INDICATIONS FROM THE ATTITUDE INDICATOR AND NO SUCTION. THE ATTITUDE INDICATOR IS THE ONLY PRIMARY INST ON THIS ACFT OPERATED FROM VACUUM AND THE 'FCS' RECEIVES PITCH INFO FROM THE ATTITUDE INDICATOR. THE DIRECTIONAL GYRO IS SLAVED. LEVELING BACK AT 13000 FT I ADVISED ZTL THAT I HAD A VACUUM FAILURE AND NEEDED TO STAY CLR OF THE CLOUDS AS MUCH AS POSSIBLE. I WAS TOLD THAT THERE WAS XING TFC AT 12000 FT AND THAT A PLTDEV OF 400 FT HAD OCCURRED AND TO CALL THEM. THE FLT WAS CONTINUED PARTIAL PANEL TO JQF ARPT. MAINT PERSONNEL WERE CONTACTED TO TROUBLESHOOT THE DUEL VACUUM SYS. BOTH VACUUM PUMPS WERE FOUND TO BE SHEARED AT THE SHAFT AND THE VACUUM OUT INDICATORS WERE INOP. REPAIRS WERE MADE AND THE ACFT RETURNED TO SVC WITH A NOTE ON THE SHUT DOWN CHKLIST TO CHK THE VACUUM OUT INDICATORS AFTER ENG SHUTDOWN.

Data retrieved from NASA's ASRS site as of January 2009 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.