Narrative:

Attitude indicator was a mechanical (rotor) failure. Alternator failure was a mechanical (sealed bearing) failure. Neither are inspected or are annual svcable items. I was attempting to maintain VFR on top with the altitude failure and proceed to VFR landing conditions when the alternator system failed. Emergency was not declared, only immediate assistance from approach. System failures were reported to ATC. Altimeter and static check was not current to accept an IFR clearance. Localizer approach was accepted and used to land as soon as practical.

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Original NASA ASRS Text

Title: PLT OF AN SMA SEL PVT ACFT REQUESTED AN ATC ASSISTANCE AFTER FAILURE OF THE ACFT'S ATTITUDE INDICATOR AND THE ALTERNATOR DURING AN 'ON-TOP' FLT.

Narrative: ATTITUDE INDICATOR WAS A MECHANICAL (ROTOR) FAILURE. ALTERNATOR FAILURE WAS A MECHANICAL (SEALED BEARING) FAILURE. NEITHER ARE INSPECTED OR ARE ANNUAL SVCABLE ITEMS. I WAS ATTEMPTING TO MAINTAIN VFR ON TOP WITH THE ALT FAILURE AND PROCEED TO VFR LNDG CONDITIONS WHEN THE ALTERNATOR SYS FAILED. EMER WAS NOT DECLARED, ONLY IMMEDIATE ASSISTANCE FROM APCH. SYS FAILURES WERE RPTED TO ATC. ALTIMETER AND STATIC CHK WAS NOT CURRENT TO ACCEPT AN IFR CLRNC. LOC APCH WAS ACCEPTED AND USED TO LAND AS SOON AS PRACTICAL.

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.