Service difficulty report · Gyro · Snias AS350B2

Difficulty date
October 5, 2013
Submitted
October 17, 2013
Operation
Air carrier
Aircraft
N985SA
Make and model
Snias AS350B2
Aircraft serial
3111
Aircraft time
15,732 hours, 21,122 cycles
Engine
Tmeca ARRIEL1D1
Engine time
3,731 hours, 2,165 cycles
Part
Gyro
Part number
5050010902
Part serial
22894
Condition
Failed
Location
Directional
Stage of operation
CR
How discovered
O
Nature of condition
B
Precautionary procedure
A

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

PILOT REPORTED AN ELECTRICAL TYPE BURNING ODOR FOLLOWED BY LIGHT WISPS OF SMOKE FROM UNDER THE INSTRUMENT PANEL HOOD. FLIGHT WAS ABORTED, AND A PRECAUTIONARY LANDING WAS MADE, WHERE THE ACFT WAS SHUTDOWN AND REMOVED FROM SERVICE. UPON FURTHER INSPECTION BY MAINTENANCE IT WAS DETERMINED THE DIRECTIONAL GYRO HAD OVERHEATED. THE AFT COVER OF THE DIRECTIONAL GYRO HAD CRACKED ALLOWING OVERHEATED GREASE TO SEEP FROM THE CASE. IT WAS DETERMINED THAT THE GREASE WAS THE SOURCE OF THE ODOR, AND WAS PRESUMED TO BE THE SOURCE OF THE LIGHT SMOKE. INSPECTION OF ALL THE OTHER INSTRUMENT SYS REVEALED NO OTHER DAMAGE. THE DIRECTIONAL GYRO WAS DISABLED, AND THE ACFT WAS GROUND RUN WITH ALL SYSTEMS RUNNING FOR APPROXIMATELY 15 MINUTES. ALL SYSTEMS FUNCTIONED NORMAL, WITH NO FURTHER INDICATION OF ODOR, OR SMOKE. A SHORT MAINTENANCE FLIGHT WAS CONDUCTED TO RETURN THE ACFT TO BASE. ALL SYSTEMS FUNCTIONED NORMAL, WITH NO PROBLEMS NOTED. A SERVICEABLE DIRECTIONAL GYRO WAS INSTALLED, AND THE ACFT WAS RETURNED TO SERVICE.