N93SF

ATA 7200

DURING DESCENT, AT 13,900 FT, EXPERIENCED A BRIEF LT ENGINE ROLLBACK. ALL IGNITERS AND PUMPS WERE ON AT THE TIME. RELIT ON ITS OWN, LEAVING THE LT BLEED AIR FAIL AND LT GEN FAIL WITH THE ASSOCIATED MASTER WARNING ANNUNCIATORS FLASHING. TURNED LT GENERATOR BACK ON. BLEED AIR LIGHT WENT OUT ON ITS OWN. CANCELED MASTER WARNING. DURING THE RNAV (GPS) 19, EXPERIENCED A SECOND LT ENGINE UNCOMMANDED SHUTDOWN WHILE PASSING ROUGHLY 8000 FT. THIS WAS APPROXIMATELY 8 MINUTES AFTER THE INITIAL FAILURE. SAME INDICATIONS EXISTED. NEITHER FAILURE RESULTED IN AN NTS LIGHT. ENGINE CONTINUED TO WINDMILL WITH OIL PRESSURE REMAINING IN GREEN ALTHOUGH TORQUE WAS AT ZERO OUTPUT. AT A REDUCED POWER SETTING FOR APPROACH WITH APPROXIMATELY 1100 LBS TORQUE WHEN SECOND FAILURE OCCURRED. DUE TO THE REDUCED POWER, HAD SOME MINOR YAW RATE ASSOCIATED WITH THE FAILURE AND CORRESPONDING TRIM WAS APPLIED. ATTEMPTED AN ENGINE AIRSTART, SUCCESSFUL. RETRIMMED AND CONTINUED THROUGH THE COMPLETION OF THE APPROACH AND LANDING. AFTER ARRIVAL, PERFORMED ENGINE RUNS WITH RAPID CHANGES IN POWER SETTINGS WITH THE FULL RANGE OF IN-FLIGHT POWER SETTINGS. NO ANOMALIES OF EITHER POWERPLANT OCCURRED DURING RUNS. COMPLIED WITH FLAME OUT CHECK IAW MM. NO DISCREPANCIES WERE FOUND. ALL PARAMETERS WERE NORMAL.

ATA 2435

DURING A CHECKRIDE, THE CHIEF PILOT SHUTDOWN THE RT ENGINE IN FLIGHT. WHEN ATTEMPTING RE-START, THE FUEL LEVER JAMMED IN THE CUTOFF POSITION. THE CREW CONDUCTED A SUCCESSFUL, UNEVENTFUL, SINGLE ENGINE LANDING AT THE BASE AIRPORT. UPON INVESTIGATION, THE TECHNICIAN DISCUSSED THE AFT SHROUD ON THE RT STARTER GENERATOR HAD SLIPPED AFT, BLOCKING THE LINKAGE THAT WAS IN CUTOFF. THE SHROUD WAS REPOSITIONED, THE SHROUD CLAMP SECURED. THE CUTOFF LINKAGE WAS THEN FOUND TO HAVE FREE AND NORMAL RANGE OF MOTION. (K)

ATA 2730

TORQUE TUBE MOUNT BRACKET WAS CRACKED FROM TAPER PIN HOSE (HEAD SIDE) TO THE END OF PART. TAPER PIN MIGHT HAVE BEEN OVERTORQUED.