SF50Vision Jet

Parts most often named Housing (15)

RETARD BREAKER POINT LEAD WIRE ATTACHED TO DISTRIBUTOR HOUSING, HAS TERMINAL END BROKEN. WIRE IS TOO SHORT TO CRIMP NEW TERMINAL END ON. WIRE IS ATTACHED TO HOUSING WITH EPOXY LIKE COVERING AND NO ALLOWANCE IN THE MAINTENANCE MANUAL FOR SPLICING OR REPLACING WIRE. REPLACED HOUSING WITH NEW.

THE RETARD BREAKER POINTS WIRE THAT IS ATTACHED TO THE DISTRIBUTOR HOUSING WAS FOUND TO HAVE THE TERMINAL END THAT ATTACHES TO THE POINTS BROKEN. THE WIRE WAS TOO SHORT TO ALLOW FOR CRIMPING A NEW TERMINAL ON. THE WIRE IS ATTACHED TO THE HOUSING AND COVERED WITH AN EPOXY LIKE MATERIAL, AND THERE IS NO PROVISION IN THE MAINTENANCE MANUAL FOR SPLICING OR REPLACING THIS WIRE. THE HOUSING WAS REPLACED WITH A NEW UNIT.

Parts most often named Compressor (2) · Blade (1) · Rotor (1)

THE ACFT WAS SQUAWKED FOR A BANG NOISE DURING FLIGHT. THE ENGINE WAS BORESCOPE INSPECTED AND FOUND TO HAVE A DAMAGED HPC ROTOR. DISASSEMBLY OF THE ENGINE REVEALED A MISSING THIRRD STAGE IP BLADE. HPC ROTOR WAS SECONDARY DAMAGE.

AFTER A FIELD EVENT, THE REQUIRED VIBRATION TESTING INDICATED UNACCEPTABLE 1ELP LEVELS AROUND .8 IPS. FIELD TROUBLE SHOOTING DISCOVERED A MISSING 3RD STAGE IP ROTOR BLADE. DISASSEMBLY OF THE ENGINE HAS CONFIRMED ONE MISSING 3RD STAGE IP BLADE. THE IP ROTOR HAS BEEN HELD FOR FURTHER INVESTIGATION IF NECESSARY.

Parts most often named Pad (2) · Brake Pads (1)

DURING CONDITIONING OF NEW BRAKE PADS THE LEFT BRAKE FAILED RESULTING IN LOSS OF BRAKING AND LOSS OF STEERING CONTROL. UPON EXAMINATION THE LEFT BRAKE OUTBOARD BRAKE PAD LINING WAS MISSING FROM THE BACKING PLATE. PIECES OF THE LINING WERE FOUND IN THE BRAKE ASSEMBLY AND ON THE GROUND.

Parts most often named B-Nut (1) · Shutoff Valve (1)

Parts most often named Transponder (1) · Shutoff Valve (1)

SLC IS REPORTING [tail no. removed], AN R66 IN FLORIDA, AS WELL AS [tail no. removed] OUT OF SLC AS [tail no. removed]. IT IS NOT A ONE TIME OCCURRENCE. IT’S BEEN GOING ON FOR MONTHS.

Parts most often named Duct (1) · Unknown (1)

ON DEPARTURE, RECEIVED ECS CONTROL OVERHEAT, ECS CONTROL FAIL, TCV FAIL, AND A BURNING ODOR. TROUBLESHOT THE BLEED AIR SYSTEM TO SEE THE CAUSE OF THE CAS MESSAGES. FOUND THE AIRE DUCT LOOSE ON THE RAM AIR PLENUM TO BASS HEAT EXCHANGER PLENUM IN THE TAIL CONE. SECURED THE AIR DUCT AND SYSTEM FUNCTIONED OK.

Parts most often named Not Reported (1)

Parts most often named Fuel Control (1)

FADEC CTRL DEGRADED 58 (FUEL METERING VALVE) ENGINE POWER FLUCTUATES AT MCT ON LANDING, THRUST LEVER IDLE POWER REMAINED AT 26%

Parts most often named Pitot System (1)

DISCREPANCY FROM PILOT MARK HARRIS; SFD IAS AND ALT MISCOMPARE ALERTS FOLLOWED BY FROZEN IAS AND ALTITUDE INDICATIONS. AT 6000, INSTRUMENTS RETURNED TO NORMAL. FINDINGS AND FIX ARE STILL IN WORKS AND WILL BE REPORT ONCE COMPLETED. CIRRUS AIR SAFETY TEAM AND ENGINEERING SHOULD HAVE A REPORT FROM THE AIRCRAFT DOWNLOAD.

Parts most often named Duct (1)

ECS BLEED HOT AND THEN OVERHEAT MESSAGE. ON REMOVING THE INTERIOR OF THE BAGGAGE COMPARTMENT, IT WAS DISCOVERED THAT THE RAM AIR PLENUM HAD MELTED. FURTHER REVIEW SHOWED THAT THE RAM AIR DUCT HAD COME OFF OF THE PLENUM ITSELF.