N392AS
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
6 reports on file, 2010-11-30 – 2016-07-11.
Part: PDU — INTERMITTENT (TE FLAP) · airframe 3,811 hrs · 2,379 cycles
FLAP FAIL CAS MESSAGE DURING DECENT, WHEN MOVING FLAP SELECTOR FROM 0 TO 1. QRH FOLLOWED AND CREW DIVERTED. MX PERFORMED MULTIBLE OPERATIONAL CHECKS IAW MM. NO ISSUE IDENTIFIED. MANUFACTURER IS RECOMMENDING REPLACING THE FCES IAW SERVICE BULLETIN 505-27-0022. REPLACED FCE 1 & 2 IAW SB AND FLAP POWER DRIVE UNIT. OPS AND FUNCTIONAL CHECKED IAW AMM. FCE REMOVED, PN 462900-1011, SN 0124, 0097. FCE INSTALLED PN 462900-1017, SN 0837, 0840.
Part: SCREW — BACKED OUT (WINDSHIELD) · airframe 3,256 hrs · 2,030 cycles
FOUND TORQUE ON WINDSHIELD SCREW 1/4 TO 1 TURN LOOSE ON 50% OF SCREWS.
Part: INLET — CRACKED (ZONE 400) · airframe 416 hrs · 279 cycles
ON PREFLIGHT INSP, 2 CRACKS WERE FOUND IN THE RT ENGINE INLET. THE INLET WAS INSPECTED WITH EDDY CURRENT AND ANOTHER 8 CRACKS WERE FOUND. INLET WAS REPLACED AND ACFT WAS RETURNED TO SERVICE. A VIBRATION AND SONIC SURVEY WERE COMPLIED WITH, NO DEFECTS WERE NOTED.
Part: TRANSDUCER — INTERMITTENT (ZONE 100) · airframe 411 hrs · 276 cycles
CAS MESSAGE "BRAKE FAIL". ACFT DIVERTED TO AIRPORT WITH LONGER RUNWAY. ON LANDING, THE BRAKES WERE FAILED THE ACFT WAS STOPPED WITH THE EMERGENCY BRAKES. INSTALLED NEW LT BRAKE PEDAL TRANSDUCER PN Q3008, SN 845836. OPS CHECKED OK.
Part: INLET — CRACKED (NR 2 ENGINE) · airframe 364 hrs · 246 cycles
DURING POSTFLIGHT, IT WAS DISCOVERED THAT THE INLET LIP ON THE NR2 ENGINE IS COMING APART. IT HAS A SEGMENT OF MATERIAL MISSING. CRACKED IN 2 OTHER LOCATIONS AND 3 RIVET HEADS MISSING IN ANOTHER LOCATION.
Part: PROBE — INOPERATIVE (ZONE 100) · airframe 343 hrs · 234 cycles
ON TAKEOFF ROLL CREW HAD CAS MESSAGE INDICATING AP FAIL AND YD FAILED . TAKEOFF WAS ABORTED AND ACFT WAS RETURNED TO FBO. RT SMART PROBE WAS REPLACED AND ACFT WAS RETURNED TO SERVICE.