N441SA

DIAMOND AIRCRAFT IND GMBH DA 42 NG · 2023 · Fixed-wing multi-engine · 2 engines · 4 seats · Valid Registration

Registered owner: CHEN AVIATION INC, NJ (owner ≠ operator)

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.

3 reports on file, 2002-01-03 – 2011-02-18.

OTHER · 2011-02-18 Matched by certificate designator
ATA 3244

Part: TIRE — FLAT (NLG) · airframe 13,932 hrs · 9,979 cycles

NOSE TIRE WENT FLAT ON LANDING. PULLED ONTO TAXIWAY AND STOPPED.

Source: SDR 3SVA441SA21811
PARTIAL RPM/PWR LOSS; WARNING INDICATION · 2004-07-15 Unresolved
ATA 7200

Part: ENGINE — POWER LOSS (RIGHT) · airframe 11,388 hrs · 8,590 cycles

UPON DEPARTURE AT APPROX 1000 FEET AGL, WHILE STILL IN THE TRAFFIC PATTERN, THE RIGHT SIDE ENGINE TORQUE ROLLED BACK TO LESS THAN 200LBS. THE PILOT ELECTED NOT TO TROUBLESHOOT THE LOSS OF TORQUE AND SECURED THE ENGINE AND RETURNED TO THE AIRPORT. SUBSEQUENT INSPECTION OF THE ENGINE AND FUEL SYSTEM REVEALED NO PROBLEMS. THE AIRCRAFT WAS THEN GROUND RUN FOR FIFTEEN MINUTES AT TAKEOFF AND CLIMB POWER WITH NO ANOMALIES NOTED. THE AIRCRAFT WAS THEN FLOWN TO BASE WITH NO INFLIGHT DISCREPANCIES. PROBABLE CAUSE OF POWER REDUCTION IS THE ELECTRONIC ENGINE CONTROL SYSTEM. TO HELP REDUCE RECURRENCES, A ROUTINE CLEANING OF ELECTRICAL CONNECTIONS BETWEEN THE EEC, FCU AND RELATED COMPONENTS DURING PHASE INSPECTIONS.

Source: SDR LATA02010501
OTHER · 2002-01-03 Unresolved
ATA 2435

Part: STARTER GEN — SHORTED (ENGINE)

COWLING OF AIRCRAFT FOUND WITH EXCESSIVE CARBON CONTAMINATION. REMOVED STARTER GENERATOR. TEARDOWN REPORT REVEALED THE STARTER SHORTED. CAUSE UNKNOWN.

Source: SDR LAT2002F00000