N5421M

No registry detail on file · not in current registry

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.

17 reports on file, 2004-10-07 – 2008-07-23.

OTHER · 2008-07-23 Matched by certificate designator
ATA 8530

Part: CYLINDER — CRACKED (ENGINE)

CRACKED BETWEEN FIN NR 1 AND FIN NR 3 AFT OF THE INJECTOR. ECI REV 3 E SERIES CYLINDER. ALL DEFECTIVE. (K)

Source: SDR XGN2008F00006
OTHER · 2008-07-23 Matched by certificate designator
ATA 8530

Part: CYLINDER — CRACKED (ENGINE)

CRACKED BETWEEN FIN NR 1 AND FIN NR 3 AFT OF THE INJECTOR. MFG REV 3 E SERIES CYLINDER. ALL DEFECTIVE. (K)

Source: SDR XGN2008F00008
OTHER · 2008-07-23 Matched by certificate designator
ATA 8530

Part: CYLINDER — CRACKED (ENGINE)

CRACKED BETWEEN FIN NR 1 AND FIN NR 3 AFT OF THE INJECTOR. MFG REV E SERIES CYLINDER. ALL DEFECTIVE.

Source: SDR XGN2008F00007
OTHER · 2008-02-27 Matched by certificate designator
ATA 8530

Part: CYLINDER — CRACKED (ENGINE)

CYLINDER CRACKED BETWEEN NR 1-3 FIN BEHIND INJECTOR, DEFECTIVE PRODUCT. (K)

Source: SDR XGN2008F00005
OTHER · 2008-02-27 Matched by certificate designator
ATA 8530

Part: CYLINDER — CRACKED (ENGINE)

CYLINDER CRACKED BEHIND NR 1-3 FIN BY FUEL INJECTOR, DEFECTIVE PRODUCT. (K)

Source: SDR XGN2008F00004
OTHER · 2008-02-27 Unresolved
ATA 8530

Part: CYLINDER — CRACKED (ENGINE)

CRACKED BETWEEN FIN NR1-3, BEHIND INJECTOR. DEFECTIVE PRODUCT. (K)

Source: SDR 2008FA0000260
OTHER · 2008-02-27 Matched by certificate designator
ATA 8530

Part: CYLINDER — CRACKED (ENGINE)

CYLINDER CRACKED BETWEEN FIN NR1-3 BEHIND INJECTOR, DEFECTIVE PRODUCT. (K)

Source: SDR XGN2008F00003
Earlier reports · 2004–2005 · 10 reports

2005

OTHER · 2005-06-14 Matched by certificate designator
ATA 8530

Part: CYLINDER — CRACKED (ENGINE)

THIS CYLINDER WAS IN THE NR 6 POSITION AND IS A TYPE (X) HEAD. THIS CRACKED VYLINDER HEAD WAS FOUND AT THE 100 HOUR INSPECTION. WE ARE FINDING SIGNS OF AIR LEAKAGE ON THE EXHAUST SIDE OF THE CYLINDER HEAD WHEN DOING A COMPRESSION CHECK. WE ARE SPRAYING SOAPY WATER ON THE CYLINDER HEAD. (K)

Source: SDR XGN2005F00006
OTHER · 2005-06-04 Matched by certificate designator
ATA 8530

Part: CYLINDER — CRACKED (ENGINE)

CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)

Source: SDR XGN2006F00035
OTHER · 2005-04-24 Matched by certificate designator
ATA 8530

Part: CYLINDER — CRACKED (ENGINE)

CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)

Source: SDR XGN2006F00057
OTHER · 2005-04-18 Matched by certificate designator
ATA 8530

Part: CYLINDER — CRACKED (ENGINE)

CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)

Source: SDR XGN2006F00036
OTHER · 2005-04-05 Matched by certificate designator
ATA 8530

Part: CYLINDER — CRACKED (ENGINE)

CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)

Source: SDR XGN2006F00056
OTHER · 2005-04-05 Matched by certificate designator
ATA 8530

Part: CYLINDER — CRACKED (ENGINE)

CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)

Source: SDR XGN2006F00034
OTHER · 2005-03-05 Matched by certificate designator
ATA 8530

Part: CYLINDER — CRACKED (ENGINE)

CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)

Source: SDR XGN2006F00033
OTHER · 2005-03-02 Matched by certificate designator
ATA 8530

Part: CYLINDER — CRACKED (ENGINE)

CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)

Source: SDR XGN2006F00032

2004

OTHER · 2004-11-01 Matched by certificate designator
ATA 8530

Part: CYLINDER — CRACKED (ENGINE)

CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)

Source: SDR XGN2006F00031
PARTIAL RPM/PWR LOSS; WARNING INDICATION · 2004-10-07 Unresolved
ATA 8520

Part: PUSHROD — FAILED (ENGINE)

ENGINE HAD MANIFOLD AND FUEL PRESSURE VARIATION IN FLT, THE ACFT BEGAN TO VIBRATE AND THE PILOT SHUTDOWN ENGINE. THE NR 1 AND NR 2 ROD`S FAILED AND SEPARATED FROM THE CRANKSHAFT AND CREATED (2) LARGE HOLES IN THE CASE AND KNOCKING BOTH MAGNETOS LOOSE. THERE ARE SIGNS OF OIL STARVATION ON THE CRANK AND OVERHEATING ASIGNS ON THE CRANKSHAFT. REMOVAL OF OTHER CYLINDERS INDICATED OIL STARVATION ON THE NR (6) AND (5) ROD`S ALSO. OVERHEATING OF THE CRANK AT THOSE LOCATIONS IS EVIDENT. PILOT VERIFIED LOSING OIL PRESSURE BEFORE SHUTTING THE ENGINE. (K)

Source: SDR 2008F00023