N421GF

CESSNA 421C · Valid Registration

Registered owner: GEAFR LLC, DE (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

O · 2004-08-02 Unresolved
ATA 8520

CRANKSHAFT HAD BEEN ULTRASONIC INSPECTED IAW APPLICABLE CSB 99-6A DURING OVERHAUL. RETURNED TO SERVICE AND AFTER 141.1 HOURS, FAILED IN SAME GENERAL OF REQUIRE INSPECTIONS. BROKEN AT NR 3 MAIN JOURNAL TO NR 5 ROD THROW.

Source: SDR VA12004F00000 · FAA SDRS
O · 2004-06-15 Unresolved
ATA 7310

PILOT EXPERIENCED EGT FLUXUATIONS, MADE PRECAUTIONARY LANDING. INSPECTION REVEALED CYLINDER NR 4 INJECTOR LINE WAS CRACKED AND LEAKING FUEL AT THE BASE OF THE BRAZED ON SLEEVE BETWEEN THE SLEEVE AND THE BALL END.

Source: SDR 2004FA0000632 · FAA SDRS
O · 2003-10-10 Matched by certificate designator
ATA 6121

ON TAKE OFF THE RT ENGINE FEATHERED. INSPECTION REVEALED PROPELLER SYNCROPHASER COIL HAD BECOME SEPARATED FROM THE GOVERNOR BODY, CAUSING THE PROPELLER TO FEATHER. THE ATTACHING STUDS ON THE COIL HAD SHEARED AND BECAME BOUND UP WITH THE FLYWEIGHT ASSY. PULLING THE METERING ROD NTO THE FEATHER POSITION. RECOMMEND A CLOSER INSPECTION OF THE (PN C20722) COIL OR POSSIBLY REPLACEMENT AT OVERHAUL. (K)

Source: SDR J7B2003F00001 · FAA SDRS
K · 1999-05-01 Unresolved
ATA 8500

PILOT REPORTED EXCESSIVE OIL LEAK ON RIGHT ENGINE CAWLING PULLED AND 3 INCH - 4 INCH CRACK NOTED AT NR 5 CYLINDR BASE. IDENTIDAL PROBLEM OCCURRED.

Source: SDR 99ZZZX2275 · FAA SDRS