N414AW

CESSNA 414 · Fixed-wing multi-engine · 2 engines · 7 seats · Valid Registration

Registered owner: ALYCONE TRUST CORP TRUSTEE, KS (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

Accident · 1996-05-27 Unresolved
Cessna 414 No injuries Part 91 — operator not named in the NTSB record
Source: NTSB case FTW96LA227

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, 2002-10-24 – 2017-10-17.

OTHER · 2017-10-17 Unresolved
ATA 8520

Part: LIFTER — SPALLED (ENGINE)

ENGINE WAS DISASSEMBLED FOR PROP STRIKE INSPECTION. FOUND LIFTERS BEGINNING TO SPALL AND WERE REPLACED WITH NEW LIFTERS AT THIS TIME TO PREVENT DAMAGE TO CAMSHAFT. LIFTERS WERE INSTALLED IN MAY OF 2010 AND HAVE 303.7 HOURS SINCE NEW.

Source: SDR 2RM2017F00000
OTHER · 2017-10-17 Unresolved
ATA 8520

Part: LIFTER — SPALLED (ENGINE)

ENGINE WAS DISASSEMBLED FOR PROP STRIKE INSPECTION. FOUND LIFTERS BEGINNING TO SPALL AND WERE REPLACED WITH NEW LIFTERS AT THIS TIME TO PREVENT DAMAGE TO CAMSHAFT. LIFTERS WERE INSTALLED IN MAY OF 2010 AND HAVE 303.7 HOURS SINCE NEW.

Source: SDR 2RM2017F00001
OTHER · 2008-12-01 Matched by certificate designator
ATA 5340

Part: SUPPORT — CRACKED (BS 718) · airframe 16,824 hrs · 15,328 cycles

AFT COMPARTMENT RT HYDRAULIC SUPPORT AT FS 718 FOUND CRACKED IN AFT LOWER CORNER. AFT COMPARTMENT RT HYDRAULIC SUPPORT AT FS 718 ON AFT LOWER CORNER REPAIRED IAW CRJ200 REO 601R-53-62-031 REV A.

Source: SDR A6WA200840624
FLUID LOSS; WARNING INDICATION · 2005-11-06 Matched by certificate designator
ATA 7200

Part: GASKET — FAILED (ROCKER BOX)

PILOT NOTED DROP IN ENGINE OIL PRESSURE IN CRUISE FLIGHT. POSTFLIGHT INSPECTION REVEALED SILICON GASKET (SUCKED) INTO THE ROCKER BOX ALLOWING SUBSTANTIAL OIL LOSS. ENGINE SHUTDOWN, PROP FEATHERED, PRECAUTIONARY LANDING ACCOMPLISHED WITHOUT INCIDENT. (K)

Source: SDR K2Z2005F00001
OTHER · 2003-09-25 Matched by certificate designator
ATA 3240

Part: LINE — CORRODED (RT BRAKE)

PILOT REPORTED LOSS OF RIGHT SIDE BRAKE PRESSURE UPON LANDING. FOUND RT BRAKE MASTER CYLINDER EMPTY. FOUND HYDRAULIC LEAK UNDER COPILOT SIDE FLOOR. COURSE OF LEAK DUE TO CORRODED ALUMINUM BRAKE LINE, BRAKE LINE CORROSION CAUSED BY SCATT DUCT STEEL SUPPORT WIRE IN CONTACT WITH BRAKE LINE. FOUND SIMILARLY CORRODED OXYGEN LINES IN HEADLINER ON SAME AIRCRAFT LAST YEAR. SAME CAUSE. AIR DUCTS IN CONTACT WITH ALUMINUM LINES. CAREFUL INSPECTION AND REPLACEMENT OF ALUMINUM LINES THAT ARE IN CONTACT WITH SCATT TYPE AIR DUCTS.

Source: SDR F2P2003F00001
OTHER · 2002-10-24 Matched by certificate designator
ATA 3520

Part: LINE — CORRODED (OXYGEN SUPPLY)

WHILE PERFORMING AN OXYGEN SYSTEM FUNCTION CHECK A OXYGEN LEAK WAS DETECTED BETWEEN THE TWO LEFT SIDE PASSENGER OVERHEAD (O2) OUTLETS. A SMALL HOLE WAS FOUND IN (O2) LINE. THIS HOLE WAS A RESULT OF DISSIMILAR METAL CORROSION BETWEEN THE ALUMINUM (O2) LINE AND THE STEEL SUPPORT SPRINGS OF THE PASSENGER VENTILATION DUCT. UPON FURTHER INSPECTION CORROSION HAD DEVELOPED ON OTHER (O2) SUPPLY LINES WERE THESE LINES ARE IN CONTACT WITH THE VENTILATION DUCTS.

Source: SDR F2P2002F00000