Location
Wichita, KS
Owner type
Corporation
Serial number
4140520
Type
Fixed wing multi engine
Engine
Reciprocating
Airworthiness
Standard, normal
Airworthiness date
May 14, 1974
Certificate issued
August 5, 2026
Expires
August 31, 2033
Mode S code
A4E311

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Continental TSIO-520 model are included below.

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Airworthiness directives that may apply · 85

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1969In forceSuperseded2026
ADs by the year they took effect: 88 ADs
19691
19701
19711
19722
19742
19751
19764
19771
19784
19792
19803
19812
19822
19831
19851
19872
19885
19892
19903
19911
19933
19951
19961
19971
19984
19991
20002
20011
20042
20054
20072
20081
20092
20102
20112
20122
20142
20163
20182
20201
20222
20236
See all 97 ADs

Information bulletins that may apply · 23

Advisory, not mandatory.

See all 24 bulletins

NTSB investigations · 1

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

FAA incident reports · 4

FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.

Service difficulty reports · 6

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR 2RM2017F00001Lifter · spalledENGINE 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.Oct 17, 2017 · N414AW · Cessna 414 · Reciprocating Engine Power SectionSDR 2RM2017F00000Lifter · spalledENGINE 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.Oct 17, 2017 · N414AW · Cessna 414 · Reciprocating Engine Power SectionSDR A6WA200840624Support · crackedAFT 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.Dec 1, 2008 · N414AW · Cessna 414 · Fuselage Main, Attach FittingsSDR K2Z2005F00001Gasket · failedPILOT 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)Nov 6, 2005 · N414AW · Cessna 414 · Engine (Turbine/Turboprop)SDR F2P2003F00001Line · corrodedPILOT 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 WSep 25, 2003 · N414AW · Cessna 414 · Landing Gear Brake SystemSDR F2P2002F00000Line · corrodedWHILE 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 ANOct 24, 2002 · N414AW · Cessna 414 · Passenger Oxygen System

STCs that may be installed · 402

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 402 STCs