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N86VS

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Cessna 414 · Continental TSIO-520 series

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Registered owner
Plotkin Aviation LLC
Location
Boca Raton, FL
Owner type
LLC
Serial number
414-0955
Type
Fixed wing multi engine
Engine
Reciprocating
Airworthiness
Standard, normal
Airworthiness date
June 30, 1977
Certificate issued
January 20, 2023
Expires
January 31, 2030
Mode S code
ABCE6A
Cessna 414Airframe model · 7 seats · 2 engines · 242 registeredTCDS A7CEAirframe · Cessna 414TCDS E8CEEngine · Continental TSIO-520 series

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
See all 97 ADs

Information bulletins that may apply · 23

Advisory, not mandatory.

See all 24 bulletins

NTSB investigations

No NTSB investigations matched to N86VSMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Cessna 414 aircraft

FAA incident reports · 1

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

Incident 19990624022089ILevel Off Touchdown · Redmond, OROn approach to rdm from bakersfield, CA pilot heard a "bang" when extending gear. Nose gear did not show green. Tower confirmed lack of extension. Pilot reviewed checklist, circled airport to use fuel to 10 gal. Then performed controlled landing. Butler…Jun 24, 1999 · Minor damage

Service difficulty reports · 3

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

SDR 2025F00273Support · corrodedDURING A PREFLIGHT WALKAROUND, SURFACE CORROSION WAS OBSERVED ON THE VERTICAL STABILIZER AFT SECTION. AFTER CLOSER INSPECTION SEVERE DELAMINATION WAS SEEN ON THE AFT VERTICAL SUPPORT ANGLES AND AFT STAB BULKHEAD SECTION. THE RUDDER TRIM TAB BRACKET ALSO HAD SINov 26, 2025 · N86VS · Cessna 414 · Vertical Stabilizer Miscellaneous StructureSDR KISA202602050001Angle · corrodedDURING A PREFLIGHT WALK AROUND CORROSION WAS OBSERVED ON THE AFT SPAR ANGLE CHANNEL OF THE VERTICAL STABILIZER. UPON FURTHER INVESTIGATION SIGNIFICANT INTERGRANULAR CORROSION WAS FOUND RESULTING IN EXFOLIATION OF THE SURFACE OT THE SPAR ANGLE. THIS RESULTED INNov 25, 2025 · N86VS · Cessna 414 · Vertical Stabilizer Miscellaneous StructureSDR 99ZZZX2650Fender · brokePILOT REPORTED HEARING A 'BANG' SHORTLY AFTER SELECTING GEAR DOWN. NOSE GEAR DID NOT EXTEND. INVEST REVEALED THE NOSE WHEEL FENDER LODGED ABOVE NOSE GEAR IN THE WHEELWELL. THIS JAMMED THE UPLOCK MECHANISM. THE NOISE WAS CAUSED BY THE RETRACT ROD FITTING BRJun 23, 1999 · N86VS · Cessna 414 · Landing Gear/Wheel Fairing

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