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Aircraft record

N5614C1978 Cessna 414A

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Jul 7, 2017.

Safety record in brief:No NTSB accidents or incidents since 198210 ADs may apply6 service difficulty reports

Registration
Deregistered
Last based in
Blanding, UT
owner city / state
Engine
TSIO-520 SER · 300 hp
Cont Motor
Owners
1
since 1997
NTSB events
None
since 1982
ADs may apply
10
confirm with A&P
Service reports
6
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Pacific Air Ambulance
Owner type
Corporation
City, state
Blanding, UT
Certificate issued
Sep 16, 1997
Canceled
Jul 7, 2017
Airworthiness
Standard · Normal
Airworthiness date
Nov 15, 1978

We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.

Airframe & engine

FAA Registry + type data

Airframe

Manufacturer
Cessna
Model
414A
Year
1978
Serial number
414A0203
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
8
Engines
2
Max takeoff weight
Up to 12,499 lb
Mode S code
A72D88

Engine

Make and model
Cont Motor Tsio-520 Ser
Type
Reciprocating
Power
300 hp

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 1997 – 2017Pacific Air AmbulanceBlanding, UT
  2. until 1955Cessna Aircraft CoWichita, KS · different airframe: Cessna 140b S/N 15547

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

Accident history for this model

ADs published since 1998 that may apply (10)

These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.

ADSubjectEffectiveApplies to
2017-10-09Textron Aviation Inc. AirplanesJun 7, 2017Airframe (414A)Certain serial numbers: 402C 402C0001–402C1020; 414A 414A0001–414A1212. Only with: Equipped with Cessna Multi-Engine Service Kit SK402-47 (Original Issue, Rev A, or Rev B) or nacelle fittings P/Ns 5292029-9, -10, -11, -12, -21, -22, -23, or -24.
2016-17-08Elevator Tab Control SystemSep 12, 2016Airframe (414A)
2015-07-03Nacelles/PylonsApr 24, 2015Airframe (414A)Certain serial numbers: 402C 402C0001–402C1020; 414A 414A0001–414A1212
2012-23-01WingsDec 26, 2012Airframe (414A)Only with: Model 402C modified by STC SA927NW; Model 414A modified by STC SA892NW.
2009-16-03Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 Series Reciprocating…Sep 9, 2009Engine (TSIO-520 SER)Only with: SAP investment cast cylinder assemblies P/Ns SA52000-A1, SA52000-A20P, SA52000-A21P, SA52000-A22P, SA52000-A23P, SA55000-A1, or SA55000-A20P installed.
Show all 10 ADs
ADSubjectEffectiveApplies to
2005-20-25The Cessna Aircraft Company Models 401, 401A, 401B, 402, 402A, 402B, 402C, 404, 411…Nov 9, 2005Airframe (414A)Certain serial numbers: 401 655; 401 401-0001–401-0322; 401A 655; 401A 401A0001–401A0132; 401B 401B0001–401B0221; 402 402-0001–402-0322; …. Only with: Equipped with an avionics bus circuit breaker switch P/N CM3589-50, 593-250-101, 593-250-102, W31-X2M5A-50, or W31-X1000-50.
2005-12-13Cessna Aircraft Company Models 402C and 414A AirplanesJun 22, 2005Airframe (414A)
2000-01-16Cessna Aircraft Company 300 and 400 Series AirplanesFeb 15, 2000Airframe (414A)
98-24-14Cessna Aircraft Company Models 340A and 414A AirplanesDec 21, 1998Airframe (414A)Certain serial numbers: 340A 215–1817; 414A 1–1212. Only with: Equipped with any WYE tube P/N 9910299-25 or P/N 9910299-26 in the engine exhaust system.
98-04-28Cessna Aircraft Company Models T303, 310R, T310R, 335, 340A, 402B, 402C, 404, F406, 414…Mar 13, 1998Airframe (414A)

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (6)

Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.

  • Flight controls · pushrod · failedAug 24, 2004

    AILERON TRIM PUSH ROD ASSY (PN 51155464) FAILED, CAUSING THE AILERON TRIM TAB TO BIND IN THE UP POSITION. AIRCRAFT LANDED AT AN AUXILIARY AIRFIELD WITHOUT INCIDENT. PUSH ROD REPLACED WITH NEW MFG PUSH ROD ASSY (PN 51155464). OLD PUSH ROD, ROD END BEARING FAILED. THERE IS NO TIME REPLACEMENT OF…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · actuator · inoperativeNov 9, 1999

    NOSE GEAR COLLAPSED ON LANDING CAUSING DAMAGE TO BOTH PROPS, ENGS, AND NOSE STRUCTURE DAMAGE TO BOTTOM OF ACFT FROM RADAR DOME TO BS 43.0. NOSE OF THE ACFT WAS PLACED ON A JACK. NOSE GEAR ACTUATOR WAS LOCKED DOWN. THERE WAS NO PHYSICAL DAMAGE TO NOSE GEAR UNLOCKING OF LOCKING SYS. NOSE GEAR…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine indicating · tach generator · failedSep 11, 1998

    THE LT ENGINE RPM GAUGE FAILED ON RUN-UP. DISCOVERED THE TACHOMETER GENERATOR P/N 22A667 DRIVE SHAFT HAD SHEARED. THE TACHOMETER GENERATOR WAS REPLACED AND AIRPLANE RETURNED TO SERVICE. THE TACHOMETER HAD BEEN OVERHAULED AND PUT BACK INTO SERVICE 3-29-96. TOTAL TIME SINCE OVERHAUL 1497.7 HOURS.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 6 reports
  • Hydraulic power · pump · leakingApr 22, 1997

    PILOT REPORTED BOTH LEFT AND RIGHT HYDRAULIC FLOW LIGHTS ON THE CAUTION PANEL WERE ILLUMINATED. LANDING GEAR WAS EXTENDED USING THE EMERGENCY EXTENSION PROCEDURE. AIRPLANE LANDING WITHOUT INCIDENT. FLUID DISCOVERED LEAKING FROM RIGHT ENGINE NACELLE DRAIN. DISCOVERED THE RIGHT HYDRAULIC PUMP SHAFT…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Hydraulic power · packing · cutJan 27, 1997

    PILOT REPORTED THAT BOTH LEFT AND RIGHT HYDRAULIC PRESSURE CAUTION LIGHTS WERE ILLUMINATED. LANDING GEAR WOULD NOT EXTEND. LANDING GEAR WAS EXTENDED USING THE EMERGENCY EXTENSION PROCEDURE. AIRPLANE WAS JACKED AND THE LANDING GEAR OPERATIONAL CHECK WAS PERFORMED. FLUID WAS DISCOVERED LEAKING FROM…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Hydraulic power · pump · seal failedNov 5, 1996

    LT AND RT HYD LOW FLOW LITES CAME ON IN FLIGHT. LANDING GEAR HAD TO BE EXTENDED USING THE LANDING GEAR EMERGENCY PROCEDURE. ACFT LANDED WITHOUT INCIDENT. RIGHT HYD PUMP NOSE SEAL LEAKED HYDRAULIC FLUID OVERBOARD THROUGH THE NOSE CASE DRAIN. PUMP REPLACED. AIRCRAFT RETURNED TO SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Related aircraft

Show all 8 related aircraft
All 363 registered Cessna 414A aircraft

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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