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Aircraft record

N266211989 Cessna 550

DeregisteredUnclaimedSource: FAA, updated Oct 17, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Mar 22, 2021.

Safety record in brief:No NTSB accidents or incidents since 19827 ADs may apply7 service difficulty reports

Registration
Deregistered
Last based in
North Salt Lake, UT
owner city / state
Owners
1
since 2017
NTSB events
None
since 1982
ADs may apply
7
confirm with A&P
Service reports
7
since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026
Last registered owner
Tvpx Aircraft Solutions INC Trustee
Owner type
Corporation
City, state
North Salt Lake, UT
Certificate issued
Aug 28, 2017
Canceled
Mar 22, 2021
Airworthiness
Restricted · Aerial Advertising
Airworthiness date
Aug 4, 1997

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
550
Year
1989
Serial number
550-0593
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
8
Engines
2
Max takeoff weight
12,500 - 19,999 lb
Mode S code
A297FF

Engine

Make and model
P&W Canada Jt15d-4
Type
Turbo-fan
Power
2,500 lb thrust

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

Ownership history

Ownership history from FAA records
  1. 2017 – 2021Tvpx Aircraft Solutions INC TrusteeNorth Salt Lake, UT

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 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 (7)

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
2015-17-12Air ConditioningSep 29, 2015Airframe (550)Certain serial numbers: 500 0001–0689; 501 0001–0689; 550 0002–0733; 550 0801–1136; 551 0002–0733; 551 0801–1136; …. Only with: Air conditioning system installed via Cessna STC SA3849SW, SA7580SW, SA7753SW, or SA8918SW.
2013-09-11Air ConditioningJul 5, 2013Airframe (550)Certain serial numbers: 500 0001–0689; 501 0001–0689; 550 0002–0733; 550 0801–1136; 551 0002–0733; 551 0801–1136; …
2007-11-17Cessna Model 500, 501, 550, 551, S550, 560, 560XL, and 750 AirplanesJul 6, 2007Airframe (550)Serial numbers per Cessna Service Bulletins SB500-26-02, SB550-26-05, SB560-26-01, SB560XL-26-02, SB750-26-05, SBS550-26-02 (Table 1 of this AD)
2006-06-03Cessna Model 500, 501, 550, S550, 551, and 560 AirplanesApr 20, 2006Airframe (550)Certain serial numbers: 500 0001–0689; 501 0001–0689; S550 0001–0160; 550 0002–0733; 551 0002–0733; 550 0801–1075; …
2004-09-05Cessna Model 500, 501, 550, and 551 AirplanesJun 2, 2004Airframe (550)Certain serial numbers: 500 0001–0689; 501 0001–0689; 550 0002–0733; 551 0002–0733. Only with: Equipped with BFGoodrich brake assembly P/N 2-1528-6 or 2-1530-4.
Show all 7 ADs
ADSubjectEffectiveApplies to
98-04-38Cessna Model 500, 501, 550, 551, and 560 Series AirplanesMar 25, 1998Airframe (550)Only with: Equipped with pneumatic deicing boots.
95-25-10Cessna Model 441, 500, 550, and 560 Series AirplanesJan 22, 1996Airframe (550)Serial numbers per Allied Signal Aerospace Service Bulletins 103576-21-4054, 103576-21-4056, and 103648-21-4055. Only with: Equipped with Allied Signal outflow/safety valves identified in Allied Signal Aerospace Service Bulletins 103576-21-4054, 103576-21-4056, and 103648-21-4055.

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

Service Difficulty Reports (7)

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.

  • Landing gear · actuator · out of positionMar 18, 2008

    AIRCREW REPORTED LANDING GEAR WARNING HORN SOUNDED AND GEAR-IN-TRANSIT INDICATOR ILLUMINATED AS AIRCRAFT WAS BEING TOWED OVER A BUMP (HANGAR THRESHOLD). SCHEDULED FLIGHT WAS CANCELLED. MAINTENANCE CREW WAS ABLE TO DUPLICATE EVENT BY SLIGHT ACCELERATION OF TOW VEHICLE AND OBSERVED NOSE GEAR DOWN…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Flight controls · actuator · bindingMay 18, 2007

    FOLLOWING INSTALLATION OF A NEWLY OVERHAULED ELEVATOR TRIM TAB ACTUATOR, PARTIAL BINDING OF THE ACTUATOR OCCURRED. FURTHER INVESTIGATION REVEALED THAT THIS ACTUATOR HAD EXCESSIVELY WORN END BEARINGS ALLOWING LATERAL PLAY IN INTERNAL JACKSCREWS SUFFICIENT TO CAUSE BINDING ONCE INSTALLED. ALSO…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Flight controls · actuator · bindingMay 11, 2007

    A NEWLY OVERHAULED ELEVATOR TRIM TAB ACTUATOR WAS BINDING AND WOULD NOT PROVIDE ADEQUATE DEFLECTION AT THE TRIM TAB ONCE INSTALLED. FURTHER INVESTIGATION REVEALED THAT THIS ACTUATOR HAD EXCESSIVE PLAY AT THE END BEARINGS AND THAT THE PRIMARY SPROCKET PN WAS INCORRECT RELATIVE TO THE ASSEMBLY PN.…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 7 reports
  • Fuel · wire harness · chafedSep 25, 2003

    IN TROUBLESHOOTING A SUBMERGED FUEL BOOST PUMP CIRCUIT BREAKER POPPING, MAINTENANCE TECHNICIANS DISCOVERED THE FUEL BOOST PUMP ELECTRICAL HARNESS HAD CHAFFED THROUGH THE BUNDLE INSULATION AND WAS ARCING ON ALUMINUM FUEL LINE P/N 6526355-37 INSIDE THE WET WING. THE POTENTIAL FOR FUEL VAPOR IGNITION…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · skin · crackedApr 30, 2001

    DURING A SCHEDULED PHASE INSPECTION THE LEFT AILERON WAS REMOVED. UPON REMOVAL THE LEADING EDGE SKIN AT THE WEIGHT ATTACHMENT SCREWS WAS FOUND CRACKED. THIS HAD ALLOWED THE SKIN TO CRACK ABOVE AND BELOW A SCREW APPROX. .5000. THE RIGHT AILERON WAS ALSO REMOVED AND TWO OF THESE LEADING EDGE WEIGHT…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Air conditioning and pressurization · controller · misoverhauledJul 30, 1996

    ACFT CLLIMBED TO FL 260. CREW NOTICED A DISCREPANCY IN THE CABIN PRESSURE DIFFERENTIAL, ALTITUDE AND CONTROLLER INDICATION. AFTER INVESTIGATION AND COMPARISON WITH ANOTHER ACFT, IT WAS FOUND DURING OVERHAUL THE INCORRECT FACE HAD BEEN INSTALLED ON THE RATE CONTROLLER.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · skin · crackedFeb 17, 1996

    AFTER AIRCRAFT WAS STRIPPED FOR PAINT JOB, SKIN CRACK FOUND ON UPPER RIGHT WING SURFACE AT WS 49.0, CRACK MEASURED 3 INCHES 'DIAGONALLY' PASSING THROUGH RIVETS THAT ATTACH FLAP BELLCRANK SUPPORT. ONE-THIRD OF HEAD OF MIDDLE RIVETS SHEARED. CESSNA ENGINEERING SUGGESTS THAT FAILURE IS RESULT OF…

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

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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