Skip to content
KnownTail
Aircraft record

N954CC1976 Cessna 182Q

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:No NTSB accidents or incidents since 19824 ADs may apply11 service difficulty reports

Registration
Valid
expires May 31, 2031
Based in
Edina, MN
owner city / state
Engine
O-470 SERIES · 230 hp
Cont Motor
Owners
1
since 2024
NTSB events
None
since 1982
ADs may apply
4
confirm with A&P
Service reports
11
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Individual owner
City, state
Edina, MN
Certificate issued
May 16, 2024
Expires
May 31, 2031
Airworthiness
Standard · Normal
Airworthiness date
Dec 9, 1976

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
182Q
Year
1976
Serial number
18265290
Aircraft type
Fixed wing single engine
Category
Land
Certification
Type Certificated
Seats
4
Engines
1
Max takeoff weight
Up to 12,499 lb
Mode S code
AD43B8

Engine

Make and model
Cont Motor O-470 Series
Type
Reciprocating
Power
230 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. 2024 – nowIndividual ownerEdina, MN · current

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 (4)

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
2025-23-08Hoses and TubesDec 2, 2025Airframe (182Q)Only with: Equipped with an affected part as defined in paragraph (g)(1) of this AD installed in accordance with STC SA03302AT.
2011-10-09Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190…Jun 17, 2011Airframe (182Q)
2009-04-05Cessna Aircraft Company Models 182Q and 182R AirplanesMar 27, 2009Airframe (182Q)Only with: Equipped with SMA diesel engine Model SR305-230-1 (or SR305-230 converted to SR305-230-1 per SMA SB-01-76-002) installed under STC SA03302AT.
2007-09-01Cessna Aircraft Company Models 182H, 182J, 182K, 182L, 182M, 182N, 182P, 182Q, and 182R…Apr 25, 2007Airframe (182Q)Only with: Air Plains Services Corporation STC SA00152WI installed and a ground power receptacle mounted on the firewall (forward ground power receptacle).

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

Service Difficulty Reports (11)

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.

  • Reciprocating engine · cylinder · wornNov 2, 1999

    DURING A ROUTINE 100-HOUR INSPECTION, EXCESSIVE LEAKAGE IS FOUND GOING PAST THE PISTON RINGS ON THE NR 6 CYLINDER. THE TOP TWO PISTON RING GAPS ARE FOUND ALIGNED AND THERE IS A NEGATIVE CHOKE IN THE CYLINDER.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Reciprocating engine · valve guide · wornDec 21, 1998

    DURING A ROUTINE 100-HOUR INSPECTION, THE NR 4 CYLINDER WAS FOUND TO HAVE LEAKAGE PAST THE EXHAUST VALVE. FURTHER INVESTIGATION REVEALED A WORN OUT EXHAUST VALVE GUIDE. REPLACING THE GUIDE AND RE-FACING THE EXHAUST VALVE RESOLVED THE PROBLEM. SUBMITTER SUGGESTED POSSIBLE CAUSE AS DEFECTIVE PARTS…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine fuel and control · oil cooler · crackedSep 29, 1998

    DURING A ROUTINE INSPECTION, A CRACK WAS FOUND ON THE OIL COOLER NEAR THE AFT, LOWER SUPPORT, STRUT ATTACH POINT (WELD). SUBMITTER SUGGESTED POSSIBLE CAUSE AS IMPROPER WELDING DURING MANUFACTURE OR REMANUFACTURE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Reciprocating engine · intake valve · wornAug 14, 1998

    DURING AN INSPECTION REQUIRED BY TCM CSB98-1B, TITLED INTAKE AND EXHAUST VALVE INSPECTION, THE INTAKE VALVE TIPS ON THE NR'S 2, 4, AND 6 CYLINDERS WERE FOUND EXCESSIVELY WORN. SUBMITTER SUGGESTED POSSIBLE CAUSE AS DEFECTIVE PARTS INSTALLED INTO THE ENGINE AT REMANUFACTURE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Reciprocating engine · crankcase · crackedFeb 20, 1998

    DURING A ROUTINE OIL CHANGE, A CRACK WAS FOUND IN THE CRANKCASE THAT RADIATES ABOUT ONE INCH TOWARDS THE CENTER OF THE ENGINE STARTING FROM THE FORWARD UPPER HOLD DOWN STUD ON THE NR 5 CYLINDER. THE ENGINE WAS RETURNED TO THE FACTORY FOR A CRANKCASE REPLACEMENT. SUBMITTER SUGGESTED POSSIBLE CAUSE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Reciprocating engine · lifters · pittedJan 28, 1998

    DURING A ROUTINE COMPRESSION CHECK, THE NR 2 CYLINDER EXHAUST VALVE WAS FOUND LEAKING. AFTER THE CYLINDER WAS REMOVED, ALL CAM LIFTERS FOUND PITTED AND THE NR 5 CYLINDER INTAKE CAM LOBE FOUND SCOURED. THE ENGINE REMOVED FROM SERVICE. SUBMITTER SUGGESTED POSSIBLE CAUSE AS DEFECTIVE PARTS AND/OR…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine fuel and control · carburetor · not markedSep 2, 1997

    CARBURETORS BEING PRODUCED BY PRECISION AIRMOTIVE ARE NOT IN COMPLIANCE WITH MARVEL-SCHEBELER AD 63-22-03. THE LETTER 'V' IS NOT STAMPED UNDER THE SERIAL NUMBER. SUBMITTER STATED REQUIRE PRECISION AIRMOTIVE TO RECTIFY ALL THE CARBURETORS THEY HAVE PRODUCED THIS WAY OR REVISE AD 63-22-03 TO REFLECT…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Reciprocating engine · valve guide · wornMay 20, 1997

    DURING A ROUTINE COMPRESSION CHECK, LEAKAGE WAS FOUND PAST THE EXHAUST VALVE ON THE NR 3 CYLINDER. THE REMOVED CYLINDER, EXHAUST VALVE AND GUIDE WERE FOUND WORN OUT. SUBMITTER SUGGESTED POSSIBLE CAUSE AS DEFECTIVE PARTS AND/OR ASSEMBLY PROCESS FROM THE FACTORY.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Reciprocating engine · camshaft · scoredNov 15, 1996

    A ROUTINE OIL CHANGE AND OIL FILTER INSPECTION REVEALS EXCESSIVE METAL. FURTHER INVESTIGATION FINDS THE CAMSHAFT HAS FAILED ON CERTAIN CAM LOBES. ENGINE IS REMOVED FROM SERVICE. SUBMITTER SUGGESTED POSSIBLE CAUSE AS DEFECTIVE PART.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Reciprocating engine · valve guide · wornSep 7, 1996

    DURING A ROUTINE COMPRESSION CHECK, LEAKAGE WAS FOUND ON THE EXHAUST VALVES ON THE NR 1 AND NR 3 CYLINDERS. THE REMOVED CYLINDERS, EXHAUST VALVES AND GUIDES WERE FOUND WORN OUT. SUBMITTER SUGGESTED POSSIBLE CAUSE AS DEFECTIVE PARTS AND/OR ASSSEMBLY PROCES FROM THE FACTORY.

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

Showing the 10 most recent of 11 reports.

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

Request owner name removalReport an error in this record