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Aircraft record

N951CC1979 Cessna 182Q

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:No NTSB accidents or incidents since 19824 ADs may apply4 service difficulty reports

Registration
Valid
expires Apr 30, 2029
Based in
Ridgecrest, CA
owner city / state
Engine
O-470 SERIES · 230 hp
Cont Motor
Owners
1
since 2019
NTSB events
None
since 1982
ADs may apply
4
confirm with A&P
Service reports
4
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Co-owners
City, state
Ridgecrest, CA
Certificate issued
Apr 15, 2019
Expires
Apr 30, 2029
Airworthiness
Standard · Normal
Airworthiness date
May 7, 1979

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
1979
Serial number
18266998
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
AD3893

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. 2019 – nowCo-ownersRidgecrest, CA · 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 (4)

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.

  • Stabilizers · bracket · crackedJun 13, 2000

    DURING 100-HOUR ANNUAL INSPECTION, THE HORIZONTAL STABILIZER ATTACHMENT POINT REINFORCEMENT ON LEFT SIDE WAS FOUND CRACKED. SUSPECTED CAUSE WAS PART HIGH TIME. ALTHOUGH THE RIGHT REINFORCEMENT WAS NOT CRACKED, IT WAS REPLACED DUE TO HIGH TIME. (X)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Reciprocating engine · cylinder · wornJun 13, 2000

    CYLINDER NR 6 WAS REMOVED BECAUSE THE COMPRESSION WAS 50/80 DUE TO LEAKAGE PAST THE INTAKE VALVE. AFTER INSPECTION OF THE CYLINDER, THE CYLINDER ASSY WAS REPLACED DUE TO A WEAR STEP AT THE TOP OF THE CYLINDER BARREL. (X)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine indicating · line · brokenJun 13, 2000

    MANIFOLD PRESSURE LINE WAS FOUND BROKEN AFTER PILOT REPORTED GAUGE READING AMBIENT PRESSURE. POSSIBLE CAUSE, HIGH PART TOTAL TIME. (X)

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 4 reports
  • Stabilizers · rib · bentJun 13, 2000

    DURING ANNUAL/100 HOUR INSPECTION, THE SECOND RIB OUTBOARD OF CENTER ON THE RT SIDE OF THE HORIZONTAL STABILIZER WAS FOUND BENT THROUGH THE LIGHTENING HOLES. POSSIBLE CAUSE OF THIS DAMAGE, IMPROPER GROUND HANDLING (SITTING ON STABILIZER TO TURN AIRCRAFT). (X)

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

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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