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Aircraft record

N488631977 Cessna 152

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Nov 29, 2019.

Safety record in brief:3 NTSB events (substantial damage at worst, latest Oct 2007)3 ADs may apply1 service difficulty report

Registration
Deregistered
Last based in
Grand Junction, CO
owner city / state
Owners
1
since 2016
NTSB events
3
substantial, 2007
ADs may apply
3
confirm with A&P
Service reports
1
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Individual owner
City, state
Grand Junction, CO
Certificate issued
Aug 22, 2016
Canceled
Nov 29, 2019
Airworthiness
Standard · Utility
Airworthiness date
Dec 29, 1977

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
152
Year
1977
Serial number
15281011
Aircraft type
Fixed wing single engine
Category
Land
Certification
Type Certificated
Seats
2
Engines
1
Max takeoff weight
Up to 12,499 lb
Mode S code
A60997

Engine

Make and model
Lycoming 0-235 Series
Type
4 Cycle
Power
115 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. 2016 – 2019Individual ownerGrand Junction, CO
  2. 1946 – 1948Individual ownerTucson, AZ · different airframe: Fairchild M-62a S/N T41-802

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 (3)

Accident · substantial damage

Oct 19, 2007 · O'Neill, NE

The pilot's failure to assure the oil filter was installed on the airplane which resulted in oil starvation. Factors associated with the accident were the mechanic not installing the oil filter, the low altitude at which the loss of engine power occurred, and the fence which the airplane contacted.

Damage
Substantial
Injuries
None
Report
CHI08CA025

From NTSB records; matched by serial number.Read NTSB report (search CAROL for CHI08CA025)

Incident · minor damage

Nov 12, 1997 · Blaine, MN

the fracture of the flap cable as a result of fatigue cracking.

Damage
Minor
Injuries
None
Report
CHI98IA035

From NTSB records; matched by serial number.Read NTSB report (search CAROL for CHI98IA035)

Accident · substantial damage

Jan 17, 1993 · Minneapolis, MN

FAILURE OF THE PILOT TO MAINTAIN DIRECTIONAL CONTROL DURING A TAKEOFF GROUND RUN.

Damage
Substantial
Injuries
None
Report
CHI93LA072

From NTSB records; matched by serial number.Read NTSB report (search CAROL for CHI93LA072)

Accident history for this model

ADs published since 1998 that may apply (3)

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
2009-10-09 R2Rudder Control SystemSep 12, 2011Airframe (152)Certain serial numbers: 150F 15061533–15064532; 150G 15064533–15064969; 150G 15064971–15067198; 150H 15067199–15069308; 150H 649; 150J 15069309–15071128; …. Only with: FA150L S/N FA1500121-FA1500261 and FA150M S/N FA1500262-FA1500336 only when equipped with FKA150-2311 and FKA150-2316.
2011-10-09Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190…Jun 17, 2011Airframe (152)
2008-22-18Cessna Aircraft Company 150 Series AirplanesDec 9, 2008Airframe (152)Only with: BRS-150 Parachute System with serial number 50001 through 50006 installed via STC SA64CH.

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

Service Difficulty Reports (1)

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 · control cable · failedNov 12, 1997

    DURING STALL RECOVERY WORK, THE FLAPS WERE BEING MOVED TO A 20 DEGREE POSITION WHEN THE LEFT FLAP RETRACTED TO FULL UP TRAIL POSITION AND RIGHT FLAP REMAINED DOWN (THIS OCCURRED AFTER A LOUD BANG). THE ACFT ROLLED LEFT. PILOT INITIATED EMERGENCY PROCEDURES AND LANDED PLANE. LEFT FLAP CABLE BROKE…

    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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