Skip to content
KnownTail
Aircraft record

N9654B1981 Cessna 172RG

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:No NTSB accidents or incidents since 19824 ADs may apply6 service difficulty reports

Registration
Valid
expires May 31, 2032
Based in
Tulsa, OK
owner city / state
Owners
1
since 2025
NTSB events
None
since 1982
ADs may apply
4
confirm with A&P
Service reports
6
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Individual owner
City, state
Tulsa, OK
Certificate issued
May 5, 2025
Expires
May 31, 2032
Airworthiness
Standard · Normal
Airworthiness date
Aug 26, 1981

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
172RG
Year
1981
Serial number
172RG0947
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
AD719F

Engine

Make and model
Lycoming O&Vo-360 Ser
Type
Reciprocating
Power
180 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. 2025 – nowIndividual ownerTulsa, OK · current
  2. until 1957Cessna Aircraft CoWichita, KS · different airframe: Cessna 180a S/N 32951

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
2011-10-09Cessna Aircraft Company Models 150, 152, 170, 172, 175, 177, 180, 182, 185, 188, 190…Jun 17, 2011Airframe (172RG)
2008-10-02Cessna Aircraft Company 172, 175, 180, 182, 185, 206, 207, 208, 210, and 303 Series…May 12, 2008Airframe (172RG)Certain serial numbers: 172S 172S10672–172S10674; 172S 172S10676; 172S 172S10678–172S10680; 172S 172S10682; 172S 172S10683; 172S 172S10685; …. Only with: Applies only to airplanes that have a P/N 2013142-18 alternate static air source selector valve installed after November 19, 2007.
2001-23-03Cessna Aircraft Company Models 172N, 172P, R172K, 172RG, F172N, F172P, FR172J, and…Dec 27, 2001Airframe (172RG)Certain serial numbers: 172N 17267585–17270049; 172N 17270051–17274009; 172N 17261445; 172N 17261578; 172N 17270050; 172P 17274010–17276654; …
2001-06-06Cessna Aircraft Company Model 172RG AirplanesMay 14, 2001Airframe (172RG)Certain serial numbers: 172RG 691; 172RG 172RG0001–172RG1191

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.

  • Fuselage · bulkhead · crackedSep 30, 2004

    CRACKS WERE LOCATED AT LT AND RT RELIEF CUTS OF STATION 124.00 UPPER FUSELAGE BULKHEAD. PROBABLE CAUSE FOR LT SIDE IS AUX POWER RECEPTACLE AND RT SIDE COULD BE FROM LANDING STRESSES.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · actuator · crackedMay 25, 2001

    FOUND ONE ACTUATOR CRACKED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · bulkhead · crackedJun 6, 1999

    PILOT REPORTED RUDDER AND TRIM STIFFNESS. EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 2413001-4, 2413001-5, 2413001-6, CRACKED. THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. SUBMITTER STATED THIS CONDITION FOUND ON SIX OTHER AIRCRAFT.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 6 reports
  • Fuselage · bulkhead · crackedJun 6, 1999

    PILOT REPORTED RUDDER AND TRIM STIFFNESS. EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 2413001-4, 2413001-5, 2413001-6, CRACKED. THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. SUBMITTER STATED THIS CONDITION FOUND ON SIX OTHER AIRCRAFT.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · bulkhead · crackedJun 6, 1999

    PILOT REPORTED RUDDER AND TRIM STIFFNESS. EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 2413001-4, 2413001-5, 2413001-6, CRACKED. THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. SUBMITTER STATED THIS CONDITION FOUND ON SIX OTHER AIRCRAFT.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · bulkhead · crackedJun 6, 1999

    PILOT REPORTED RUDDER AND TRIM STIFFNESS. EXAMINATION FOUND BULKHEADS IN LOWER FORWARD FUSELAGE SECTION, PN 2413001-3, 2413001-4, 2413001-5, 2413001-6, CRACKED. THESE CRACKS ARE BELOW CENTER RUDDER TORQUE TUBE BEARINGS AFT ATTACH POINTS. SUBMITTER STATED THIS CONDITION FOUND ON SIX OTHER AIRCRAFT.

    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

Request owner name removalReport an error in this record