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Aircraft record

N6117R1979 Cessna 172RG

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Sep 17, 2013.

Safety record in brief:1 NTSB accident (substantial damage, Aug 2009)4 ADs may apply8 service difficulty reports

Registration
Deregistered
Last based in
Paramus, NJ
owner city / state
Owners
1
since 2002
NTSB events
1
substantial, 2009
ADs may apply
4
confirm with A&P
Service reports
8
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Genesus One INC
Owner type
Corporation
City, state
Paramus, NJ
Certificate issued
Nov 21, 2002
Canceled
Sep 17, 2013
Airworthiness
Standard · Normal
Airworthiness date
Nov 9, 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
172RG
Year
1979
Serial number
172RG0087
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
A7F5D2

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. 2002 – 2013Genesus One INCParamus, NJ
  2. 1971 – 1972Amtex INCCleveland, TN · different airframe: Cessna T210f S/N T210-0017

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 (1)

Accident · substantial damage

Aug 25, 2009 · Rockaway, NJ

A total loss of engine power due to oil starvation for undetermined reasons.

Damage
Substantial
Injuries
Minor
Report
ERA09LA481

From NTSB records; matched by serial number.Read NTSB report (search CAROL for ERA09LA481)

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 (8)

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 · corrodedOct 29, 1999

    BULKHEAD, PN 2412007-2, FROM STA 75.33 TO STA 90.00. THE CORRODED AREA IS BELIEVED TO BE CAUSED BY THE ENGINE EXHAUST PIPE EMISSIONS. SUBMITTER SUGGESTED A LONGER TAILPIPE SO AS TO GET EXHAUST EMISSIONS AWAY FROM BELLY OF AIRCRAFT. INSPECTION OF LIKE MODEL AIRCRAFT REVEALED SIMILAR CORROSION.…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · bulkhead · corrodedOct 29, 1999

    BULKHEAD, PN 2412017-2, FROM STA 90.00 TO STA 108.00. THE CORRODED AREA IS BELIEVED TO BE CAUSED BY THE ENGINE EXHAUST PIPE EMISSIONS. SUBMITTER SUGGESTED A LONGER TAILPIPE SO AS TO GET EXHAUST EMISSIONS AWAY FROM BELLY OF AIRCRAFT. INSPECTION OF LIKE MODEL AIRCRAFT REVEALED SIMILAR CORROSION.…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · bulkhead · corrodedOct 29, 1999

    FORWARD BUMPER ASSEMBLIES PN 2411033-2. THE CORRODED AREA IS BELIEVED TO BE CAUSED BY THE ENGINE EXHAUST PIPE EMISSIONS. SUBMITTER SUGGESTED A LONGER TAILPIPE SO AS TO GET EXHAUST EMISSIONS AWAY FROM BELLY OF AIRCRAFT. INSPECTION OF LIKE MODEL AIRCRAFT REVEALED SIMILAR CORROSION. AIRCRAFT TT…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 8 reports
  • Fuselage · bulkhead · corrodedOct 29, 1999

    BULKHEAD, PN 2411011-1 AND DOUBLER PN 2411013-2 AT STA 75.33. THE CORRODED AREA IS BELIEVED TO BE CAUSED BY THE ENGINE EXHAUST PIPE EMISSIONS. SUBMITTER SUGGESTED A LONGER TAILPIPE SO AS TO GET EXHAUST EMISSIONS AWAY FROM BELLY OF AIRCRAFT. INSPECTION OF LIKE MODEL AIRCRAFT REVEALED SIMILAR…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · tunnel · corrodedOct 29, 1999

    TUNNEL ASSEMBLY PN 12412020-1 AFT OF STA 108.0 AFT UPPER CORNER. THE CORRODED AREA IS BELIEVED TO BE CAUSED BY THE ENGINE EXHAUST PIPE EMISSIONS. SUBMITTER SUGGESTED A LONGER TAILPIPE SO AS TO GET EXHAUST EMISSIONS AWAY FROM BELLY OF AIRCRAFT. INSPECTION OF LIKE MODEL AIRCRAFT REVEALED SIMILAR…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · floorboard · corrodedOct 29, 1999

    FLOORBOARD PN 2412019-1 FROM STA 90.00 TO STA 108.00. THE CORRODED AREA IS BELIEVED TO BE CAUSED BY THE ENGINE EXHAUST PIPE EMISSIONS. SUBMITTER SUGGESTED A LONGER TAILIPE SO AS TO GET EXHAUST EMISSIONS AWAY FROM BELLY OF AIRCRAFT. INSPECTION OF LIKE MODEL AIRCRAFT REVEALED SIMILAR CORROSION.…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · bulkhead · corrodedOct 29, 1999

    BULKHEAD, PN 2411010-5 FROM STA 65.33 TO STA 90.0. THE CORRODED AREA IS BELIEVED TO BE CAUSED BY THE ENGINE EXHAUST PIPE EMISSIONS. SUBMITTER SUGGESTED A LONGER TAILIPE SO AS TO GET EXHAUST EMISSIONS AWAY FROM BELLY OF AIRCRAFT. INSPECTION OF LIKE MODEL AIRCRAFT REVEALED SIMILAR CORROSION.…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · cover · corrodedOct 29, 1999

    RIGHT HAND COVER ASSEMBLY PN 2412016-2 AT STA 108. THE CORRODED AREA IS BELIEVED TO BE CAUSED BY THE ENGINE EXHAUST PIPE EMISSIONS. SUBMITTER SUGGESTED A LONGER TAILIPE SO AS TO GET EXHAUST EMISSIONS AWAY FROM BELLY OF AIRCRAFT. INSPECTION OF LIKE MODEL AIRCRAFT REVEALED SIMILAR CORROSION.…

    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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