N5181A

Valid Registration

2002 CESSNA 172R

N5181A is a 2002 CESSNA 172R registered to SOUTHEASTERN OKLAHOMA STATE UNIVERSITY in DURANT, OK. Its FAA registration status is Valid. It has 2 NTSB accident records on file. 20 Airworthiness Directives may apply.

Registration Details

N-Number
N5181A
Serial Number
17281102
Manufacturer
CESSNA
Model
172R
Year
2002
Registration Status
Valid
Airworthiness Date
2002-03-25
Owner
SOUTHEASTERN OKLAHOMA STATE UNIVERSITY
Owner City
DURANT
Owner State
OK

The CESSNA 172R is registered with the FAA under N-number N5181A. This airframe was manufactured in 2002. Its manufacturer serial number is 17281102. The aircraft was issued its airworthiness certificate on 2002-03-25. The current registered owner is SOUTHEASTERN OKLAHOMA STATE UNIVERSITY, based in DURANT, OK. Registration data is sourced from the FAA Releasable Aircraft Database and refreshed weekly.

Accident History

No injuries reported2025-08-27

Ardmore, OK, USA

Accident — CESSNA 172R (NTSB CEN25LA350)

No injuries reported2007-10-26

Stillwater, OK, USA

Accident — Cessna 172 (NTSB DFW08CA021)

Severity reflects injuries to people involved, not damage to the aircraft. A “no injuries” accident can still involve significant aircraft damage.

N5181A has been involved in 2 NTSB accidents since 1982. Each record above includes the date, location, severity, and NTSB summary. Buyers should review the full accident narratives and verify repairs in the aircraft's logbooks before purchase.

Applicable Airworthiness Directives

20 found
AD E8-1460Effective: 2008-01-31

Airworthiness Directives; Cessna Aircraft Company Models 172R and 172S Airplanes

We are adopting a new airworthiness directive (AD) for certain Cessna Aircraft Company (Cessna) Models 172R and 172S airplanes. This AD requires you to inspect the fuel return line assembly for chafing; replace the fuel return line assembly if chafing is found; and inspect the clearance between the fuel return line assembly and both the right steering tube assembly and the airplane structure, adjusting as necessary. This AD results from reports of chafed fuel return line assemblies, which were caused by the fuel return line assembly rubbing against the right steering tube assembly during full rudder pedal actuation. We are issuing this AD to detect and correct chafing of the fuel return line assembly, which could result in fuel leaking under the floor and fuel vapors entering the cabin. This condition could lead to fire under the floor or in the cabin area.

Airworthiness Directives (ADs) are FAA-mandated safety directives that apply to specific aircraft, engines, or components. N5181A may be affected by 20 directives. All applicable ADs must be complied with for the aircraft to remain legally airworthy. Buyers should verify AD compliance in the aircraft's logbooks before purchase.

+19 more Airworthiness Directives found for this aircraft

Full list, with effective dates and links to the official Federal Register documents, is included in the paid report.

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Get the complete history for N5181A

Full accident narratives, all Airworthiness Directives, ownership chain, and a downloadable PDF.

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