N21662

Valid Registration

2004 CESSNA 172S

N21662 is a 2004 CESSNA 172S registered to SMEDLEY JONATHAN G in LEANDER, TX. Its FAA registration status is Valid. It has 3 NTSB accident records on file. 12 Airworthiness Directives may apply.

Registration Details

N-Number
N21662
Serial Number
172S9647
Manufacturer
CESSNA
Model
172S
Year
2004
Registration Status
Valid
Airworthiness Date
2004-06-01
Owner
SMEDLEY JONATHAN G
Owner City
LEANDER
Owner State
TX

The CESSNA 172S is registered with the FAA under N-number N21662. This airframe was manufactured in 2004. Its manufacturer serial number is 172S9647. The aircraft was issued its airworthiness certificate on 2004-06-01. The current registered owner is SMEDLEY JONATHAN G, based in LEANDER, TX. Registration data is sourced from the FAA Releasable Aircraft Database and refreshed weekly.

Accident History

No injuries reported1996-03-05

VALPARAISO, IN, USA

Accident — Cessna 172 (NTSB CHI96LA103)

No injuries reported1991-07-04

MILLVILLE, OH, USA

Accident — CESSNA 172 (NTSB NYC91LA169)

No injuries reported1983-09-27

KANSAS CITY, MO, USA

Accident — CESSNA 172 (NTSB MKC83LA223)

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

N21662 has been involved in 3 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

12 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. N21662 may be affected by 12 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.

+11 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 N21662

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

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