N121CW

Valid Registration

2001 CESSNA 172S

N121CW is a 2001 CESSNA 172S registered to AEROSTAR TRAINING SERVICES LLC in KISSIMMEE, FL. Its FAA registration status is Valid. It has 4 NTSB accident records on file. 12 Airworthiness Directives may apply.

Registration Details

N-Number
N121CW
Serial Number
172S8975
Manufacturer
CESSNA
Model
172S
Year
2001
Registration Status
Valid
Airworthiness Date
2001-10-23
Owner
AEROSTAR TRAINING SERVICES LLC
Owner City
KISSIMMEE
Owner State
FL

The CESSNA 172S is registered with the FAA under N-number N121CW. This airframe was manufactured in 2001. Its manufacturer serial number is 172S8975. The aircraft was issued its airworthiness certificate on 2001-10-23. The current registered owner is AEROSTAR TRAINING SERVICES LLC, based in KISSIMMEE, FL. Registration data is sourced from the FAA Releasable Aircraft Database and refreshed weekly.

Accident History

No injuries reported2025-07-30

Kissimmee, FL, USA

Accident — CESSNA 172S (NTSB ERA25LA281)

No injuries reported2013-07-22

New Smyrna Beach, FL, USA

Accident — CESSNA 172S (NTSB ERA13CA335)

No injuries reported2005-09-18

Show Low, AZ, USA

Accident — Cessna 172S (NTSB LAX05CA302)

Fatal injuries1994-08-23

PEKIN, IL, USA

Accident — WATSON KR-2 (NTSB CHI94LA294)

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

N121CW has been involved in 4 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. N121CW 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 N121CW

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

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