N2183A

Valid Registration

1999 MOONEY M20R

N2183A is a 1999 MOONEY M20R registered to LEE CHRISTOPHER M in PORT JERVIS, NY. Its FAA registration status is Valid. It has 2 NTSB accident records on file. 4 Airworthiness Directives may apply.

Registration Details

N-Number
N2183A
Serial Number
29-0198
Manufacturer
MOONEY
Model
M20R
Year
1999
Registration Status
Valid
Airworthiness Date
1999-10-13
Owner
LEE CHRISTOPHER M
Owner City
PORT JERVIS
Owner State
NY

The MOONEY M20R is registered with the FAA under N-number N2183A. This airframe was manufactured in 1999. Its manufacturer serial number is 29-0198. The aircraft was issued its airworthiness certificate on 1999-10-13. The current registered owner is LEE CHRISTOPHER M, based in PORT JERVIS, NY. Registration data is sourced from the FAA Releasable Aircraft Database and refreshed weekly.

Accident History

No injuries reported1992-09-18

SAN ANTONIO, TX, USA

Accident — FAIRCHILD SA-227-AC (NTSB FTW92LA228)

No injuries reported1983-08-12

PARKER, CO, USA

Accident — PIPER PA-22-135 (NTSB DEN83LA189)

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

N2183A 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

4 found
AD E7-3575Effective: 2007-03-05

Airworthiness Directives; Mooney Airplane Company, Inc., (Mooney) Models M20M and M20R Airplanes

The FAA adopts a new airworthiness directive (AD) for certain Mooney Airplane Company, Inc., Models M20M and M20R airplanes. This AD requires you to remove the upper left and upper right engine mount attaching hardware, cut out and remove the upholstery and insulation between the fuselage tubular frame and the firewall, and replace the upper left and upper right engine mount attaching hardware with the new parts kit. This AD results from failure of the engine mount attaching hardware to maintain torque as a result of firewall insulation and upholstery being compressed between the fuselage tubular frame and the firewall at the upper left and upper right engine mount attach points. We are issuing this AD to prevent the upper right and upper left engine mounting hardware from losing torque, which could result in a reduction in engine mount load carrying capability and could lead to engine mount failure.

Airworthiness Directives (ADs) are FAA-mandated safety directives that apply to specific aircraft, engines, or components. N2183A may be affected by 4 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.

+3 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 N2183A

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

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