N2351A

Valid Registration

1978 PIPER PA-38-112

N2351A is a 1978 PIPER PA-38-112 registered to CHAPMAN THOMAS N in HARVARD, IL. Its FAA registration status is Valid. It has 2 NTSB accident records on file. 1 Airworthiness Directive may apply.

Registration Details

N-Number
N2351A
Serial Number
38-78A0649
Manufacturer
PIPER
Model
PA-38-112
Year
1978
Registration Status
Valid
Airworthiness Date
1978-09-08
Owner
CHAPMAN THOMAS N
Owner City
HARVARD
Owner State
IL

The PIPER PA-38-112 is registered with the FAA under N-number N2351A. This airframe was manufactured in 1978. Its manufacturer serial number is 38-78A0649. The aircraft was issued its airworthiness certificate on 1978-09-08. The current registered owner is CHAPMAN THOMAS N, based in HARVARD, IL. Registration data is sourced from the FAA Releasable Aircraft Database and refreshed weekly.

Accident History

No injuries reported2023-08-10

Harvard, IL, USA

Accident — PIPER PA-38-112 (NTSB CEN23LA362)

Fatal injuries1995-09-15

NEW SMYRNA BCH, FL, USA

Accident — PIPER PA-38-112 (NTSB MIA95FA224)

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

N2351A 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

1 found
AD 98-2776Effective: 1998-02-11

Airworthiness Directives; The New Piper Aircraft Corporation Model PA-38-112 Airplanes

This amendment adopts a new airworthiness directive (AD) that applies to The New Piper Aircraft Corporation (Piper) Model PA-38-112 airplanes. This action requires repetitively replacing the upper rudder hinge bracket. Reports of fatigue cracks occurring on the upper rudder hinge bracket, and the manufacture of a new upper rudder hinge bracket with a life limited improved design prompted this action. The actions specified by this AD are intended to prevent cracks in the upper rudder hinge bracket, which could result in separation of the rudder from the airplane and loss of control of the airplane.

Airworthiness Directives (ADs) are FAA-mandated safety directives that apply to specific aircraft, engines, or components. N2351A may be affected by 1 directive. 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.

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Get the complete history for N2351A

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

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