N2315V

Valid Registration

PIPER PA-38-112

N2315V is a PIPER PA-38-112 registered to ANYWHERE ATP LLC in MOUNT JULIET, TN. Its FAA registration status is Valid. It has 4 NTSB accident records on file. 1 Airworthiness Directive may apply.

Registration Details

N-Number
N2315V
Serial Number
38-82A0085
Manufacturer
PIPER
Model
PA-38-112
Year
—
Registration Status
Valid
Airworthiness Date
1981-10-22
Owner
ANYWHERE ATP LLC
Owner City
MOUNT JULIET
Owner State
TN

The PIPER PA-38-112 is registered with the FAA under N-number N2315V. Its manufacturer serial number is 38-82A0085. The aircraft was issued its airworthiness certificate on 1981-10-22. The current registered owner is ANYWHERE ATP LLC, based in MOUNT JULIET, TN. Registration data is sourced from the FAA Releasable Aircraft Database and refreshed weekly.

Accident History

No injuries reported1987-05-10

CHANDLER, AZ, USA

Accident — PIPER PA-38-112 (NTSB LAX87LA204)

No injuries reported1985-11-06

CHANDLER, AZ, USA

Accident — PIPER PA-38-112 (NTSB LAX86LA034)

No injuries reported1983-09-20

SAN MARTIN, CA, USA

Accident — PIPER PA 38-112 (NTSB LAX83LA451)

No injuries reported1983-06-18

MORGAN HILL, CA, USA

Accident — PIPER PA-38-112 (NTSB LAX83LA292)

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

N2315V 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

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. N2315V 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 N2315V

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

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