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Public Record · As of May 5, 2026

N203S

Piper PA-23-150 · 1956 View Type →

Status

Registration Valid

Type

Fixed Wing Multi Engine

Engine

LYCOMING 0-320 SERIES

Last Cert Issue

—

Aircraft Resources

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01 /  Registration

Filed with the Federal Aviation Administration

Every cell below is a literal field from the FAA Aircraft Registry. Click any value to open the FAA registry record for N203S.

Tail Number

N203S

Serial Number

23-412

Make

PIPER

Model

PA-23-150

Year of Manufacture

1956

Mfr / Model Code

7102303

Type Aircraft

Fixed Wing Multi Engine

Type Engine

Reciprocating

Engines

2

Seats

5

Engine Manufacturer

LYCOMING

Engine Model

0-320 SERIES

Horsepower

180 hp

Weight Class

CLASS 1

Certification

Standard · code 1

Registrant

JESTICE JOANNA CHRISTY · Individual

Address

621 GRITNEY RD · DALEVILLE, AL 36322-4678

FAA Region

7 · County 045

Status

Registration Valid

Airworthiness Date

—

Cert Issue Date

—

Expiration Date

—

Last FAA Action

—

Mode S Hex (ICAO24)

A19EB8

Mode S (Octal)

50317270

Live position via ICAO24 A19EB8

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02 /  NTSB Records

Events on file with the National Transportation Safety Board

03 /  Airworthiness Directives

Applicable to PIPER PA-23-150

Federal Aviation Administration airworthiness directives matched to make and model. Each entry links to the Federal Register publication.

  • Oct 31, 2022

    Airworthiness Directives; Piper Aircraft, Inc. (Type Certificate Previously Held by The New Piper Aircraft Inc. and Piper Aircraft Corporation) Airplanes

    The FAA is withdrawing a notice of proposed rulemaking (NPRM) and supplemental notice of proposed rulemaking (SNPRM) that proposed to supersede Airworthiness Directive (AD) 92-13-04 for certain Piper Aircraft Corporation (now Piper Aircraft, Inc.) (Piper) Model PA-23-150 (type certificated as PA-23) and PA-23-160 airplanes. AD 92-13-04 requires preflight wa…

    Federal Register →

  • Apr 2, 2007

    Airworthiness Directives; Superior Air Parts, Inc. (SAP), Cylinder Assemblies Part Numbers Series: SA47000L, SA47000S, SA52000, SA55000, SL32000W, SL32000WH, SL32006W, SL36000TW, SL36000W, and SL36006W

    The FAA is revising an existing airworthiness directive (AD) for certain SAP cylinder assemblies installed in Teledyne Continental Motors (TCM) 470, 520, and 550 series reciprocating engines, Lycoming Engines (LE) 320, 360, and 540 series reciprocating engines, Avco Lycoming (AL) 540 series reciprocating engines, and Superior Air Parts, Inc. (SAP) 360 serie…

    Federal Register →

  • Feb 23, 2007

    Airworthiness Directives; Superior Air Parts, Inc. (SAP), Cast Cylinder Assemblies Part Numbers Series: SA47000L, SA47000S, SA52000, SA55000, SL32000W, SL32000WH, SL32006W, SL36000TW, SL36000W, and SL36006W

    The FAA is adopting a new airworthiness directive (AD) for certain SAP cast cylinder assemblies installed in Teledyne Continental Motors (TCM) 470, 520, and 550 series reciprocating engines, Lycoming Engines (LE) 320, 360, and 540 series reciprocating engines, Avco Lycoming (AL) 540 series reciprocating engines, and Superior Air Parts, Inc. (SAP) 360 series…

    Federal Register →

  • Feb 12, 1998

    Airworthiness Directives; The New Piper Aircraft, Inc. (Formerly Piper Aircraft Corporation) Models PA-23 (PA-23-150), PA-23-160, PA-23- 235, and PA-23-250 Airplanes

    This document proposes to revise an earlier proposed airworthiness directive (AD) that would have required installing external fuel ramp assemblies on The New Piper Aircraft, Inc. (Piper) Models PA-23 (PA-23-150), PA-23-160, PA-23-235, and PA-23-250 airplanes, and incorporating pilots' operating handbook (POH) revisions for Piper Models PA-23 (PA-23-150), a…

    Federal Register →

04 /  Service Difficulty Reports

FAA SDR filings

The FAA does not currently expose a public API for Service Difficulty Reports. We do not back-fill or paraphrase. Search the FAA SDR portal directly →

05 /  Sources & Methodology

Every fact on this page links to its primary US-government source

We render only what the agency publishes. Found a factual error? Report it → We acknowledge within 5 business days and resolve within 14.