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Public Record · As of May 5, 2026

N3095X

Ayres Corporation S2R-T34 · 1991 View Type →

Status

Registration Valid

Type

Fixed Wing Single Engine

Engine

P&W CANADA PT6A-60A

Last Cert Issue

—

Aircraft Resources

Engine · Pratt & Whitney Canada → Search FAA TCDS for AYRES CORPORATION S2R-T34 →

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 N3095X.

Tail Number

N3095X

Serial Number

T34-174

Make

AYRES CORPORATION

Model

S2R-T34

Year of Manufacture

1991

Mfr / Model Code

0970106

Type Aircraft

Fixed Wing Single Engine

Type Engine

Turbo-prop

Engines

1

Seats

1

Engine Manufacturer

P&W CANADA

Engine Model

PT6A-60A

Horsepower

1050 hp

Weight Class

CLASS 1

Certification

Restricted (+1 flag) · code 31

Registrant

MORRIS EQUIPMENT LLC · LLC

Address

340 W 32ND ST # 413 · YUMA, AZ 85364-8128

FAA Region

4 · County 027

Status

Registration Valid

Airworthiness Date

—

Cert Issue Date

—

Expiration Date

—

Last FAA Action

—

Mode S Hex (ICAO24)

A343DE

Mode S (Octal)

50641736

Live position via ICAO24 A343DE

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02 /  NTSB Records

Events on file with the National Transportation Safety Board

03 /  Airworthiness Directives

Applicable to AYRES CORPORATION S2R-T34

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

  • Jan 20, 2010

    Airworthiness Directives; Thrush Aircraft, Inc. Model 600 S2D and S2R Series Airplanes

    We are adopting a new airworthiness directive (AD) to supersede AD (AD) 2006-07-15, which applies to Thrush Aircraft, Inc. Model 600 S2D and S2R (S-2R) series airplanes (type certificate previously held by Quality Aerospace, Inc. and Ayres Corporation). AD 2006-07-15 currently requires repetitive inspections of the 1/4-inch and 5/16-inch bolt hole areas on…

    Federal Register →

  • May 4, 2009

    Airworthiness Directives; Thrush Aircraft, Inc. (Type Certificate Previously Held by Quality Aerospace, Inc. and Ayres Corporation) Model 600 S2D and S2R (S-2R) Series Airplanes

    We propose to supersede Airworthiness Directive (AD) 2006-07- 15, which applies to Thrush Aircraft, Inc. Model 600 S2D and S2R (S-2R) series airplanes (type certificate previously held by Quality Aerospace, Inc. and Ayres Corporation). AD 2006-07-15 currently requires repetitive inspections of the \1/4\-inch and \5/16\-inch bolt hole areas on the wing front…

    Federal Register →

  • Apr 4, 2006

    Airworthiness Directives; Thrush Aircraft, Inc. Model 600 S2D and S2R (S-2R) Series Airplanes

    The FAA is adopting a new airworthiness directive (AD) to supersede AD 2003-07-01, which applies to certain Thrush Aircraft, Inc. Model 600 S2D and S2R (S-2R) series airplanes (type certificate previously held by Quality Aerospace, Inc. and Ayres Corporation). AD 2003-07-01 currently requires you to repetitively inspect the \1/4\- inch and \5/16\-inch bolt…

    Federal Register →

  • Apr 1, 2003

    Airworthiness Directives; Quality Aerospace, Inc. S2R Series and Model 600 S2D Airplanes

    This amendment supersedes Airworthiness Directive (AD) 2000- 11-16, which currently applies to certain Quality Aerospace, Inc. (Quality Aerospace) (formerly Ayres Corporation) S2R series and Model 600 S2D airplanes. AD 2000-11-16 requires you to repetitively inspect the \1/4\-inch and \5/16\-inch bolt hole areas on the lower spar caps for fatigue cracking;…

    Federal Register →

  • Nov 8, 2002

    Airworthiness Directives; Quality Aerospace, Inc., S2R Series and Model 600 S2D Airplanes

    This document proposes to supersede Airworthiness Directive (AD) 2000-11-16, which currently applies to certain Quality Aerospace, Inc. (Quality Aerospace) (formerly Ayres Corporation) S2R series and Model 600 S2D airplanes. AD 2000-11-16 requires you to repetitively inspect the \1/4\-inch and \5/16\-inch bolt hole areas on the lower spar caps for fatigue c…

    Federal Register →

  • Jun 7, 2000

    Airworthiness Directives; Ayres Corporation S2R Series and Model 600 S2D Airplanes

    This amendment supersedes Airworthiness Directive (AD) 97-17- 03, which currently requires you to accomplish the following on Ayres Corporation (Ayres) S2R Series and Model 600 S2D airplanes: inspect the \1/4\-inch and \5/16\-inch bolt hole areas on the lower spar caps for fatigue cracking; replace any lower spar cap where fatigue cracking is found; and rep…

    Federal Register →

  • Feb 16, 2000

    Airworthiness Directives; Ayres Corporation S2R Series and Model 600 S2D Airplanes

    This document proposes to revise an earlier proposed airworthiness directive (AD) that the Federal Aviation Administration (FAA) issued against Ayres Corporation (Ayres) S2R series and Model 600 S2D airplanes. The earlier proposed rule would supersede the existing AD with a new AD that would require you to repetitively inspect the \1/ 4\-inch and \5/16\-inc…

    Federal Register →

  • Nov 24, 1999

    Airworthiness Directives; Ayres Corporation S2R Series Airplanes

    This document proposes to adopt a new airworthiness directive (AD) that would apply to all Ayres Corporation (Ayres) S2R series airplanes that are equipped with at least one main landing gear fuselage attach bolt with a grease fitting installed through the shank. The proposed AD would require replacing the main landing gear fuselage attach bolts that are dr…

    Federal Register →

  • Jan 13, 1999

    Airworthiness Directives; Ayres Corporation S2R Series and Model 600 S2D Airplanes

    This document proposes to supersede Airworthiness Directive (AD) 97-17-03, which currently requires inspecting the \1/4\-inch and \5/16\-inch bolt hole areas on the lower spar caps for fatigue cracking on Ayres S2R series and Model 600 S2D airplanes, and replacing any lower spar cap where fatigue cracking is found. That AD resulted from an accident on an Ay…

    Federal Register →

  • Aug 18, 1997

    Airworthiness Directives; Ayres Corporation S2R Series Airplanes

    This amendment supersedes Airworthiness Directive (AD) 97-13- 11, which currently requires inspecting the \1/4\-inch and \5/16\-inch bolt hole areas on the lower spar caps for fatigue cracking on Ayres S2R series airplanes, and replacing any lower spar cap if fatigue cracking is found. That AD resulted from an accident on an Ayres S2R series airplane where…

    Federal Register →

  • Jul 10, 1997

    Airworthiness Directives; Ayres Corporation S2R Series Airplanes

    This document publishes in the Federal Register an amendment adopting Airworthiness Directive (AD) 97-13-11, which was sent previously to known U.S. owners and operators of certain Ayres Corporation (Ayres) S2R series airplanes. This AD requires inspecting the \1/4\-inch and \5/16\-inch bolt hole areas on the lower spar caps for fatigue cracking, and replac…

    Federal Register →

  • Apr 26, 1996

    Airworthiness Directives; Hartzell Propeller Inc. HC-A3V, HC-B3M, HC-B3T, HC-B4M, HC-B4T, and HC-B5M Series Propellers

    This document proposes the adoption of a new airworthiness directive (AD) that is applicable to Hartzell Propeller Inc. (Hartzell) HC-A3V, HC-B3M, HC-B3T, HC-B4M, HC- B4T, and HC-B5M series propellers. This proposal would require hub replacement over a 10-year time period with a concurrent blade and blade clamp inspection. This proposal is prompted by repor…

    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.