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Statement of Ronald Ridenour

Piper PA-25 Pawnee · Airworthiness Directives

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Overview

This document is a statement supporting the comments from the Soaring Society of America regarding a proposed Airworthiness Directive (AD) for the Piper PA-25 Pawnee. The statement is authored by Ronald Ridenour, an experienced A&P mechanic and pilot, who has worked extensively on the PA-25. The document discusses the implications of the proposed AD, particularly concerning maintenance practices and the identification of corrosion in the aircraft. Ridenour provides insights based on his long-term experience with the PA-25, emphasizing the importance of proper inspections and the potential challenges posed by the proposed regulations.

  • The proposed AD for the Piper PA-25 Pawnee addresses corrosion issues that could affect safety.
  • Ronald Ridenour has over 47 years of experience with the PA-25, providing him with significant insight into its maintenance.
  • Corrosion has been identified in several PA-25 aircraft, necessitating thorough inspections.
  • The hourly labor rates for aircraft technicians in the Chicago area range from $120 to $245.
  • Ridenour recommends using a 3 mm borescope for better inspection of critical components.

Document

Source

Originally published by www.ssa.org. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
Airworthiness Directives
Year
2025
Pages
3
File size
229 KB
Publisher
www.ssa.org
How rare is it?
1Piper PA-25 Pawnee registered worldwide · 0 active

Common. Rarer than 24% of the aircraft models we track.

Documentation completeness
4/7

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In this document

Background on Proposed AD

The document references a proposed Airworthiness Directive (Docket No. FAA–2025–3990) aimed at addressing safety concerns related to the Piper PA-25 Pawnee. The proposed AD is based on findings of corrosion in several aircraft, which could compromise safety if not addressed.

Author's Qualifications

Ronald Ridenour outlines his extensive qualifications, including his degree in aeronautical engineering, A&P mechanic certification, and experience as a pilot and designated pilot examiner. His background lends credibility to his comments on the proposed AD.

Corrosion Findings

Ridenour discusses specific instances of corrosion found in PA-25 aircraft, referencing photographs from South American crash investigations. He highlights the importance of identifying corrosion during inspections to prevent accidents.

Concerns with Proposed AD

The statement expresses concerns regarding the difficulties and costs associated with implementing the proposed AD. Ridenour agrees with the SSA Comment Letter's assessment of the potential risks and expenses involved.

Inspection Recommendations

Ridenour advocates for the use of a 3 mm borescope for inspecting critical areas of the PA-25, suggesting that this method is more effective and less invasive than the procedures outlined in the proposed AD.

Safety notes

  • Corrosion can compromise the structural integrity of the aircraft and must be addressed promptly during inspections.

Full document text

Statement of Ronald Ridenour 1. I submit this Statement in support of the letter from the Soaring Society of America of December 22, 2025 (the “SSA Comment Letter”). That letter provides comments on a proposed Piper PA-25 Airworthiness Directive identified as follows (the “Proposed AD”): Docket No. FAA–2025–3990; Project Identifier MCAI–2025–00097–A Document Citation: 90 FR 51610 Document Number: 2025-200-84 Publication Date: 11/18/2025 RIN 2120–AA64 2. I am a graduate of Purdue University, where I was awarded a degree in aeronautical and astronautical engineer. Since 1978I have been a licensed Airframe and Powerplant Mechanic, No. 1985138 with Inspection Authorization. I also hold pilot ratings in airplanes and gliders, including flight instructor (airplane and glider), and ATP. I also hold type ratings for several Boeing transport aircraft, and other turbine powered aircraft. I served as a pilot and line check airman for United Airlines prior to retiring in 2017. Since 1975 I have served as a Designated Pilot Examiner for the FAA for ratings for airplanes and gliders. For 18 years I owned and operated a glider flight school in the Chicago area. 3. I have for many years regularly perform maintenance and repair work on airplanes and gliders, including the Piper Pawnee PA-25 that has been owned by the Chicago Glider since 1991. I have done so for 47 years. I also sometime serve as a tow pilot, flying the Piper Pawnee in glider tow operations at the Chicago Glider Club, which is located in Minooka, Illinois. I am currently the President of the Chicago Glider Club. 4. Among other maintenance and repair work on the PA-25, in 2021 I assisted Donald Kroesch in replacing the ceconite fabric on the wing covers on the Chicago Glider Club’s PA-25, 2 and did the pre-recover inspection of the wings before the new fabric was installed. I am very familiar with the structure of the Piper PA-25 Pawnee wing, and other areas of the aircraft. 5. As an A&P with inspection authorization, I have done hundreds of annual and 100- hour inspections on airplanes and gliders. I am well acquainted with the risk of corrosion in aircraft. I review for corrosion as part of such inspections that I conduct. I know what corrosion looks like and have found it on occasion in aircraft that I have inspected. 6. I have reviewed the photos of three South American PA-25 crashes included in the SSA Comment Letter as Figures 1-3. Each shows visible evidence of corrosion that should have resulted in grounding the aircraft and repairing or replacing corroded components. Figure 1 shows visible corrosion in discoloration located on the interior to the spar flange. Figure 2 shows visible corrosion on the left portion of the spar, which is brown in color and obviously corroded. Figure 3 shows visible corrosion as evidenced by the brown color of the metal. 7. I have read the SSA Comment Letter and agree with in its comments concerning the difficulties and expenses that would result from implementing the Proposed AD. I have also read Donald Kroesch’s Statement in support of the SSA Comment Letter. I agree with his description of the difficulties, costs and risks of damage to the wing spar from implementation of the Proposed AD. 8. I believe the hourly labor estimates for implementing the Proposed AD as contained in the SSA Comment letter are fair and reasonable. 9. I am acquainted with hourly labor rates for aircraft technician in the Chicago area. They range from $120 to $245 per hour. 10. I also agree with the SSA Comment Letter that the use of a 3 mm borescope to inspect the front spar and its connection to the leading-edge sheet metal is a far better, less