AD 2024-25883
Published 2024-11-07 · 18 models · 12,499 US-registered tails affected · Federal Register
Airworthiness Directives; Piper Aircraft, Inc. Airplanes Federal Register ↗
Abstract
This document announces an extension of the comment period for the referenced NPRM, which proposed to supersede Airworthiness Directive (AD) 2020-26-16, which applies to certain Piper Aircraft, Inc. (Piper) Model PA-28-151, PA-28-161, PA-28-181, PA-28-235, PA-28R- 180, PA-28R-200, PA-28R-201, PA-28R-201T, PA-28RT-201, PA-28RT-201T, PA-32-260, PA-32-300, PA-32R-300, PA-32RT-300, and PA-32RT-300T airplanes. This NPRM invited comments concerning the proposed requirements for calculating the calculated service hours (CSH) to determine the times for required actions for each main wing spar; repetitively inspecting the lower main wing spar bolt holes for crack(s) and non-crack damage and taking corrective actions as needed; and replacing or modifying main wing spars at a specified time. This NPRM also invited comments concerning the proposal to revise the applicability by removing certain airplanes and adding a new airplane model. This extension of the comment period is necessary to provide all interested persons an opportunity to present their views on the proposed requirements of this NPRM.
Applicability · by US fleet size
- PIPER PA-28-181 TCDS 2A13 3,535 tails
- PIPER PA-28-161 TCDS 2A13 1,525 tails
- PIPER PA-28R-200 TCDS 2A13 1,223 tails
- PIPER PA-32-300 TCDS A3SO 993 tails
- PIPER PA-28-151 TCDS 2A13 961 tails
- PIPER PA-28-235 TCDS 2A13 859 tails
- PIPER PA-32-260 TCDS A3SO 650 tails
- PIPER PA-28R-180 TCDS 2A13 535 tails
- PIPER PA-32R-300 TCDS A3SO 510 tails
- PIPER PA-28R-201T TCDS 2A13 368 tails
- PIPER PA-28R-201 TCDS 2A13 352 tails
- PIPER PA-28RT-201T TCDS 2A13 255 tails
- PIPER PA-32RT-300T TCDS A3SO 205 tails
- PIPER PA-32RT-300 TCDS A3SO 201 tails
- PIPER PA-28RT-201 TCDS 2A13 179 tails
- PIPER PA-28 TCDS 2A13 117 tails
- NEW PIPER PA-28-181 TCDS 2A13 16 tails
- NEW PIPER PA-28-161 TCDS 2A13 15 tails
Federal Register text
Verbatim; the Federal Register publication is the legally binding document. Cite: 89 FR 88173. View on Federal Register ↗
[Federal Register Volume 89, Number 216 (Thursday, November 7, 2024)] [Proposed Rules] [Pages 88173-88174] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc No: 2024-25883]
======================================================================== Proposed Rules Federal Register ________________________________________________________________________ This section of the FEDERAL REGISTER contains notices to the public of the proposed issuance of rules and regulations. The purpose of these notices is to give interested persons an opportunity to participate in the rule making prior to the adoption of the final rules. ========================================================================
Federal Register / Vol. 89, No. 216 / Thursday, November 7, 2024 / Proposed Rules
[[Page 88173]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2024-2142; Project Identifier AD-2024-00033-A] RIN 2120-AA64
Airworthiness Directives; Piper Aircraft, Inc. Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM); extension of comment period.
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SUMMARY: This document announces an extension of the comment period for the referenced NPRM, which proposed to supersede Airworthiness Directive (AD) 2020-26-16, which applies to certain Piper Aircraft, Inc. (Piper) Model PA-28-151, PA-28-161, PA-28-181, PA-28-235, PA-28R- 180, PA-28R-200, PA-28R-201, PA-28R-201T, PA-28RT-201, PA-28RT-201T, PA-32-260, PA-32-300, PA-32R-300, PA-32RT-300, and PA-32RT-300T airplanes. This NPRM invited comments concerning the proposed requirements for calculating the calculated service hours (CSH) to determine the times for required actions for each main wing spar; repetitively inspecting the lower main wing spar bolt holes for crack(s) and non-crack damage and taking corrective actions as needed; and replacing or modifying main wing spars at a specified time. This NPRM also invited comments concerning the proposal to revise the applicability by removing certain airplanes and adding a new airplane model. This extension of the comment period is necessary to provide all interested persons an opportunity to present their views on the proposed requirements of this NPRM.
DATES: The comment period for the NPRM published on September 23, 2024, at 89 FR 77457, and scheduled to close on November 7, 2024, is extended until December 9, 2024.
ADDRESSES: You may send comments, using the procedures found in 14 CFR 11.43 and 11.45, by any of the following methods: Federal eRulemaking Portal: Go to regulations.gov. Follow the instructions for submitting comments. Fax: (202) 493-2251. Mail: U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE, Washington, DC 20590. Hand Delivery: Deliver to Mail address above between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2024-2142; or in person at Docket Operations between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this NPRM, any comments received, and other information. The street address for Docket Operations is listed above.
FOR FURTHER INFORMATION CONTACT: Fred Caplan, Aviation Safety Engineer, FAA, 1701 Columbia Avenue, College Park, GA 30337; phone: (404) 474- 5507; email: [email protected].