Published 2013-09-05 · Federal Register document 2013-21453
Airworthiness Directives; Piper Aircraft, Inc. Airplanes
Publication summary
The FAA is correcting an airworthiness directive (AD) that published in the Federal Register. That AD applies to all Piper Aircraft, Inc. Models PA-31, PA-31-325, and PA-31-350 airplanes. Table 1 of paragraph (g) lists the incorrect model/part number for the Model PA-31-350, tail pipe assembly, top. This document corrects that error. In all other respects, the original document remains the same.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:42.577882+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2013-a7b684f4a1b4614e
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- results[284]
- Raw source SHA-256
- a7b684f4a1b4614eef5ec9064d04a70a4701b45b0acd50058e29f235c625e705
Correction notice · separate source edition
Recorded publication clauses
- AD identifier printed in this edition
- 2013-10-04
- Effective date printed in this edition
- Unknown
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Find all recorded historical references to AD 2013-10-04 · 0 printed reference observations in this pinned collection.
These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.
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They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.
Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: d6c75749b46bbfd607ddc13acfb08ec30b7690e0582f718499eb2d76adbc41cf. Source manifest: 7cc4964014692e8c3ce3e3a79fb11e3bdafbdc9670fd90ebe36b54bb70d3c865.
Official source · 2013-09-05
Publication text
This is the complete recorded text of this dated publication.
Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.
Read the complete official publication text
[Federal Register Volume 78, Number 172 (Thursday, September 5, 2013)]
[Rules and Regulations]
[Page 54561]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2013-21453]
========================================================================
Rules and Regulations
Federal Register
________________________________________________________________________
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Federal Register / Vol. 78, No. 172 / Thursday, September 5, 2013 /
Rules and Regulations
[[Page 54561]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2012-0983; Directorate Identifier 2012-CE-001-AD;
Amendment 39-17457; AD 2013-10-04]
RIN 2120-AA64
Airworthiness Directives; Piper Aircraft, Inc. Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; correction.
-----------------------------------------------------------------------
SUMMARY: The FAA is correcting an airworthiness directive (AD) that
published in the Federal Register. That AD applies to all Piper
Aircraft, Inc. Models PA-31, PA-31-325, and PA-31-350 airplanes. Table
1 of paragraph (g) lists the incorrect model/part number for the Model
PA-31-350, tail pipe assembly, top. This document corrects that error.
In all other respects, the original document remains the same.
DATES: This final rule is effective September 5, 2013. The effective
date for AD 2013-10-04 (78 FR 35110, June 12, 2013) remains July 17,
2013.
ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov; or in person at the Docket Management Facility
between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The AD docket contains this AD, the regulatory evaluation,
any comments received, and other information. The address for the
Docket Office (phone: 800-647-5527) is Document Management Facility,
U.S. Department of Transportation, Docket Operations, M-30, West
Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE.,
Washington, DC 20590.
FOR FURTHER INFORMATION CONTACT: Gary Wechsler, Aerospace Engineer,
Atlanta Aircraft Certification Office, FAA, 1701 Columbia Avenue,
College Park, Georgia 30337; telephone: (404) 474-5575; fax: (404) 474-
5606; email: [email protected].
SUPPLEMENTARY INFORMATION: Airworthiness Directive 2013-10-04 (78 FR
35110, June 12, 2013), currently requires a detailed repetitive
inspection of the exhaust system, expanding the inspection scope to
include the entirety of each airplane exhaust system, and repair or
replacement of parts as necessary for all Piper Aircraft, Inc. Models
PA-31, PA-31-325, and PA-31-350 airplanes.
As published, the part number for the tail pipe assembly, top;
under the Model PA-31-350; in Table 1 of paragraph (g) is incorrect.
No other part of the preamble or regulatory information has been
changed; therefore, only the changed portion of the final rule is being
published in the Federal Register.
The effective date of this AD remains July 17, 2013.
Correction of Regulatory Text
Sec. 39.13 [Corrected]
In the Federal Register of June 12, 2013, AD 2013-10-04; Amendment
39-17457 is corrected as follows:
On page 35114, we are revising Table 1 of paragraph (g)--Recurring
60-hour Inspections for Lycoming and Piper Exhaust System Parts, for
the entry ``tail pipe assembly, top'' in the third sub-column of column
3, Model/part number, remove ``40319-10'' and add ``40310-10'' in its
place.
Issued in Kansas City, Missouri, on August 28, 2013.
Earl Lawrence,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 2013-21453 Filed 9-4-13; 8:45 am]
BILLING CODE 4910-13-P
Why this text is shown
The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-09-08T07:46:28.321171+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.
Open the captured official edition
- Source SHA-256
- 167fac4d3ac9ae5a8e829714ed4f3701864526430f57e644249566f31a617a5b
- Text SHA-256
- d6c75749b46bbfd607ddc13acfb08ec30b7690e0582f718499eb2d76adbc41cf
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Coverage and limits
These are dated publication metadata, recorded clauses and literal source observations. Word, model-label, header and reference matches do not establish current legal effect, manufacturer/model identity, aircraft applicability, installed configuration or compliance.
The collection uses 33 explicit annual source snapshots. Source captures and operative-text qualifications have separate states. Missing information remains unknown.