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FAA airworthiness directive publication

AD 2013-10-04

2013-09-05 · Correction notice · Federal Register document 2013-21453

This page records a selected historical publication. Its current legal status, applicability to an individual aircraft and compliance have not been determined. Consult the current FAA directive and aircraft configuration and maintenance records.

This correction remains a separate publication; it is not presented as a newly issued independent directive.

What this historical correction says

Source publication 2013-09-05 · Document 2013-21453.

The notice publishes only a correction fragment. The summary or discussion below is not a complete applicability clause or a complete model list.

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.

Original date wording

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.

Dates describing the correction and the original rule remain separate as written.

Original summary or discussion context

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.

Literal source labels for discovery: PA-31, PA-31-325, PA-31-350. Labels remain as written; series, aliases and engine suffixes are not expanded.

Dated original publication

  • AD 2013-10-04 · 2013-06-12 · document 2013-13666
    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.
    
    

Each link opens a separate dated source. These words and dates do not determine which directive controls today, aircraft applicability, installed configuration or compliance. No corrected rule body has been merged.

Historical relationship observation unknown

This correction notice is a separate source edition and was not interpreted as a new rule. This does not establish that there are no related or currently applicable directives.

Earlier extraction record

The earlier extraction kept these fields unknown. Its original record is preserved below. Newly retained correction excerpts are shown above; applicability and compliance remain undetermined.

Applicability text in this publication

An applicability clause was not extracted from this publication. Applicability remains undetermined.

Effective-date text

An effective-date observation was not extracted from this publication.

Publication context

A relationship to prior directives has not been established from this publication.

Official sources

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Sources retrieved: HTML 2026-09-08; PDF 2026-09-08.

The displayed text comes from the HTML publication. Refer to the official documents for the original wording.

This selected source edition is not a complete list of current airworthiness directives. Referenced manufacturer service documents are not reproduced here.

Related sources

Explore all recorded source editions of this AD identifier · Find selected publications with this AD number. Matching numbers are discovery links; source identity, current legal status and aircraft applicability remain separate.

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