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.