Published 2009-06-25 · Federal Register document E9-14810
Airworthiness Directives; Pratt & Whitney (PW) JT9D-7 Series Turbofan Engines; Correction
Publication summary
The FAA is correcting airworthiness directive (AD) 2009-04-18, which was previously published in the Federal Register. That AD applies to PW models JT9D-7, -7A, -7AH, -7H, -7F, and -7J turbofan engines. The two references to the engine manual in paragraph (h) and in Table 1, are incomplete. This document corrects those references. In all other respects, the original document remains the same.
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Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:30.011257+00:00. The title, summary and date are source facts.
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- federal_register_ad_metadata_2009-cb57e588bd107238
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- cb57e588bd10723805ef0ea28ddc0685de14711012023c7e7d12178879efaeed
Correction notice · separate source edition
Recorded publication clauses
- AD identifier printed in this edition
- 2009-04-18
- Effective date printed in this edition
- Unknown
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Official source · 2009-06-25
Publication text
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Read the complete official publication text
[Federal Register Volume 74, Number 121 (Thursday, June 25, 2009)]
[Rules and Regulations]
[Page 30211]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: E9-14810]
========================================================================
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Federal Register
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Federal Register / Vol. 74, No. 121 / Thursday, June 25, 2009 / Rules
and Regulations
[[Page 30211]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2008-0759; Directorate Identifier 2008-NE-02-AD;
Amendment 39-15824; AD 2009-04-18]
RIN 2120-AA64
Airworthiness Directives; Pratt & Whitney (PW) JT9D-7 Series
Turbofan Engines; Correction
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule; correction.
-----------------------------------------------------------------------
SUMMARY: The FAA is correcting airworthiness directive (AD) 2009-04-18,
which was previously published in the Federal Register. That AD applies
to PW models JT9D-7, -7A, -7AH, -7H, -7F, and -7J turbofan engines. The
two references to the engine manual in paragraph (h) and in Table 1,
are incomplete. This document corrects those references. In all other
respects, the original document remains the same.
DATES: Effective Date: Effective June 25, 2009.
FOR FURTHER INFORMATION CONTACT: Kevin Dickert, Aerospace Engineer,
Engine Certification Office, FAA, Engine and Propeller Directorate, 12
New England Executive Park, Burlington, MA 01803; e-mail:
[email protected]; telephone (781) 238-7117; fax (781) 238-7199,
for more information about this AD.
SUPPLEMENTARY INFORMATION: On March 31, 2009 (74 FR 14458), we
published a final rule AD, FR Doc, E9-6749, in the Federal Register.
That AD applies to PW models JT9D-7, -7A, -7AH, -7H, -7F, and -7J
turbofan engines. We need to make the following corrections:
Sec. 39.13 [Corrected]
0
On page 14459, in Table 1, in the first column, in the second line,
``770408'' is corrected to read ``770408, Section 72-51-00, Assembly-
02''.
0
On page 14459, in the third column, in paragraph (h), in the third
line, ``1.B.(32) of the JT9D-7 Engine Manual'' is corrected to read
``1.B.(32) of Section 72-51-00, Assembly-02 of the JT9D-7 Engine
Manual''.
Issued in Burlington, Massachusetts, on June 17, 2009.
Carlos Pestana,
Acting Manager, Engine and Propeller Directorate, Aircraft
Certification Service.
[FR Doc. E9-14810 Filed 6-24-09; 8:45 am]
BILLING CODE 4910-13-P
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