[Federal Register Volume 60, Number 115 (Thursday, June 15, 1995)]
[Rules and Regulations]
[Pages 31387-31388]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 95-14629]
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DEPARTMENT OF TRANSPORTATION
14 CFR Part 39
[Docket No. 95-NM-96-AD; Amendment 39-9246; AD 95-11-13]
Airworthiness Directives; McDonnell Douglas Model MD-11 Series
Airplanes Equipped With Pratt & Whitney Model PW4460 and PW4462 Engines
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule; correction.
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SUMMARY: This document corrects a typographical error that appeared in
paragraph (c) of the above-captioned airworthiness directive (AD) that
was published in the Federal Register June 1, 1995 (60 FR 28527). A
typographical error in paragraph (c) of the AD resulted in a reference
to a part number that is inaccurate.
[[Page 31388]] DATES: Effective June 16, 1995.
The incorporation by reference of certain publications listed in
the regulations was previously approved by the Director of the Federal
Register as of June 16, 1995 (60 FR 28527, June 1, 1993).
FOR FURTHER INFORMATION CONTACT: Wahib Mina, Aerospace Engineer,
Airframe Branch, ANM-120L, FAA, Los Angeles Aircraft Certification
Office, 3960 Paramount Boulevard, Lakewood, California 90712; telephone
(310) 627-5324; fax (310) 627-5210.
SUPPLEMENTARY INFORMATION: Airworthiness Directive (AD) 95-11-13,
amendment 39-9246, applicable to certain McDonnell Douglas Model MD-11
series airplanes, was published as a final rule in the Federal Register
on June 1, 1995 (60 FR 28527). As published, that final rule contained
a typographical error in paragraph (c). Paragraph (c) indicated that no
person shall install an aft mount beam assembly, part number (P/N) 221-
021-501. However, the correct P/N is 221-0261-501, which is cited
correctly throughout the rest of the final rule.
This document corrects the reference to the P/N cited in the
paragraph (c) of AD 95-11-13, to read as follows:
``(c) As of the effective date of this AD, no person shall install
an aft mount beam assembly, P/N 221-0261-501, on any airplane, unless
it has been previously inspected and re-identified in accordance with
the paragraph 3.B., Phase 2, of the Accomplishment Instructions of
McDonnell Douglas Alert Service Bulletin MD11-71A073, Revision 1, dated
May 16, 1995.''
Since no other part of the regulatory information has been changed,
the final rule is not being republished.
Issued in Renton, Washington, on June 9, 1995.
Darrell M. Pederson,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 95-14629 Filed 6-14-95; 8:45 am]
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