[Federal Register Volume 61, Number 174 (Friday, September 6, 1996)]
[Rules and Regulations]
[Page 47051]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 96-22773]
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DEPARTMENT OF TRANSPORTATION
14 CFR Part 39
[Docket No. 91-ANE-29; Amendment 39-9470; AD 91-21-01 R1]
RIN 2120-AA64
Airworthiness Directives; Textron Lycoming Model TIO-540-S1AD
Reciprocating Engines
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule; correction.
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SUMMARY: This document makes a correction to Airworthiness Directive
(AD) 91-21-01 R1 applicable to Textron Lycoming Model TIO-540-S1AD
reciprocating engines that was published in the Federal Register on
June 7, 1996 (61 FR 29003). The reference to the New York Aircraft
Certification Office in Note 3 following the paragraph describing the
procedure for obtaining an alternative method of compliance was
omitted. This document corrects that omission. In all other respects,
the original document remains the same.
EFFECTIVE DATE: September 6, 1996.
FOR FURTHER INFORMATION CONTACT: Richard Fiesel, Aerospace Engineer,
New York Aircraft Certification Office, FAA, Engine and Propeller
Directorate, 10 Fifth St., 3rd Floor, Valley Stream, NY 11581-1200;
telephone (516) 256-7504, fax (516) 568-2716.
SUPPLEMENTARY INFORMATION: A final rule airworthiness directive
applicable to Textron Lycoming Model TIO-540-S1AD reciprocating
engines, was published in the Federal Register on June 7, 1996 (61 FR
29003). The following correction is needed:
Sec. 39.13 [Corrected]
On page 29005, in the first column, in the Compliance Section, in
Note 3 of paragraph (c), in the fourth line, ``obtained from.'' is
corrected to read ``obtained from the New York Aircraft Certification
Office''.
Issued in Burlington, MA, on August 28, 1996.
Jay J. Pardee,
Manager, Engine and Propeller Directorate, Aircraft Certification
Service.
[FR Doc. 96-22773 Filed 9-5-96; 8:45 am]
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