[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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