Airworthiness Directives; Lycoming Engines (Formerly Textron Lycoming), Direct-Drive Reciprocating Engines; Correction

[Federal Register Volume 69, Number 123 (Monday, June 28, 2004)]
[Rules and Regulations]
[Page 36007]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 04-14477]



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Federal Register / Vol. 69, No. 123 / Monday, June 28, 2004 / Rules 
and Regulations

[[Page 36007]]



DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 89-ANE-10-AD; Amendment 39-13644; AD 2004-10-14]
RIN 2120-AA64


Airworthiness Directives; Lycoming Engines (Formerly Textron 
Lycoming), Direct-Drive Reciprocating Engines; Correction

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction.

-----------------------------------------------------------------------

SUMMARY: This document makes corrections to Airworthiness Directive 
(AD) 2004-10-14, applicable to Lycoming Engines (formerly Textron 
Lycoming), direct-drive reciprocating engines that was published in the 
Federal Register on May 21, 2004 (69 FR 29210). Some corrections to 
engine models have been made by adding missing dashes, clarification to 
changes in requirements from the proposed rule are made, and some 
corrections are made for clarification in the compliance section. In 
all other respects, the original document remains the same.

DATES: Effective Date: Effective June 28, 2004.

FOR FURTHER INFORMATION CONTACT: Norm Perenson, Aerospace Engineer, New 
York Aircraft Certification Office, FAA, 1600 Stewart Avenue, Suite 
410, Westbury, NY 11590; telephone (516) 228-7337; fax (516) 794-5531.

SUPPLEMENTARY INFORMATION: A final rule AD, FR Doc. 04-11406, 
applicable to Lycoming Engines direct-drive reciprocating engines 
(except O-145, O-320-H, O-360-E, IO-360-E, LTO-360-E, O-435, and TIO 
541 series engines), was published in the Federal Register on May 21, 
2004 (69 FR 29210). The following corrections are needed:
    On page 29210, in the second column, in the SUMMARY section, in the 
sixth and seventh lines, ``O-320H, O-360E, LO-360E, LTO-360E'' are 
corrected to read ``O-320-H, O-360-E, LO-360-E, LTO-360-E, TO-360-E''.
    In the third column, in the SUMMARY section, in the 14th line, 
after the words ``propeller strike.'', a sentence is added to read 
``This AD removes the requirement to perform inspections at overhaul 
and during repair of the gear train, because Lycoming has incorporated 
those procedures from their Service Bulletin into their Overhaul 
Manual.''
    Also in the third column, in the SUPPLEMENTARY INFORMATION section, 
in the seventh and eighth lines, ``O-320H, O-360E, LO-360E, LTO-360E'' 
is corrected to read ``O-320-H, O-360-E, LO-360-E, LTO-360-E, TO-360-
E''.
    On page 29211, in the second column, after the second paragraph, 
add the following paragraph:

Other Corrections

    The TO-360-E engine model was inadvertently omitted from the list 
of exceptions of engines. That engine model has been added to the list 
of exceptions of engines not affected by this AD. Also, some of the 
engine model numbers were missing dashes and are corrected in this AD. 
Also, the phrase of after the effective date of this AD, was 
inadvertently omitted from paragraph (e). This phrase is added to 
paragraph (e) to cover engines that experience a propeller strike after 
the effective date of the AD.


Sec.  39.13  [Corrected]

0
Also, on page 29211, in the third column, eighth paragraph, fourth and 
fifth lines, ``O-320H, O-360E, LO-360E, LTO-360E'' is corrected to read 
``O-320-H, O-360-E, LO-360-E, LTO-360-E, TO-360-E''.
0
Also, on page 29211, in the third column, paragraph (e), which reads 
``Compliance with this AD is required as indicated before further 
flight if the engine has experienced a propeller strike as defined in 
paragraphs (i) and (j) of this AD, unless already done.'' is corrected 
to read ``Compliance with this AD is required as indicated before 
further flight if the engine experiences a propeller strike after the 
effective date of this AD, as defined in paragraphs (i) and (j) of this 
AD.''.

    Issued in Burlington, MA, on June 18, 2004.
Francis A. Favara,
Acting Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. 04-14477 Filed 6-25-04; 8:45 am]
BILLING CODE 4910-13-P

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