[Federal Register Volume 61, Number 167 (Tuesday, August 27, 1996)]
[Rules and Regulations]
[Page 43952]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 96-21853]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Parts 27 and 29

[Docket No. 28008; Amdt. 27-33, 29-40]
RIN 2120-AF65


Rotorcraft Regulatory Changes Based on European Joint 
Airworthiness Requirement; Correction

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; correction.

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SUMMARY: This document contains a correction to the final rule 
published in the Federal Register on May 10, 1996 (61 FR 21904). That 
final rule amended the airworthiness standards for normal and transport 
category rotorcraft under parts 27 and 29 of Title 14, Code of Federal 
Regulations (CFR) relating to performance systems, propulsion and 
airframes.

FOR FURTHER INFORMATION CONTACT: Carroll Wright, (817) 222-5120.

Need for Correction

    In the final rule document (FR Doc. 96-11493) published in the 
Federal Register on May 10, 1996, (61 FR 21904), on page 21908, at the 
end of the first column, Item No. 14 is corrected to read as follows:
    14. Section 29.1305 is amended by redesignating existing paragraphs 
(a)(6) through (a)(25) as paragraphs (a)(7) through (a)(26), by adding 
a new paragraph (a)(6), and by changing the words ``paragraph (a)(13)'' 
in the text of redesignated paragraph (a)(13) to read as ``paragraph 
(a)(14)''.


Sec. 29.1305  [Corrected]

    (a) * * *
    (6) An oil pressure indicator for each pressure-lubricated gearbox.
* * * * *
    (13) A tachometer for each engine that, if combined with the 
applicable instrument required by paragraph (a)(14) of this section, 
indicates rotor r.p.m. during autorotation.
* * * * *
    Issued in Washington, DC, on August 22, 1996.
Donald P. Byrne,
Assistant Chief Counsel for Regulations.
[FR Doc. 96-21853 Filed 8-26-96; 8:45 am]
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