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Airworthiness Standards: Transport Category Rotorcraft; Equipment: Flight and Navigation Instruments; Correction

Document Details

Information about this document as published in the Federal Register.

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AGENCY:

Federal Aviation administration (FAA), DOT.

ACTION:

Correcting amendment.

SUMMARY:

This document corrects an error that appears in the Code of Federal Regulations (CFR), title 14, as of January 1, 2004. The regulation relates to attitude-indicating instruments that are required to be installed on transport category rotorcraft.

DATES:

Effective on January 12, 2005.

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FOR FURTHER INFORMATION CONTACT:

Terry Pearsall, phone (202) 267-3042.

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SUPPLEMENTARY INFORMATION:

Need for Correction

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As published in the CFR, these regulations contain errors in which the word “altitude” was incorrectly substituted for the word “attitude”. Accordingly, § 29.1303(g) of 14 CFR part

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List of Subjects in 14 CFR Part 29, Subpart F

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Accordingly,

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PART 29—AIRWORTHINESS STANDARDS: TRANSPORT CATEGORY ROTORCRAFT

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1. The authority citation for part 29 continues to read as follows:

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Authority: 49 U.S.C. 106(g), 40113, 44701-44702, 44704.

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2. Revise paragraphs (g) introductory text, (g)(1) and (g)(4) of § 29.1303 to read as follows:

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Flight and navigation instruments.
* * * * *

(g) A gyroscopic rate-of-turn indicator combined with an integral slip-skid indicator (turn-and-bank indicator) except that only a slip-skid indicator is required on rotorcraft with a third attitude instrument system that—

(1) Is usable through flight attitudes of ± 80 degrees of pitch and ± 120 degrees of roll;

(2) * * *

(3) * * *

(4) Operates independently of any other attitude indicating system;

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Anthony F. Fazio,

Director, Office of Rulemaking.

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[FR Doc. 05-553 Filed 1-11-05; 8:45 am]

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