Federal Aviation administration (FAA), DOT.
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.
Effective on January 12, 2005.Start Further Info
FOR FURTHER INFORMATION CONTACT:
Terry Pearsall, phone (202) 267-3042.End Further Info End Preamble Start Supplemental Information
Need for CorrectionStart Amendment Part
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 Start Printed Page 201229 is corrected by making the following correcting amendments:End Amendment Part Start List of Subjects
List of Subjects in 14 CFR Part 29, Subpart F
Accordingly, 14 CFR part 29 is corrected by making the following correcting amendments:End Amendment Part Start Part
PART 29—AIRWORTHINESS STANDARDS: TRANSPORT CATEGORY ROTORCRAFTEnd Part Start Amendment Part
1. The authority citation for part 29 continues to read as follows:End Amendment Part Start Amendment Part
2. Revise paragraphs (g) introductory text, (g)(1) and (g)(4) of § 29.1303 to read as follows:End Amendment Part
(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;
Anthony F. Fazio,
Director, Office of Rulemaking.
[FR Doc. 05-553 Filed 1-11-05; 8:45 am]
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