# Flight and navigation instruments.
**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.
**FOR FURTHER INFORMATION CONTACT:**
Terry Pearsall, phone (202) 267-3042.
**SUPPLEMENTARY INFORMATION:**
**Need for Correction**
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 29 is corrected by making the following correcting amendments:
**List of Subjects in 14 CFR Part 29, Subpart F**
Equipment.
**14 CFR Part 29**
Accordingly, 14 CFR part 29 is corrected by making the following correcting amendments:
**PART 29—AIRWORTHINESS STANDARDS: TRANSPORT CATEGORY ROTORCRAFT**
1. The authority citation for part 29 continues to read as follows:
**Authority:**
49 U.S.C. 106(g), 40113, 44701-44702, 44704.
2. Revise paragraphs (g) introductory text, (g)(1) and (g)(4) of § 29.1303 to read as follows:
§ 29.1303
(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.