Enhanced Airworthiness Program for Airplane Systems/Fuel Tank Safety (EAPAS/FTS); Technical Correction, 47818 [E8-18859]

Download as PDF 47818 Federal Register / Vol. 73, No. 159 / Friday, August 15, 2008 / Rules and Regulations Authority: 12 U.S.C. 4001–4010, 12 U.S.C. 5001–5018. 2. The Fourth District routing symbol list in appendix A is revised to read as follows: I Appendix A to Part 229—Routing Number Guide to Next-Day Availability Checks and Local Checks * * * * * Fourth Federal Reserve District [Federal Reserve Bank of Cleveland] Head Office 0220 2220 0223 2223 0410 2410 0412 2412 0420 2420 0421 2421 0422 2422 0423 2423 0430 2430 0432 2432 0433 2433 0434 2434 0440 2440 0441 2441 0442 2442 0515 2515 0519 2519 0720 2720 0724 2724 0740 2740 0749 2749 0813 2813 0830 2830 0839 2839 0863 2863 * * * SUPPLEMENTARY INFORMATION: Background On November 8, 2007, the FAA published a final rule to establish part 26 in the Code of Federal Regulations (72 FR 63364). The heading for subpart B of that part contained the phrase ‘‘aging systems’’ instead of the intended ‘‘airplane systems.’’ This final rule corrects that error. Justification for Immediate Adoption Because this action corrects merely a typographical error, the FAA finds that notice and public comment under 5 U.S.C. 553(b) is unnecessary. For the same reason, the FAA finds that good cause exists under 5 U.S.C. 553(d) for making this rule effective upon publication. List of Subjects in 14 CFR Part 26 * * By order of the Board of Governors of the Federal Reserve System, acting through the Secretary of the Board under delegated authority, August 11, 2008. Robert deV. Frierson, Deputy Secretary of the Board. [FR Doc. E8–18850 Filed 8–14–08; 8:45 am] BILLING CODE 6210–01–P DEPARTMENT OF TRANSPORTATION 14 CFR Part 26 [Docket No. FAA–2004–18379; Amendment No. 26–0] PART 26—CONTINUED AIRWORTHINESS AND SAFETY IMPROVEMENTS FOR TRANSPORT CATEGORY AIRPLANES 1. The authority citation for part 26 continues to read as follows: I Subpart B—Enhanced Airworthiness Program for Airplane Systems 2. The heading for subpart B is revised to read as set forth above. I RIN 2120–AI31 sroberts on PROD1PC70 with PROPOSALS Aircraft, Aviation safety, Continued airworthiness. I In consideration of the foregoing, the Federal Aviation Administration amends Chapter I of Title 14, Code of Federal Regulations part 26 as follows: Authority: 49 U.S.C. 106(g), 40113, 44701, 44702 and 44704. Federal Aviation Administration Enhanced Airworthiness Program for Airplane Systems/Fuel Tank Safety (EAPAS/FTS); Technical Correction Federal Aviation Administration (FAA), DOT. ACTION: Final rule; technical correction. AGENCY: VerDate Aug<31>2005 SUMMARY: This final rule corrects a subpart heading in the Code of Federal Regulations. The heading was inadvertently misstated when the FAA published the rule in November 2007. EFFECTIVE DATE: This final rule is effective August 15, 2008. FOR FURTHER INFORMATION CONTACT: Annette K. Kovite, ANM–113, Standardization Branch, Federal Aviation Administration, 1601 Lind Avenue, SW., Renton, WA 98057, telephone: 425–227–1262, facsimile: 425–227–1320, e-mail: Annette.Kovite@faa.gov. 17:44 Aug 14, 2008 Jkt 214001 Issued in Washington, DC, on August 11, 2008. Pamela Hamilton-Powell, Director, Office of Rulemaking, Aviation Safety. [FR Doc. E8–18859 Filed 8–14–08; 8:45 am] BILLING CODE 4910–13–P PO 00000 Frm 00002 Fmt 4700 Sfmt 4700 DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2008–0864; Directorate Identifier 2008–NM–120–AD; Amendment 39–15644; AD 2008–17–06] RIN 2120–AA64 Airworthiness Directives; Bombardier Model DHC–8–400 Series Airplanes Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule; request for comments. AGENCY: SUMMARY: The FAA is superseding an existing airworthiness directive (AD) that applies to certain Bombardier Model DHC–8–400 series airplanes. The existing AD currently requires revising the Limitations section of the airplane flight manual (AFM) to include procedures for pulling the ‘‘HYD PWR XFER’’ circuit breaker in the event of the loss of all hydraulic fluid in the No. 1 or No. 2 hydraulic system. This AD requires a revision to the AFM to include additional procedures for ensuring that the ‘‘PTU CNTRL’’ switch is Normal, the ‘‘PTU CNTRL ON’’ advisory light is out, and the ‘‘HYD PWR XFER’’ circuit breaker is pulled in the event of the illumination of the ‘‘#2 HYD ISO VALVE’’ caution light. This AD resulted from low No. 2 hydraulic pressure in-flight, which caused the power transfer unit to overspeed, and the fluid flow within the No. 1 hydraulic system to increase. We are issuing this AD to prevent possible loss of both the No. 1 and No. 2 hydraulic systems, resulting in the potential loss of several functions essential for safe flight and landing of the airplane. DATES: This AD becomes effective September 2, 2008. The Director of the Federal Register approved the incorporation by reference of certain publications listed in the AD as of September 2, 2008. On July 10, 2007 (72 FR 30968, June 5, 2007), the Director of the Federal Register approved the incorporation by reference of certain other publications. We must receive any comments on this AD by September 15, 2008. ADDRESSES: You may send comments by any of the following methods: • Federal eRulemaking Portal: Go to https://www.regulations.gov. Follow the instructions for submitting comments. • Fax: 202–493–2251. • Mail: U.S. Department of Transportation, Docket Operations, M– E:\FR\FM\15AUR1.SGM 15AUR1

Agencies

[Federal Register Volume 73, Number 159 (Friday, August 15, 2008)]
[Rules and Regulations]
[Page 47818]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E8-18859]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 26

[Docket No. FAA-2004-18379; Amendment No. 26-0]
RIN 2120-AI31


Enhanced Airworthiness Program for Airplane Systems/Fuel Tank 
Safety (EAPAS/FTS); Technical Correction

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; technical correction.

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SUMMARY: This final rule corrects a subpart heading in the Code of 
Federal Regulations. The heading was inadvertently misstated when the 
FAA published the rule in November 2007.

EFFECTIVE DATE: This final rule is effective August 15, 2008.

FOR FURTHER INFORMATION CONTACT: Annette K. Kovite, ANM-113, 
Standardization Branch, Federal Aviation Administration, 1601 Lind 
Avenue, SW., Renton, WA 98057, telephone: 425-227-1262, facsimile: 425-
227-1320, e-mail: Annette.Kovite@faa.gov.

SUPPLEMENTARY INFORMATION:

Background

    On November 8, 2007, the FAA published a final rule to establish 
part 26 in the Code of Federal Regulations (72 FR 63364). The heading 
for subpart B of that part contained the phrase ``aging systems'' 
instead of the intended ``airplane systems.'' This final rule corrects 
that error.

Justification for Immediate Adoption

    Because this action corrects merely a typographical error, the FAA 
finds that notice and public comment under 5 U.S.C. 553(b) is 
unnecessary. For the same reason, the FAA finds that good cause exists 
under 5 U.S.C. 553(d) for making this rule effective upon publication.

List of Subjects in 14 CFR Part 26

    Aircraft, Aviation safety, Continued airworthiness.

0
In consideration of the foregoing, the Federal Aviation Administration 
amends Chapter I of Title 14, Code of Federal Regulations part 26 as 
follows:

PART 26--CONTINUED AIRWORTHINESS AND SAFETY IMPROVEMENTS FOR 
TRANSPORT CATEGORY AIRPLANES

0
1. The authority citation for part 26 continues to read as follows:

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

Subpart B--Enhanced Airworthiness Program for Airplane Systems

0
2. The heading for subpart B is revised to read as set forth above.

    Issued in Washington, DC, on August 11, 2008.
Pamela Hamilton-Powell,
Director, Office of Rulemaking, Aviation Safety.
[FR Doc. E8-18859 Filed 8-14-08; 8:45 am]
BILLING CODE 4910-13-P

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