Airworthiness Directives; Rolls-Royce plc RB211 Series Turbofan Engines; Correction, 58254 [E6-16235]

Download as PDF 58254 Federal Register / Vol. 71, No. 191 / Tuesday, October 3, 2006 / Rules and Regulations Done in Washington, DC, this 28th day of September 2006. W. Ron DeHaven, Administrator, Animal and Plant Health Inspection Service. [FR Doc. E6–16299 Filed 10–2–06; 8:45 am] BILLING CODE 3410–34–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003–NE–12–AD; Amendment 39–14609; AD 2006–11–05] RIN 2120–AA64 § 39.13 [Corrected] On page 29587, in the first column of Table 1, in the second row, in the third line, ‘‘–524B–02, B–B–02, B3–02, and B4 series, Pre SB No. 72–7730’’ is corrected to read ‘‘–524B–02, B–B–02, B3–02, and B4 series, Pre and Post accomplishment of SB No. 72–7730’’. Issued in Burlington, Massachusetts, on September 26, 2006. Peter A. White, Acting Manager, Engine and Propeller Directorate, Aircraft Certification Service. [FR Doc. E6–16235 Filed 10–2–06; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Airworthiness Directives; Rolls-Royce plc RB211 Series Turbofan Engines; Correction Federal Aviation Administration Federal Aviation Administration, DOT. ACTION: Final rule; correction. [Docket No. 30516; Amdt. No. 3187] 14 CFR Part 97 AGENCY: This document makes a correction to Airworthiness Directive (AD) 2006–11–05 applicable to RollsRoyce plc (RR) RB211–22B series, RB211–524B, –524C2, –524D4, –524G2, –524G3, and –524H series, and RB211– 535C and –535E series turbofan engines with high pressure compressor (HPC) stage 3 disc assemblies, part numbers (P/Ns) LK46210, LK58278, LK67634, LK76036, UL11706, UL15358, UL22577, UL22578, and UL24738 installed. That AD published in the Federal Register on May 23, 2006 (71 FR 29586). The ‘‘–524B–02, B–B–02, B3–02, and B4 series, Pre SB No. 72–7730’’ in the Regulatory section is incorrect. This document corrects that requirement. In all other respects, the original document remains the same. DATES: Effective Date: October 3, 2006. FOR FURTHER INFORMATION CONTACT: Ian Dargin, Aerospace Engineer, Engine Certification Office, FAA, Engine and Propeller Directorate, 12 New England Executive Park, Burlington, MA 01803; telephone (781) 238–7178; fax (781) 238–7199. SUPPLEMENTARY INFORMATION: A final rule AD FR Doc, 06–4713 applicable to RR RB211–22B series, RB211–524B, –524C2, –524D4, –524G2, –524G3, and –524H series, and RB211–535C and –535E series turbofan engines with high pressure compressor (HPC) stage 3 disc assemblies, part numbers (P/Ns) LK46210, LK58278, LK67634, LK76036, UL11706, UL15358, UL22577, UL22578, and UL24738 installed, was published in the Federal Register on May 23, 2006 (71 FR 29586). The following correction is needed: mstockstill on PROD1PC61 with RULES SUMMARY: VerDate Aug<31>2005 14:44 Oct 02, 2006 Jkt 211001 Standard Instrument Approach Procedures; Miscellaneous Amendments Federal Aviation Administration (FAA), DOT. ACTION: Final rule. AGENCY: SUMMARY: This amendment amends Standard Instrument Approach Procedures (SIAPs) for operations at certain airports. These regulatory actions are needed because of changes occurring in the National Airspace System, such as the commissioning of new navigational facilities, addition of new obstacles, or changes in air traffic requirements. These changes are designed to provide safe and efficient use of the navigable airspace and to promote safe flight operations under instrument flight rules at the affected airports. This rule is effective October 3, 2006. The compliance date for each SIAP is specified in the amendatory provisions. The incorporation by reference of certain publications listed in the regulations is approved by the Director of the Federal Register as of October 3, 2006. ADDRESSES: Availability of matter incorporated by reference in the amendment is as follows: For Examination— 1. FAA Rules Docket, FAA Headquarters Building, 800 Independence Ave., SW., Washington, DC 20591; 2. The FAA Regional Office of the region in which affected airport is located; or DATES: PO 00000 Frm 00012 Fmt 4700 Sfmt 4700 3. The National Flight Procedures Office, 6500 South MacArthur Blvd., Oklahoma City, OK 73169 or, 4. The National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202–741–6030, or go to: https://www.archives.gov/ federal_register/ code_of_federal_regulations/ ibr_locations.html. For Purchase—Individual SIAP copies may be obtained from: 1. FAA Public Inquiry Center (APA– 200), FAA Headquarters Building, 800 Independence Avenue, SW., Washington, DC 20591; or 2. The FAA Regional Office of the region in which the affected airport is located. By Subscription—Copies of all SIAPs, mailed once every 2 weeks, are for sale by the Superintendent of Documents, U.S. Government Printing Office, Washington, DC 20402. FOR FURTHER INFORMATION CONTACT: Donald P. Pate, Flight Procedure Standards Branch (AFS–420), Flight Technologies and Programs Division, Flight Standards Service, Federal Aviation Administration, Mike Monroney Aeronautical Center, 6500 South MacArthur Blvd., Oklahoma City, OK 73169 (mail address: P.O. Box 25082 Oklahoma City, OK 73125); telephone: (405) 954–4164. SUPPLEMENTARY INFORMATION: This amendment to Title 14, Code of Federal Regulations, part 97 (14 CFR part 97) amends Standard Instrument Approach Procedures (SIAPs). The complete regulatory description of each SIAP is contained in the appropriate FAA Form 8260, as modified by the the National Flight Data Center (FDC)/Permanent Notice to Airmen (P–NOTAM), which is incorporated by reference in the amendment under 5 U.S.C. 552(a), 1 CFR part 51, and § 97.20 of the Code of Federal Regulations. Materials incorporated by reference are available for examination or purchase as stated above. The large number of SIAPs, their complex nature, and the need for a special format make their verbatim publication in the Federal Register expensive and impractical. Further, airmen do not use the regulatory text of the SIAPs, but refer to their graphic depiction on charts printed by publishers of aeronautical materials. Thus, the advantages of incorporation by reference are realized and publication of the complete description of each SIAP contained in FAA form documents is unnecessary. The provisions of this amendment state the E:\FR\FM\03OCR1.SGM 03OCR1

Agencies

[Federal Register Volume 71, Number 191 (Tuesday, October 3, 2006)]
[Rules and Regulations]
[Page 58254]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E6-16235]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 2003-NE-12-AD; Amendment 39-14609; AD 2006-11-05]
RIN 2120-AA64


Airworthiness Directives; Rolls-Royce plc RB211 Series Turbofan 
Engines; Correction

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction.

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SUMMARY: This document makes a correction to Airworthiness Directive 
(AD) 2006-11-05 applicable to Rolls-Royce plc (RR) RB211-22B series, 
RB211-524B, -524C2, -524D4, -524G2, -524G3, and -524H series, and 
RB211-535C and -535E series turbofan engines with high pressure 
compressor (HPC) stage 3 disc assemblies, part numbers (P/Ns) LK46210, 
LK58278, LK67634, LK76036, UL11706, UL15358, UL22577, UL22578, and 
UL24738 installed. That AD published in the Federal Register on May 23, 
2006 (71 FR 29586). The ``-524B-02, B-B-02, B3-02, and B4 series, Pre 
SB No. 72-7730'' in the Regulatory section is incorrect. This document 
corrects that requirement. In all other respects, the original document 
remains the same.

DATES: Effective Date: October 3, 2006.

FOR FURTHER INFORMATION CONTACT: Ian Dargin, Aerospace Engineer, Engine 
Certification Office, FAA, Engine and Propeller Directorate, 12 New 
England Executive Park, Burlington, MA 01803; telephone (781) 238-7178; 
fax (781) 238-7199.

SUPPLEMENTARY INFORMATION: A final rule AD FR Doc, 06-4713 applicable 
to RR RB211-22B series, RB211-524B, -524C2, -524D4, -524G2, -524G3, and 
-524H series, and RB211-535C and -535E series turbofan engines with 
high pressure compressor (HPC) stage 3 disc assemblies, part numbers 
(P/Ns) LK46210, LK58278, LK67634, LK76036, UL11706, UL15358, UL22577, 
UL22578, and UL24738 installed, was published in the Federal Register 
on May 23, 2006 (71 FR 29586). The following correction is needed:


Sec.  39.13  [Corrected]

    On page 29587, in the first column of Table 1, in the second row, 
in the third line, ``-524B-02, B-B-02, B3-02, and B4 series, Pre SB No. 
72-7730'' is corrected to read ``-524B-02, B-B-02, B3-02, and B4 
series, Pre and Post accomplishment of SB No. 72-7730''.

    Issued in Burlington, Massachusetts, on September 26, 2006.
Peter A. White,
Acting Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
 [FR Doc. E6-16235 Filed 10-2-06; 8:45 am]
BILLING CODE 4910-13-P