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