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incorporation by reference of these
documents in accordance with 5 U.S.C.
552(a) and 1 CFR part 51. For copies of the
documents, contact Airbus, 1 Rond Point
Maurice Bellonte, 31707 Blagnac Cedex,
France. You can review copies at the Docket
Management Facility, U.S. Department of
Transportation, 400 Seventh Street, SW.,
room PL–401, Nassif Building, Washington,
DC; or at the National Archives and Records
Administration (NARA). For information on
the availability of this material at NARA, call
(202) 741–6030, or go to http://
www.archives.gov/federal_register/
code_of_federal_regulations/
ibr_locations.html.
Related Information
(k) French airworthiness directive F–2004–
074, dated May 26, 2004, also addresses the
subject of this AD.
Issued in Renton, Washington, on July 16,
2004.
Kalene C. Yanamura,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service
[FR Doc. 04–16914 Filed 7–28–04; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2003–NE–12–AD; Amendment
39–13434; AD 2004–01–20]
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) 2004–01–20, which is 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 was published in the
Federal Register on January 20, 2004
(69 FR 2661). The compliance
information for the RB211–535C engine
was inadvertently omitted from the AD.
Also, under Related Information, the
referenced service bulletin is not the
latest revision. This document adds the
omitted information and corrects the
service bulletin reference. In all other
respects, the original document remains
the same.
EFFECTIVE DATE: Effective January 20,
2004.
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. 04–759, applicable to
RR RB211–22B series, RB211–524B,
–524C2, –524D4, –524G2, –524G3, and
–524H series, and RB211–535C and
–535E series turbofan engines with HPC
stage 3 disc assemblies, P/Ns LK46210,
LK58278, LK67634, LK76036, UL11706,
UL15358, UL22577, UL22578, and
UL24738 installed, was published in the
Federal Register on January 20, 2004
(69 FR 2661). The following corrections
are needed:
§ 39.13 [Corrected]

On page 2663, in the first column, after
paragraph (f)(4), add paragraph (f)(5) to
read:
‘‘(5) Discs in RB211–535C operation
are unaffected by the interim rework
cyclic band limits in Table 1 of this AD,
but must meet the calendar life
requirements of either paragraph (f)(1)
or (f)(2) of this AD, as applicable.’’

On page 2663, in the second column,
in paragraph (j), in the 4th and 5th lines,
change ‘‘RB.211–72–9661, Revision 3,
dated December 20, 1999’’ to ‘‘RB.211–
72–9661, Revision 4, dated January 4,
2002’’.
Issued in Burlington, MA, on July 21, 2004.
Francis A. Favara,
Acting Manager, Engine and Propeller
Directorate, Aircraft Certification Service.
[FR Doc. 04–17283 Filed 7–28–04; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF THE TREASURY
Office of Foreign Assets Control
31 CFR Part 541
Zimbabwe Sanctions Regulations
AGENCY: Office of Foreign Assets
Control, Treasury.
ACTION: Interim final rule.
SUMMARY: The Office of Foreign Assets
Control of the U.S. Department of the
Treasury is adding new regulations to
implement Executive Order 13288 of
　
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