Airworthiness Directives; Airbus Model A318, A319, A320, and A321 Series Airplanes, 78883 [C1-2010-27614]

Download as PDF Federal Register / Vol. 75, No. 242 / Friday, December 17, 2010 / Rules and Regulations 1, dated October 14, 2010, to perform the BSIs for engines listed in paragraph(c)(1) of this AD. (k) Use paragraphs 3.A through 3.H of the Accomplishment Instructions of Pratt & Whitney SB No. PW4G–100–72–226, dated April 22, 2010, to perform the BSIs for engines listed in paragraphs(c)(2) and (c)(3) of this AD. Optional Terminating Action (l) As optional terminating action to the repetitive inspection requirements of this AD, install new 9th stage compressor stator segments, part number (P/N) 50S479–01, P/N 50S479–02, P/N 50S479–03, and P/N 50S479–04, and perform one of the following: (1) At the time the new 9th stage compressor stator segments are installed, replace the HPC drum rotor disk assembly with a new, 0 cycle, HPC drum rotor disk assembly; or (2) At the time the new 9th stage compressor stator segments are installed, replace the 10th stage HPC disk with a new, 0 cycle, 10th stage HPC disk; or (3) Perform a one-time BSI or FPI for cracks in the AVT shelf slots on the 10th stage HPC disk of the HPC drum rotor disk assembly between 4,000 and 7,200 cycles-in-service since installation of the new 9th stage compressor stator segments. (i) If a crack is found, remove the HPC drum rotor disk assembly from service. (ii) If no crack is found, then no further inspections are required. (4) Guidance on installation of the new 9th stage compressor stator segments can be found in Pratt & Whitney SB No. PW4ENG 72–801, Revision 1, dated September 8, 2010, for engines listed in paragraph(c)(1) of this AD and in Pratt & Whitney SB No. PW4G– 100–72–225 dated April 20, 2010, for engines listed in paragraphs(c)(2) and (c)(3) of this AD. Alternative Methods of Compliance (AMOCs) (m) The Manager, Engine Certification Office, has the authority to approve AMOCs for this AD if requested using the procedures found in 14 CFR 39.19. srobinson on DSKHWCL6B1PROD with RULES Related Information (n) Contact James Gray, Aerospace Engineer, Engine Certification Office, FAA, Engine and Propeller Directorate, 12 New England Executive Park, Burlington, MA 01803; e-mail: james.e.gray@faa.gov; telephone (781) 238–7742; fax (781) 238– 7199, for more information about this AD. Material Incorporated by Reference (o) You must use Pratt & Whitney Service Bulletin (SB) No. PW4G–100–72–226, dated April 22, 2010, and Pratt & Whitney SB No. PW4ENG 72–799, Revision 1, dated October 14, 2010, to perform the borescope inspections required by this AD. The Director of the Federal Register approved the incorporation by reference of these documents in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Contact Pratt & Whitney, 400 Main St., East Hartford, CT 06108; telephone (860) 565–8770; fax (860) 565–4503, for a copy of this service VerDate Mar<15>2010 19:53 Dec 16, 2010 Jkt 223001 78883 information. You may review copies at the FAA, New England Region, 12 New England Executive Park, Burlington, MA; 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/cfr/ibrlocations.html. DEPARTMENT OF COMMERCE Issued in Burlington, Massachusetts, on November 17, 2010. Peter A. White, Assistant Manager, Engine and Propeller Directorate, Aircraft Certification Service. Implementation of Additional Changes From the Annual Review of the Entity List [FR Doc. 2010–31723 Filed 12–16–10; 8:45 am] Bureau of Industry and Security 15 CFR Part 744 [Docket No. 101102553–0553–01] RIN 0694–AF01 Bureau of Industry and Security, Commerce. ACTION: Final rule. AGENCY: BILLING CODE 4910–13–P This rule amends the Export Administration Regulations (EAR) to implement additional changes to the Entity List (Supplement No. 4 to Part 744) on the basis of the annual review of the Entity List conducted by the EndUser Review Committee (ERC). The changes from the annual review will be implemented in three rules. The first rule published on May 28, 2010 (75 FR 29884) implemented the results of the annual review for listed entities located in Canada, Egypt, Germany, Hong Kong, Israel, Kuwait, Lebanon, Malaysia, South Korea, Singapore, and the United Kingdom. The second rule, published today, implements the results of the annual review for entities located in China and Russia. This rule removes five entities from the Entity List under Russia and makes twenty-one modifications to the Entity List (consisting of modifications to eighteen Chinese entries and three Russian entries currently on the Entity List) by adding additional addresses, aliases and/or clarifying the names for these twenty-one entities. The third rule, which will likely be published in early 2011, will implement the remaining results of the annual review. The Entity List provides notice to the public that certain exports, reexports, and transfers (in-country) to entities identified on the Entity List require a license from the Bureau of Industry and Security and that availability of license exceptions in such transactions is limited. SUMMARY: DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2010–0279; Directorate Identifier 2009–NM–148–AD; Amendment 39–16496; AD 2010–23–07] RIN 2120–AA64 Airworthiness Directives; Airbus Model A318, A319, A320, and A321 Series Airplanes Correction In rule document 2010–27614 beginning on page 68181 in the issue of Friday, November 5, 2010, make the following corrections: § 39.13 [Corrected] 1. On page 68183, in § 39.13(c), in the second column, in the first column of the table, in the 30th entry, ‘‘D554 71000 000 00’’, should read ‘‘D554 71001 000 00’’. 2. On the same page, in the same section, in the third column, in the second column of the table, in the 19th entry, ‘‘TS–Z072’’, should read ‘‘TS– 2072’’. 3. On page 68184, in the same section, in the first column, in the first column of the table, in the 12th entry, ‘‘D554 11002 000 00 003’’ should read ‘‘D554 71002 000 00 0003’’. 4. On the same page, in the same section, in the same column, in the same column of the table, in the 14th entry, ‘‘D554 11004 000 00 0000’’ should read ‘‘D554 71004 000 00 0000’’. [FR Doc. C1–2010–27614 Filed 12–16–10; 8:45 am] BILLING CODE 1505–01–D PO 00000 Frm 00007 Fmt 4700 Sfmt 4700 Effective Date: This rule is effective December 17, 2010. Although there is no formal comment period, public comments on this regulation are welcome on a continuing basis. ADDRESSES: You may submit comments, identified by RIN 0694–AF01, by any of the following methods: E-mail: publiccomments@bis.doc.gov. Include ‘‘RIN 0694–AF01’’ in the subject line of the message. DATES: E:\FR\FM\17DER1.SGM 17DER1

Agencies

[Federal Register Volume 75, Number 242 (Friday, December 17, 2010)]
[Rules and Regulations]
[Page 78883]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: C1-2010-27614]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2010-0279; Directorate Identifier 2009-NM-148-AD; 
Amendment 39-16496; AD 2010-23-07]
RIN 2120-AA64


Airworthiness Directives; Airbus Model A318, A319, A320, and A321 
Series Airplanes

Correction

    In rule document 2010-27614 beginning on page 68181 in the issue of 
Friday, November 5, 2010, make the following corrections:


Sec.  39.13  [Corrected]

    1. On page 68183, in Sec.  39.13(c), in the second column, in the 
first column of the table, in the 30th entry, ``D554 71000 000 00'', 
should read ``D554 71001 000 00''.
    2. On the same page, in the same section, in the third column, in 
the second column of the table, in the 19th entry, ``TS-Z072'', should 
read ``TS-2072''.
    3. On page 68184, in the same section, in the first column, in the 
first column of the table, in the 12th entry, ``D554 11002 000 00 003'' 
should read ``D554 71002 000 00 0003''.
    4. On the same page, in the same section, in the same column, in 
the same column of the table, in the 14th entry, ``D554 11004 000 00 
0000'' should read ``D554 71004 000 00 0000''.

[FR Doc. C1-2010-27614 Filed 12-16-10; 8:45 am]
BILLING CODE 1505-01-D