[Federal Register Volume 75, Number 85 (Tuesday, May 4, 2010)] [Rules and Regulations] [Pages 23572-23574] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc No: 2010-9521] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2009-0789; Directorate Identifier 2008-NM-185-AD; Amendment 39-16228; AD 2010-06-04] RIN 2120-AA64 Airworthiness Directives; Airbus Model A300 B2-1C, B2-203, B2K- 3C, B4-103, B4-203, B4-2C Airplanes; Model A310 Series Airplanes; and Model A300 B4-601, B4-603, B4-605R, B4-620, B4-622, and B4-622R Airplanes AGENCY: Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule; correction. ----------------------------------------------------------------------- SUMMARY: The FAA is correcting a typographical error in an existing [[Page 23573]] airworthiness directive (AD) that was published in the Federal Register on March 11, 2010. The error resulted in an imprecise compliance time in a table. This AD applies to certain Airbus Model A300 B2-1C, B2-203, B2K-3C, B4-103, B4-203, B4-2C airplanes; Model A310 series airplanes; and Model A300 B4-601, B4-603, B4-605R, B4-620, B4-622, and B4-622R airplanes. This AD requires repetitive inspections to detect cracks of the pylon side panels (upper section) at rib 8; and corrective actions if necessary. DATES: This correction is effective May 4, 2010. The effective date of AD 2010-06-04 remains April 15, 2010. ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov; or in person at the Docket Management Facility between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this AD, the regulatory evaluation, any comments received, and other information. The address for the Docket Office (telephone 800-647-5527) is the Document Management Facility, U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue, SE., Washington, DC 20590. FOR FURTHER INFORMATION CONTACT: Dan Rodina, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425) 227-2125; fax (425) 227-1149. SUPPLEMENTARY INFORMATION: On March 4, 2010, the FAA issued AD 2010-06- 04, Amendment 39-16228 (75 FR 11428, March 11, 2010), for certain Airbus Model A300 B2-1C, B2-203, B2K-3C, B4-103, B4-203, B4-2C airplanes; Model A310 series airplanes; and Model A300 B4-601, B4-603, B4-605R, B4-620, B4-622, and B4-622R airplanes. The AD requires repetitive inspections to detect cracks of the pylon side panels (upper section) at rib 8; and corrective actions if necessary. As published, Table 1 of this AD contained a typographical error in the second row in the second column. The compliance time of ``>17,500 total flight \1\ '' has been corrected to read ''>17,500 total flight cycles \1\.'' (The word ``cycles'' was omitted in the AD.) No other part of the regulatory information has been changed; therefore, the final rule is not republished in the Federal Register. The effective date of this AD remains April 15, 2010. Sec. 39.13 [Corrected] 0 In the Federal Register of March 11, 2010, on page 11430, in the second row in the second column, Table 1 of AD 2010-06-04 is corrected to read as follows: * * * * * Table 1--Compliance Times for Configuration 1 ---------------------------------------------------------------------------------------------------------------- Whichever occurs later And repeat the That have ---------------------------------------- inspection at For Model-- accumulated-- Inspect before the intervals not to accumulation of-- Or within-- exceed-- ---------------------------------------------------------------------------------------------------------------- A300 B2-1C, B2-203, and B2K-3C <=17,500 total 5,350 total flight 2,500 flight 4,300 flight airplanes. flight cycles \1\. cycles. cycles \2\. cycles. A300 B2-1C, B2-203, and B2K-3C >17,500 total 20,000 total 250 flight cycles 4,300 flight airplanes. flight cycles \1\. flight cycles or \2\. cycles. 40,000 total flight hours, whichever occurs first. A300 B4-103, B4-203, and B4-2C <=18,000 total 5,350 total flight 2,000 flight 4,300 flight airplanes. flight cycles \1\. cycles. cycles \2\. cycles. A300 B4-103, B4-203, and B4-2C >18,000 total 20,000 total 250 flight cycles 4,300 flight airplanes. flight cycles \1\. flight cycles or \2\. cycles. 40,000 total flight hours, whichever occurs first. A300 B4-601, B4-603, B4-605R, B4- <=18,000 total 4,200 total flight 2,000 flight 3,600 flight 620, B4-622, and B4-622R flight cycles \1\. cycles. cycles \2\. cycles. airplanes. A300 B4-601, B4-603, B4-605R, B4- >18,000 total 20,000 total 250 flight cycles 3,600 flight 620, B4-622, and B4-622R flight cycles \1\. flight cycles or \2\. cycles. airplanes. 40,000 total flight hours, whichever occurs first. A310-200 airplanes with GE CF6- <=18,000 total 9,700 total flight 1,500 flight 6,700 flight 80A3 or Pratt & Whitney engines. flight cycles \1\. cycles or 19,400 cycles \2\. cycles or 13,400 total flight flight hours, hours, whichever whichever occurs occurs first. first. A310-200 airplanes with GE CF6- >18,000 total 19,500 total 250 flight cycles 6,700 flight 80A3 or Pratt & Whitney engines. flight cycles \1\. flight cycles or \2\. cycles or 13,400 55,500 total flight hours, flight hours, whichever occurs whichever occurs first. first. A310-200 airplanes with GE CF6- <=18,000 total 7,800 total flight 1,500 flight 5,800 flight 80C2 engines. flight cycles \1\. cycles or 15,600 cycles \2\. cycles or 11,600 total flight flight hours, hours, whichever whichever occurs occurs first. first. A310-200 airplanes with GE CF6- >18,000 total 19,500 total 250 flight cycles 5,800 flight 80C2 engines. flight cycles \1\. flight cycles or \2\. cycles or 11,600 55,500 total flight hours, flight hours, whichever occurs whichever occurs first. first. A310-300 SR \3\ airplanes with <=18,000 total 8,600 total flight 1,500 total flight 6,700 flight Pratt & Whitney JT9D engines. flight cycles \1\. cycles or 24,000 cycles \2\. cycles or 18,700 total flight flight hours, hours, whichever whichever occurs occurs first. first. A310-300 SR \3\ airplanes with >18,000 total 19,500 total 250 flight cycles 6,700 flight Pratt & Whitney JT9D engines. flight cycles \1\. flight cycles or \2\. cycles or 18,700 55,500 total flight hours, flight hours, whichever occurs whichever occurs first. first. A310-300 SR \3\ airplanes with <=18,000 total 7,000 total flight 1,500 flight 5,700 flight GE engines. flight cycles \1\. cycles or 19,600 cycles \2\. cycles or 15,900 total flight flight hours, hours, whichever whichever occurs occurs first. first. [[Page 23574]] A310-300 SR \3\ airplanes with >18,000 total 19,500 total 250 flight cycles 5,700 flight GE engines. flight cycles \1\. flight cycles or \2\. cycles or 15,900 55,500 total flight hours, flight hours, whichever occurs whichever occurs first. first. A310-300 SR \3\ airplanes with <=18,000 total 7,000 total flight 1,500 flight 5,800 flight Pratt & Whitney 4000 engines. flight cycles \1\. cycles or 19,600 cycles \2\. cycles or 16,200 total flight flight hours, hours, whichever whichever occurs occurs first. first. A310-300 SR \3\ airplanes with >18,000 total 19,500 total 250 flight cycles 5,800 flight Pratt & Whitney 4000 engines. flight cycles \1\. flight cycles or \2\. cycles or 16,200 55,500 total flight hours, flight hours, whichever occurs whichever occurs first. first. A310-300 LR \4\ airplanes with <=18,000 total 5,900 total flight 1,500 flight 6,000 flight Pratt & Whitney JT9D engines. flight cycles \1\. cycles or 29,500 cycles \2\. cycles or 30,300 total flight flight hours, hours, whichever whichever occurs occurs first. first. A310-300 LR \4\ airplanes with >18,000 total 19,500 total 250 flight cycles 6,000 flight Pratt & Whitney JT9D engines. flight cycles \1\. flight cycles or \2\. cycles or 30,300 55,500 total flight hours, flight hours, whichever occurs whichever occurs first. first. A310-300 LR \4\ airplanes with <=18,000 total 4,800 total flight 1,500 flight 5,100 flight GE engines. flight cycles \1\. cycles or 24,100 cycles \2\. cycles or 25,500 total flight flight hours, hours, whichever whichever occurs occurs first. first. A310-300 LR \4\ airplanes with >18,000 total 19,500 total 250 flight cycles 5,100 flight GE engines. flight cycles \1\. flight cycles or \2\. cycles or 25,500 55,500 total flight hours, flight hours, whichever occurs whichever occurs first. first. A310-300 LR \4\ airplanes with <=18,000 total 4,800 total flight 1,500 flight 5,200 flight Pratt & Whitney 4000 engines. flight cycles \1\. cycles or 24,000 cycles \2\. cycles or 26,300 total flight flight hours, hours, whichever whichever occurs occurs first. first. A310-300 LR \4\ airplanes with >18,000 total 19,500 total 250 flight cycles 5,200 flight Pratt & Whitney 4000 engines. flight cycles \1\. flight cycles or \2\. cycles or 26,300 55,500 total flight hours, flight hours, whichever occurs whichever occurs first. first. ---------------------------------------------------------------------------------------------------------------- \1\ As of the effective date of this AD. \2\ After the effective date of this AD. \3\ ``SR'' applies to airplanes with average flights less than 4 flight hours. \4\ ``LR'' refers to airplanes with average flights of 4 or more flight hours. * * * * * Issued in Renton, Washington on April 15, 2010. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2010-9521 Filed 5-3-10; 8:45 am] BILLING CODE 4910-13-P