MEA's new A330-200s will have 44 seats in Cedar Class and 200 in Economy. They will be used to increase capacity on existing routes.

Comments on this story may be sent to aii.feedback@m2.com

"This is the first A330-200 being delivered to MEA with a new livery reflecting the Lebanese flag. With its efficient fuel economy and passenger comfort, the A330-200 will enable MEA to meet and respond to the rising demand for passenger services between Lebanon, the middle East, Africa and Europe", said Mr. El-Hout.

MEA flies an all Airbus fleet including A321s and leased A330-200s on non-stop routes to Europe, within the Middle East and Africa. The new directly purchased A330s will be deployed to increase capacity on existing routes. "Airbus' partnership with MEA is an amazing success story. It dates back to the early days when MEA operated the A300s and A310s - and today as the company embarks on a future with the world's most efficient, operationally cost effective and most comfortable aircraft in its class, all of us at Airbus wish MEA the most prosperous future", said Mr. Fekih.

The A330-200 is able to accommodate seat and class configurations to suit diverse customer requirements. It has a range of up to 6,750 nm / 12,500 km with a full passenger load. Its large under-floor cargo holds can also carry standard pallets and containers side-by-side.

(C) 2008 Mena Report (www.menareport.com)

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at VTP (vertical tail plane) attachment cutout between Frame (FR) 80 and FR86. This damage occurred between 58341 and 72891 simulated flight cycles (FC).

Due to the higher Design Service Goal and different design (e.g. doubler thickness) [of the] A330-200/-300 and A340-300 aircraft series, the damage assessment concluded [there was] potential impact on [the airplanes specified in the] applicability.

* * * * *

The unsafe condition is crack propagation in the VTP attachment cutout, which could reduce airplane structural integrity in the tail section. The proposed AD would require actions that are intended to address the unsafe condition described in the MCAI.

EFFECTIVE DATE: We must receive comments on this proposed AD by July 24, 2008.

ADDRESSES: You may send comments by any of the following methods:

. Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments.

. Fax: (202) 493-2251.

. Mail: U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue, SE., Washington, DC 20590.

. Hand Delivery: U.S. Department of Transportation, Docket Operations, M- 30, West Building Ground Floor, Room W12-40, 1200 New Jersey Avenue, SE., Washington, DC, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays.

Examining the AD Docket

You may examine the AD docket on the Internet at http://www.regulations.gov; or in person at the Docket Operations office between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this proposed AD, the regulatory evaluation, any comments received, and other information. The street address for the Docket Operations office (telephone (800) 647-5527) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt.

FOR FURTHER INFORMATION CONTACT: Vladimir Ulyanov, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425) 227-1138; fax (425) 227-1149.

SUPPLEMENTARY INFORMATION: We invite you to send any written relevant data, views, or arguments about this proposed AD. Send your comments to an address listed under the ADDRESSES section. Include "Docket No. FAA-2008-0667; Directorate Identifier 2008-NM-009-AD" at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of this proposed AD. We will consider all comments received by the closing date and may amend this proposed AD based on those comments.

We will post all comments we receive, without change, to http://www.regulations.gov, including any personal information you provide. We will also post a report summarizing each substantive verbal contact we receive about this proposed AD.

Discussion

The European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Community, has issued EASA Airworthiness Directive 2007-0284, dated November 12, 2007 (referred to after this as "the MCAI"), to correct an unsafe condition for the specified products. The MCAI states:

During fatigue tests (EF3) on the A340-600, damages were found in longitudinal doubler at VTP (vertical tail plane) attachment cutout between Frame (FR) 80 and FR86. This damage occurred between 58341 and 72891 simulated Flight Cycles (FC).

Due to the higher Design Service Goal and different design (e.g. doubler thickness) [of the] A330-200/-300 and A340-300 aircraft series, the damage assessment concluded [there was] potential impact on [the airplanes specified in the] applicability.

[T]o allow early detection of cracks, which could [prevent] possible crack propagation and consequently maintain the structural integrity of the upper shell structure between FR80 and FR86, this Airworthiness Directive (AD) mandates an inspection program [for cracking] of this area using a high frequency eddy current (HFEC) method, and a modification to improve the upper shell structure.

The unsafe condition is crack propagation in the VTP attachment cutout, which could reduce airplane structural integrity in the tail section. Corrective actions include doing eddy current inspections for cracking of certain fastener rows, and contacting Airbus for repair instructions and repairing. You may obtain further information by examining the MCAI in the AD docket.

Relevant Service Information

Airbus has issued the service bulletins specified in the following table. The compliance times in paragraph 1.E.(2) of the service bulletins range from 14,200 total flight cycles through 27,900 total flight cycles (for the initial inspection); from 1,700 flight cycles or 11,900 flight hours, whichever occurs first, through 4,600 flight cycles or 14,000 flight hours, whichever occurs first (for the repetitive inspection intervals); and from 10,700 total flight cycles through 14,200 total flight cycles (for the modification); depending upon airplane model and weight variant. The actions described in this service information are intended to correct the unsafe condition identified in the MCAI.

     Airbus Service Information
Service Bulletin                       Date
A330-53-3159                           September 19, 2007.
A330-53-3160                           July 9, 2007.
A330-53-3168                           September 19, 2007.
A340-53-4165                           September 19, 2007.
A340-53-4172                           July 10, 2007.
A340-53-4174                           September 19, 2007.

FAA's Determination and Requirements of This Proposed AD

This product has been approved by the aviation authority of another country, and is approved for operation in the United States. Pursuant to our bilateral agreement with the State of Design Authority, we have been notified of the unsafe condition described in the MCAI and service information referenced above. We are proposing this AD because we evaluated all pertinent information and determined an unsafe condition exists and is likely to exist or develop on other products of the same type design.

Differences Between This AD and the MCAI or Service Information

We have reviewed the MCAI and related service information and, in general, agree with their substance. But we might have found it necessary to use different words from those in the MCAI to ensure the AD is clear for U.S. operators and is enforceable. In making these changes, we do not intend to differ substantively from the information provided in the MCAI and related service information.

We might also have proposed different actions in this AD from those in the MCAI in order to follow FAA policies. Any such differences are highlighted in a Note within the proposed AD.

Costs of Compliance

Based on the service information, we estimate that this proposed AD would affect about 26 products of U.S. registry. We also estimate that it would take about 202 work-hours per product to comply with the basic requirements of this proposed AD. The average labor rate is $80 per work-hour. Required

[Page Number 35605]

parts would cost about $19,020 per product. Where the service information lists required parts costs that are covered under warranty, we have assumed that there will be no charge for these costs. As we do not control warranty coverage for affected parties, some parties may incur costs higher than estimated here. Based on these figures, we estimate the cost of the proposed AD on U.S. operators to be $914,680, or $35,180 per product.

Authority for This Rulemaking

Title 49 of the United States Code specifies the FAA's authority to issue rules on aviation safety. Subtitle I, section 106, describes the authority of the FAA Administrator. "Subtitle VII: Aviation Programs," describes in more detail the scope of the Agency's authority.

We are issuing this rulemaking under the authority described in "Subtitle VII, Part A, Subpart III, Section 44701: General requirements." Under that section, Congress charges the FAA with promoting safe flight of civil aircraft in air commerce by prescribing regulations for practices, methods, and procedures the Administrator finds necessary for safety in air commerce. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on products identified in this rulemaking action.

Regulatory Findings

We determined that this proposed AD would not have federalism implications under Executive Order 13132. This proposed AD would not have a substantial direct effect on the States, on the relationship between the national Government and the States, or on the distribution of power and responsibilities among the various levels of government.

For the reasons discussed above, I certify this proposed regulation:

1. Is not a "significant regulatory action" under Executive Order 12866;

2. Is not a "significant rule" under the DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979); and

3. Will not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act.

We prepared a regulatory evaluation of the estimated costs to comply with this proposed AD and placed it in the AD docket.

List of Subjects in 14 CFR Part 39

Air transportation, Aircraft, Aviation safety, Safety.

The Proposed Amendment

Accordingly, under the authority delegated to me by the Administrator, the FAA proposes to amend 14 CFR part 39 as follows:

PART 39--AIRWORTHINESS DIRECTIVES

1. The authority citation for part 39 continues to read as follows:

Authority: 49 U.S.C. 106(g), 40113, 44701.

[Section] 39.13 [Amended]

2. The FAA amends [Section] 39.13 by adding the following new AD:

Airbus: Docket No. FAA-2008-0667; Directorate Identifier 2008-NM-009-AD.

Comments Due Date

(a) We must receive comments by July 24, 2008.

Affected ADs

(b) None.

Applicability

(c) This AD applies to Airbus Model A330-200, A330-300, and A340-300 series airplanes; certificated in any category; all certified models, all serial numbers; on which Airbus modification 44205 has been embodied in production, except those on which Airbus modification 52974 or 53223 has been embodied in production.

Subject

(d) Air Transport Association (ATA) of America Code 53: Fuselage.

Reason

(e) The mandatory continuing airworthiness information (MCAI) states:

During fatigue tests (EF3) on the A340-600, damages were found in longitudinal doubler at VTP (vertical tail plane) attachment cutout between Frame (FR) 80 and FR86. This damage occurred between 58341 and 72891 simulated Flight Cycles (FC).

Due to the higher Design Service Goal and different design (e.g. doubler thickness) [of the] A330-200/-300 and A340-300 aircraft series, the damage assessment concluded [there was] potential impact on [the airplanes specified in the] applicability.

[T]o allow early detection of cracks, which could [prevent] possible crack propagation and consequently maintain the structural integrity of the upper shell structure between FR80 and FR86, this Airworthiness Directive (AD) mandates an inspection program [for cracking] of this area using a high frequency eddy current (HFEC) method, and a modification to improve the upper shell structure.

The unsafe condition is crack propagation in the VTP attachment cutout, which could reduce airplane structural integrity in the tail section. Corrective actions include doing eddy current inspections for cracking of certain fastener rows, and contacting Airbus for repair instructions and repairing.

Actions and Compliance

(f) Unless already done, do the following actions.

(1) For Airbus Model A330-300 and A340-300 series airplanes, except Model A340-300 weight variant (WV) 027 airplanes: At the applicable compliance time specified in paragraph (f)(2) of this AD, perform a HFEC inspection of the upper shell structure between FR80 and FR86, in accordance with the Accomplishment Instructions of Airbus Service Bulletin A330-53-3168 or A340- 53-4174, both dated September 19, 2007, as applicable.

(i) If no crack is detected, repeat the inspection thereafter within the intervals specified in paragraph 1.E.(2) of Airbus Service Bulletin A330-57- 3168 or A340-53-4174, as applicable.

(ii) If any crack is detected during any inspection required by this AD: Before next flight, contact Airbus for repair instructions and do applicable repairs.

(iii) Doing the modification of the upper shell structure in accordance with Airbus Service Bulletin A330-53-3159 or Airbus Service Bulletin A340-53- 4165, both dated September 19, 2007, as applicable, ends the inspections required by paragraph (f)(1) of this AD.

(2) Do the actions required by paragraph (f)(1) of this AD at the later of the compliance times specified in paragraph (f)(2)(i) and (f)(2)(ii) of this AD.

(i) Within the compliance times specified in paragraph 1.E.(2) of Airbus Service Bulletin A330-53-3168 or A340-53-4174, both dated September 19, 2007, as applicable.

(ii) Within 3 months after the effective date of this AD.

(3) At the applicable time specified in paragraphs (f)(3)(i), (f)(3)(ii), and (f)(3)(iii) of this AD or within 3 months after the effective date of this AD, whichever occurs later, modify the upper shell structure between FR80 and FR86 (including doing eddy current inspections for cracking of certain fastener rows and applicable corrective actions) in accordance with the Accomplishment Instructions of Airbus Service Bulletin A330-53-3160, dated July 9, 2007, or Airbus Service Bulletin A340-53-4172, dated July 10, 2007, as applicable. Do all applicable corrective actions before further flight.

(i) For Model A330-200 airplanes, WV 020 through WV 027: Prior to the accumulation of 13,500 total flight cycles.

(ii) For Model A330-200 airplanes, WV 050 through WV 055: Prior to the accumulation of 10,700 total flight cycles or 59,300 total flight hours, whichever occurs first.

(iii) For Model A340-300 airplanes, WV 027: Prior to the accumulation of 14,200 total flight cycles.

FAA AD Differences

Note: This AD differs from the MCAI and/or service information as follows: Although the MCAI allows further flight after cracks are found during compliance with the required action, this AD requires that you repair the crack(s) before further flight.

[Page Number 35606]

Other FAA AD Provisions

(g) The following provisions also apply to this AD:

(1) Alternative Methods of Compliance (AMOCs): The Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Send information to ATTN: Vladimir Ulyanov, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425) 227-1138; fax (425) 227-1149. Before using any approved AMOC on any airplane to which the AMOC applies, notify your appropriate principal inspector (PI) in the FAA Flight Standards District Office (FSDO), or lacking a PI, your local FSDO.

(2) Airworthy Product: For any requirement in this AD to obtain corrective actions from a manufacturer or other source, use these actions if they are FAA-approved. Corrective actions are considered FAA-approved if they are approved by the State of Design Authority (or their delegated agent). You are required to assure the product is airworthy before it is returned to service.

(3) Reporting Requirements: For any reporting requirement in this AD, under the provisions of the Paperwork Reduction Act, the Office of Management and Budget (OMB) has approved the information collection requirements and has assigned OMB Control Number 2120-0056.

Related Information

(h) Refer to MCAI European Aviation Safety Agency (EASA) Airworthiness Directive 2007-0284, dated November 12, 2007, and the service bulletins specified in Table 1 of this AD, for related information.

     Table 1.--Service Information
Airbus Service                         Date
Bulletin
A330-53-3159                           September 19, 2007.
A330-53-3160                           July 9, 2007.
A330-53-3168                           September 19, 2007.
A340-53-4165                           September 19, 2007.
A340-53-4172                           July 10, 2007.
A340-53-4174                           September 19, 2007.

Issued in Renton, Washington, on June 9, 2008.

Ali Bahrami,

Manager, Transport Airplane Directorate, Aircraft Certification Service.

[FR Doc. E8-14192 Filed 6-23-08; 8:45 am]

BILLING CODE 4910-13-P

Vol. 73, No. 122

14 CFR Part 39; [Docket No. FAA-2008-0667; Directorate Identifier 2008-NM-009- AD]; RIN 2120-AA64

Proposed Rules

Emirates has been steadily building up its presence in the two Asian economies, having previously announced additional frequencies to Shanghai and Beijing in China, and New Delhi, Bangalore, Hyderabad and Ahmedabad in India. The airline's top executives comprising Richard Vaughan, Senior Vice President, Commercial Operations East Asia and Australasia; Pradeep Kumar, Senior Vice President, Cargo Revenue Optimisation; and Salem Obaidalla, Senior Vice President, Commercial Operations, West Asia, Indian Ocean and Africa flagged off the inaugural flights.

Guangzhou, the economic centre of the Pearl River Delta, has very strong business connections with Europe and Africa. The city's chief export items include electrical goods such as televisions and refrigerators, as well as consumer products. Trade between China and Africa currently exceeds US$60 billion, making China one of the top three trading partners of Africa. It is expected to cross US$ 100 billion by 2010.

Further bearing testimony to China's burgeoning economy are statistics released by The World Tourism Organisation that forecast China will become the largest inbound and outbound tourist country by 2020. Tourism growth in China has outstripped the GDP growth rate since 1990. Generating US$461 billion of economic activity last year, China's travel and tourism industry has successfully established it as Asia's largest outbound tourist source nation, outranking Japan. At present, Guangzhou city attracts large contingents of European visitors to its historical sites that include 123 state-protected sites.

Richard Vaughan thanked the Chinese government and aviation authorities for their support and stressed Emirates' commitment to the market: "Emirates' sprawling global network, including 22 European and 15 African gateways, will support China's economic and tourism industries. Emirates services will assist the Chinese tourism authorities in their drive to attract more tourists and at the same time strengthen the trade momentum between China and Africa, currently growing at a robust 30 per cent." Emirates' flights from Europe and Africa, particularly from the United Kingdom, France, Germany, South Africa, Kenya, Cote D'Ivoire and Ghana connect to China within four to seven hours of transit time in Dubai.

He added: "Emirates' efficient and reliable air links will facilitate inbound arrivals from over 60 countries on six continents, and will support the Chinese authorities as they ready to welcome over half a million international tourists for the Beijing Olympics 2008." Kozhikode - a port city in the Indian state of Kerala - has been frequented by Middle East traders as early as the seventh century. More recently, Kozhikode is frequented by international visitors attracted by the city's tourist sites such as Kappad beach which welcomed Vasco Da Gama in the 15th century, quaint fishing and boating colonies, bird and dolphin sanctuaries for the animal lovers, as well as rock climbing and mountain trekking sites for the adventure-hungry. Kozhikode is also the original home of millions of Keralites who work and live in the Gulf region.

Salem Obaidalla noted: "Emirates presently operates services to Thiruvananthapuram and Cochin. The launch of Emirates' flights to Kozhikode will allow international tourists to cover the length and breadth of Kerala more conveniently, by enabling them to arrive in Northern Kerala and depart from the state's southern region or vice versa. The new flights will also serve Keralites living in the Gulf region and visiting home each year." "Emirates has a robust presence in the Middle East, serving the region with 163 weekly flights to 12 gateways via its Dubai hub. We have timed our flights such that they offer convenient connections to Kozhikode via Dubai." Emirates will operate an Airbus A330-200 on the Guangzhou route. It will operate both Boeing 777-200 and A330-200 aircraft on the Kozhikode route. (C) 2008 Al Bawaba (www.albawaba.com)