Airworthiness Directives:

Federal Register Volume 76, Number 114 (Tuesday, June 14, 2011)

Proposed Rules

Pages 34625-34627

From the Federal Register Online via the Government Printing Office [www.gpo.gov]

FR Doc No: 2011-14697

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration 14 CFR Part 39

Docket No. FAA-2011-0566; Directorate Identifier 2010-NM-271-AD

RIN 2120-AA64

Airworthiness Directives; The Boeing Company Model 747-100, 747- 100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747SR, and 747SP Series Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

SUMMARY: We propose to adopt a new airworthiness directive (AD) for the products listed above. This proposed AD would require modification of the fluid drain path in the leading edge area of the wing. This proposed AD was prompted by a design review following a ground fire incident and reports of flammable fluid leaks from the wing leading edge area onto the engine exhaust area. We are proposing this AD to prevent flammable fluid from leaking onto the engine exhaust nozzle, which could result in a fire.

DATES: We must receive comments on this proposed AD by July 29, 2011.

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: Deliver to Mail address above between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays.

For service information identified in this proposed AD, contact

Boeing Commercial Airplanes, Attention: Data & Services Management,

P.O. Box 3707, MC 2H-65, Seattle, Washington 98124-2207; phone: 206- 544-5000, extension 1; fax: 206-766-5680; e-mail: me.boecom@boeing.com;

Internet: https://www.myboeingfleet.com. You may review copies of the referenced service information at the FAA, Transport Airplane

Directorate, 1601 Lind Avenue, SW., Renton, Washington. For information on the availability of this material at the FAA, call 425-227-1221.

Examining the AD Docket

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 proposed AD, the regulatory evaluation, any comments received, and other information. The street address for the Docket Office (phone: 800-647-5527) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt.

FOR FURTHER INFORMATION CONTACT: Tung Tran, Aerospace Engineer,

Propulsion Branch, ANM-140S, Seattle Aircraft Certification Office

(ACO), FAA, 1601 Lind Avenue, SW., Renton, Washington 98057-3356; phone: 425-917-6505; fax: 425-917-6590; e-mail: Tung.Tran@faa.gov.

SUPPLEMENTARY INFORMATION:

Comments Invited

We invite you to send any written relevant data, views, or arguments about this proposal. Send your comments to an address listed under the ADDRESSES section. Include ``Docket No. FAA-2011-0566;

Directorate Identifier 2010-NM-271-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 because of 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

We have received a report of fuel leaking from the wing leading edge area at the inboard end of the number 5 leading edge slat of a

Model 737 airplane. The leak was discovered during a post-flight inspection with a fuel quantity of over 2,500 pounds. Subsequent investigation found that the leak occurred in an area of the front spar

Page 34626

that does not have a proper drain path. This led to the fuel draining onto the engine exhaust nozzle. The leak appears to have been caused by a loose retaining nut of the slat track down stop. We are proposing this AD to prevent flammable fluid from leaking onto the engine exhaust nozzle, which could result in a fire.

A Model 747 design review revealed that some of the design features in the Model 737 wing leading edge area also exist in Model 747 airplanes. Additional design reviews have led to similar findings in

Model 757 and Model 767 airplanes. We have issued AD 2010-23-13

Amendment 39-16502 (75 FR 68688, November 9, 2009), for Model 757 airplanes, and are considering rulemaking for Model 737 and Model 767 airplanes.

Relevant Service Information

We reviewed Boeing Special Attention Service Bulletin 747-57-2332, dated November 9, 2010. This service information divides the affected airplanes into 10 groups. For all groups, this service information describes procedures for modifying the fluid drain path in the leading edge area of the wing. The modification consists of changing fluid dam assemblies at the wing outboard leading edge station (OLES) 1250, and installing seal assemblies at OLES 1185. Additionally, this service information specifies changing the lower leading edge wing panels through repairs, parts installation, and installing drain tube assemblies.

For Groups 1 through 6, this service information also specifies installing fluid dam assemblies at wing inboard leading edge station 770.

FAA's Determination

We are proposing this AD because we evaluated all the relevant information and determined the unsafe condition described previously is likely to exist or develop in other products of the same type design.

Proposed AD Requirements

This proposed AD would require accomplishing the actions specified in the service information described previously.

Costs of Compliance

We estimate that this proposed AD will affect 258 airplanes of U.S. registry.

We estimate the following costs to comply with this proposed AD:

Estimated Costs

Cost on U.S.

Action

Labor cost

Parts cost

Cost per product

operators

Fluid drainage modification

95 work-hours x $85 per

$33,609

$41,684

$5,960,812

(Groups 1-6) (143 airplanes).

hour = $8,075.

Fluid drainage modification

90 work-hours x $85 per

29,304

36,954

4,249,710

(Groups 7-10) (115 airplanes). hour = $7,650.

According to the manufacturer, some of the costs of this proposed

AD may be covered under warranty, thereby reducing the cost impact on affected individuals. We do not control warranty coverage for affected individuals. As a result, we have included all costs in our cost estimate.

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),

(3) Will not affect intrastate aviation in Alaska, and

(4) 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.

List of Subjects in 14 CFR Part 39

Air transportation, Aircraft, Aviation safety, Incorporation by reference, 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.

Sec. 39.13 [Amended] 2. The FAA amends Sec. 39.13 by adding the following new airworthiness directive (AD):

The Boeing Company: Docket No. FAA-2011-0566; Directorate Identifier 2010-NM-271-AD.

Comments Due Date

(a) We must receive comments by July 29, 2011.

Affected ADs

(b) None.

Applicability

(c) This AD applies to The Boeing Company Model 747-100, 747- 100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, 747SR, and 747SP series airplanes, certificated in any category, as identified in Boeing Special Attention Service

Bulletin 747-57-2332, dated November 9, 2010.

Page 34627

Subject

(d) Joint Aircraft System Component (JASC)/Air Transport

Association (ATA) of America Code 57: Wings.

Unsafe Condition

(e) This AD was prompted by a design review following a ground fire incident and reports of flammable fluid leaks from the wing leading edge area onto the engine exhaust area. We are issuing this

AD to prevent flammable fluid from leaking onto the engine exhaust nozzle, which could result in a fire.

Compliance

(f) Comply with this AD within the compliance times specified, unless already done.

Leading Edge Installation

(g) Within 60 months after the effective date of this AD, modify the fluid drain path in the leading edge area of the wing, in accordance with the Accomplishment Instructions of Boeing Special

Attention Service Bulletin 747-57-2332, dated November 9, 2010.

Alternative Methods of Compliance (AMOCs)

(h)(1) The Manager, Seattle Aircraft Certification Office, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight

Standards District Office, as appropriate. If sending information directly to the manager of the ACO, send it to the attention of the person identified in the Related Information section of this AD.

Information may be e-mailed to: 9-ANM-Seattle-ACO-AMOC-Requests@faa.gov.

(2) Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/certificate holding district office.

Related Information

(i) For more information about this AD, contact Tung Tran,

Aerospace Engineer, Propulsion Branch, ANM-140S, Seattle Aircraft

Certification Office (ACO), FAA, 1601 Lind Avenue, SW., Renton,

Washington 98057-3356; phone: 425-917-6505; fax: 425-917-6590; e- mail: Tung.Tran@faa.gov.

(j) For service information identified in this AD, contact

Boeing Commercial Airplanes, Attention: Data & Services Management,

P.O. Box 3707, MC 2H-65, Seattle, Washington 98124-2207; phone: 206- 544-5000, extension 1; fax: 206-766-5680; e-mail: me.boecom@boeing.com; Internet: https://www.myboeingfleet.com. You may review copies of the referenced service information at the FAA,

Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton,

Washington. For information on the availability of this material at the FAA, call 425-227-1221.

Issued in Renton, Washington, on June 7, 2011.

Ali Bahrami,

Manager, Transport Airplane Directorate, Aircraft Certification

Service.

FR Doc. 2011-14697 Filed 6-13-11; 8:45 am

BILLING CODE 4910-13-P