Airworthiness Directives:

Federal Register Volume 76, Number 214 (Friday, November 4, 2011)

Proposed Rules

Pages 68366-68368

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

FR Doc No: 2011-28568

Federal Register

Proposed Rules

Page 68366

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration 14 CFR Part 39

Docket No. FAA-2011-1165; Directorate Identifier 2011-NM-002-AD

RIN 2120-AA64

Airworthiness Directives; The Boeing Company Model 777-200 and - 300 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 certain The Boeing Company Model 777-200 and -300 series airplanes.

This proposed AD would require replacing certain single-tabbed bonding brackets in the airplane empennage with two-tabbed bonding brackets.

This proposed AD would also require, for certain airplanes, installing new bonding jumpers, and measuring the resistance of the modified installation to verify resistance is within specified limits. This proposed AD was prompted by reports of two failures of the single- tabbed bracket on the rudder. We are proposing this AD to prevent failure of the bonding jumper bracket, which could result in loss of lightning protection ground path, which could lead to increased lightning-induced currents and subsequent damage to composite structures, hydraulic tubes, and actuator control electronics. In the event of a lightning strike, loss of lightning ground protection could result in the loss of control of the airplane.

DATES: We must receive comments on this proposed AD by December 19, 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; telephone

(206) 544-5000, extension 1; fax (206) 766-5680; email 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: Georgios Roussos, Aerospace Engineer,

Systems and Equipment Branch, ANM-130S, Seattle Aircraft Certification

Office (ACO), FAA, 1601 Lind Avenue SW., Renton, Washington 98057-3356; telephone (425) 917-6482; fax (425) 917-6590; email: georgios.roussos@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-2011-1165;

Directorate Identifier 2011-NM-002-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 received reports of two failures of the single-tabbed bracket on the rudder. The bracket was discolored and melted, the tab was completely severed and burned, and the bonding jumpers were detached from the bracket. We also received a report of a similar failure of the ground clip that connects to the other end of the jumpers to the vertical stabilizer. Boeing has determined that the root cause of these failures was a combination of electromagnetic forces on the jumpers and resistive heating of the bracket and ground clip during lightning strikes. This condition, if not corrected, could result in loss of lightning protection ground path, which could lead to increased lightning-induced currents and could subsequently damage composite structures, hydraulic tubes, and actuator control electronics. In the event of a lightning strike, loss of lightning ground protection could result in loss of control of the airplane.

Relevant Service Information

We reviewed Boeing Service Bulletin 777-55A0014, Revision 1, dated

April 1, 2010. This service bulletin describes procedures for replacing certain single-tabbed bonding brackets in the airplane empennage with two-tabbed bonding brackets.

Boeing Service Bulletin 777-55A0014, Revision 1, dated April 1, 2010, specifies prior or concurrent accomplishment of Boeing Service

Bulletin 777-55A0010, Revision 1, dated April 17, 2001, for installing new bonding jumpers, and measuring the resistance of the modified installation to verify resistance is within specified limits.

Page 68367

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 these same type designs.

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 affects 87 airplanes of U.S. registry.

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

Estimated Costs

Parts

Cost per Cost on U.S.

Action

Labor cost

cost

product

operators

Replacement................................ 21 work-hours x $85 per hour

$1,235

$3,020

$262,740

= $1,785.

Estimated Costs for Concurrent Actions

Parts

Cost per Cost on U.S.

Action

Labor cost

cost

product

operators

Replacement................................ 66 work-hours x $85 per hour

$2,668

$8,278

$248,340

= $5,610.

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-2011-1165; Directorate Identifier 2011-NM-002-AD.

Comments Due Date

(a) We must receive comments by December 19, 2011.

Affected ADs

(b) None.

Applicability

(c) The Boeing Company Model 777-200 and -300 series airplanes, certificated in any category, as identified in Boeing Service

Bulletin 777-55A0014, Revision 1, dated April 1, 2010.

Subject

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

Association (ATA) of America Code 55: Stabilizers.

Unsafe Condition

(e) This AD was prompted by reports of two failures of the single-tabbed bonding bracket on the rudder. We are issuing this AD to prevent failure of the bonding jumper bracket, which could result in loss of lightning protection ground path, which could lead to increased lightning-induced currents and subsequent damage to composite structures, hydraulic tubes, and actuator control electronics. In the event of a lightning strike, loss of lightning ground protection could result in loss of control of the airplane.

Compliance

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

Replacement

(g) Within 48 months after the effective date of this AD, replace certain single-tabbed bonding brackets in the airplane empennage with two-tabbed bonding brackets, in accordance with the

Accomplishment Instructions of Boeing Service Bulletin 777-55A0014,

Revision 1, dated April 1, 2010.

Concurrent Requirements

(h) For airplanes identified in Boeing Service Bulletin 777- 55A0010, Revision 1, dated April 17, 2001: Prior to or concurrently with accomplishing the requirements of paragraph (g) of this AD, install new bonding jumpers, and do resistance measurements of the modified installation to verify resistance is within the limits specified in the Accomplishment Instructions of Boeing Service

Bulletin 777-55A0010, Revision 1, dated April 17, 2001. Do the actions in accordance with the Accomplishment Instructions of Boeing

Service Bulletin 777-55A0010, Revision 1, dated April 17, 2001.

Page 68368

Credit for Actions Accomplished in Accordance With Previous Service

Information

(i) Replacing certain single-tabbed bonding brackets with two- tabbed bonding brackets in accordance with Boeing Alert Service

Bulletin 777-55A0014, dated May 8, 2008, before the effective date of this AD, is acceptable for compliance with the corresponding modification required by paragraph (g) of this AD.

(j) Installing new bonding jumpers, and doing resistance measurements of the modified installation that verify the resistance is within the specified limits, in accordance with Boeing Alert

Service Bulletin 777-55A0010, dated October 26, 2000, before the effective date of this AD, is acceptable for compliance with the corresponding modification required by paragraph (h) of this AD.

Alternative Methods of Compliance (AMOCs)

(k)(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 emailed 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

(l) For more information about this AD, contact Georgios

Roussos, Aerospace Engineer, Systems and Equipment Branch, ANM-130S,

Seattle Aircraft Certification Office (ACO), FAA, 1601 Lind Avenue

SW., Renton, Washington 98057-3356; telephone (425) 917-6482; fax

(425) 917-6590; email: georgios.roussos@faa.gov.

(m) 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; telephone

(206) 544-5000, extension 1; fax (206) 766-5680; email 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 October 20, 2011.

Kalene C. Yanamura,

Acting Manager, Transport Airplane Directorate, Aircraft Certification

Service.

FR Doc. 2011-28568 Filed 11-3-11; 8:45 am

BILLING CODE 4910-13-P