### 78591 Federal Register / Vol. 75, No. 241 / Thursday, December 16, 2010 / Rules and Regulations

T ABLE 

### 2—M ATERIAL 

### I NCORPORATED BY 

### R EFERENCE

Document— Revision— Date—

Boeing Alert Service Bulletin 777–57A0051 ................................................................................. Original ........................ May 15, 2006 Boeing Alert Service Bulletin 777–57A0057 ................................................................................. 1 ................................... August 2, 2007 Boeing Alert Service Bulletin 777-57A0059 .................................................................................. Original ........................ October 30, 2008 Boeing Service Bulletin 777–57A0050 .......................................................................................... 2 ................................... May 14, 2009

(1) The Director of the Federal Register approved the incorporation by reference of this service information under 5 U.S.C. 552(a) and 1 CFR part 51.

(2) 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; e-mail me.boecom@boeing.com; Internet https://www.myboeingfleet.com.

(3) You may review copies of the 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.

(4) You may also review copies of the service information that is incorporated by reference 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/ code

_ of

_ federal

_regulations/ ibr

_locations.html. Issued in Renton, Washington, on November 18, 2010. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service.
[FR Doc. 2010–30606 Filed 12–15–10; 8:45 am]

**BILLING CODE 4910–13–P**

**DEPARTMENT OF TRANSPORTATION**

**Federal Aviation Administration**

**14 CFR Part 39**

**[Docket No. FAA–2008–1098; Directorate Identifier 2008–NM–108–AD; Amendment**  **39–16532; AD 2010–24–13]**

**RIN 2120–AA64**

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

**AGENCY :**  Federal Aviation Administration (FAA), DOT.

**ACTION :**  Final rule.

**SUMMARY :**  We are adopting a new airworthiness directive (AD) for the products listed above. This AD requires adding two new indicator lights on a certain panel to inform the captain and first officer of a low pressure condition in the left and right override/jettison pumps of the center wing tanks. This AD also requires replacing the left and right override/jettison switches on the M154 fuel control module on the P4 panel with improved switches and doing the associated wiring changes. This AD also requires, for certain airplanes, installation of a mounting bracket for the new indicator lights. This AD also requires a revision to the maintenance program to incorporate airworthiness limitation No. 28–AWL– 22. This AD also requires a revision to the airplane flight manual to advise the flightcrew what to do in the event that the pump low pressure light on the flight engineer’s panel does not illuminate when the pump is selected off. This AD was prompted by fuel system reviews conducted by the manufacturer. We are issuing this AD to prevent uncommanded operation of the override/jettison pumps of the center wing tanks, and failure to manually shut off the override/jettison pumps at the correct time, either of which could lead to an ignition source inside the center wing tank. This condition, in combination with flammable fuel vapors, could result in a center fuel tank explosion and consequent loss of the airplane.

**DATES :**  This AD is effective January 20,
2011.

The Director of the Federal Register approved the incorporation by reference of a certain publication listed in the AD as of January 20, 2011.

The Director of the Federal Register approved the incorporation by reference of a certain other publication listed in this AD as of June 12, 2008 (73 FR 25977, May 8, 2008).

**ADDRESSES :**  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; 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 AD, the regulatory evaluation, any comments received, and other information. The address for the Docket Office (phone: 800–647–5527) is 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 :**  Douglas Bryant, Aerospace Engineer, Propulsion Branch, ANM–140S, FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue SW., Renton, Washington 98057–3356; telephone (425) 917–6505; fax (425) 917–6590; email: douglas.n.bryant@faa.gov.

**SUPPLEMENTARY INFORMATION :** 

Discussion

We issued a supplemental notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to include an airworthiness directive (AD) that would apply to the specified products. That supplemental NPRM published in the Federal Register on October 1, 2010 (75 FR 60661). That supplemental NPRM proposed to require adding two new indicator lights on the P10 panel to inform the captain and first officer of a low pressure condition in the left and right override/jettison pumps of the center wing tanks. That supplemental NPRM also proposed to require replacing the left and right override/ jettison switches on the M154 fuel control module on the P4 panel with improved switches and doing the associated wiring changes. That supplemental NPRM also proposed to require, for certain airplanes, installation of a mounting bracket for the new indicator lights. That supplemental NPRM also proposed to require a revision to the maintenance program to incorporate airworthiness


### 78592 Federal Register / Vol. 75, No. 241 / Thursday, December 16, 2010 / Rules and Regulations

limitation No. 28–AWL–22. That supplemental NPRM also proposed to require a revision to the airplane flight manual to advise the flightcrew what to do in the event that the pump low pressure light on the flight engineer’s panel does not illuminate when the pump is selected off.

Comments

We gave the public the opportunity to participate in developing this AD. We received no comments on the supplemental NPRM or on the determination of the cost to the public. Clarification In our response in the supplemental NPRM to Northwest Airline’s Request to Reference Later Revision of Service Bulletin Cited in Original NPRM, we described some of the changes in Boeing Service Bulletin 747–28A2288, Revision 1, dated January 21, 2010. That service bulletin was described as having installation instructions for the LOW PRESS indicator lights for airplanes that did not have the warning panel ( i.e., the P10 panel) installed. We also described the changes to paragraph (g) of the Supplemental NPRM. We have revised the Summary and paragraph (g) of this AD to clarify that both groups of airplanes, with or without the warning panel installed, must install the two new indicator lights on certain panels (either the P10 panel, or for those airplanes without the P10 panel installed, the Autopilot Flight Director panel).

Conclusion

We reviewed the relevant data and determined that air safety and the public interest require adopting the AD as proposed. Costs of Compliance

We estimate that this AD affects 185 airplanes of U.S. registry.

We estimate the following costs to comply with this AD:



### E STIMATED 

### C OSTS

Action Labor cost Parts cost Cost per product Cost on U.S. operators

Boeing Service Bulletin 747-28A2288, Revision 1. Between 30 and 32 work-hours × $85 per hour = Between $2,550 and $2,720. Between $2,768 and $2,868. Between $5,318 and $5,588. Between $983,830 and $1,033,780.

AFM revision .............. 1 work-hour × $85 per hour = $85 ................. None .......................... $85 ............................. $15,725

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

This AD will not have federalism implications under Executive Order 13132. This AD will 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 that this AD:

(1) Is not a ‘‘ significant regulatory action ’’ under Executive Order 12866, (2) Is not a ‘‘ significant rule ’’ under 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.

Adoption of the Amendment

■ Accordingly, under the authority delegated to me by the Administrator, the FAA amends 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.

**§ 39.13 [Amended]**

■ 2. The FAA amends § 39.13 by adding the following new airworthiness directive (AD):
2010–24–13 The Boeing Company: Amendment 39–16532; Docket No. FAA–2008–1098; Directorate Identifier 2008–NM–108–AD. Effective Date (a) This AD is effective January 20, 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, 747SR, and 747SP series airplanes, certificated in any category; as identified in Boeing Service Bulletin 747–28A2288, Revision 1, dated January 21, 2010.

Note 1: This AD requires revisions to certain operator maintenance documents to include a new inspection. Compliance with this inspection is required by 14 CFR 91.403(c). For airplanes that have been previously modified, altered, or repaired in the areas addressed by this inspection, the operator may not be able to accomplish the inspections described in the revisions. In this situation, to comply with 14 CFR 91.403(c), the operator must request approval for an alternative method of compliance (AMOC) according to paragraph (l) of this AD. The request should include a description of changes to the required inspection that will ensure the continued operational safety of the airplane.

Subject

(d) Air Transport Association (ATA) of America Code 28: Fuel.

Unsafe Condition

(e) This AD results from fuel system reviews conducted by the manufacturer. The Federal Aviation Administration is issuing this AD to prevent uncommanded operation of the override/jettison pumps of the center wing tanks, and failure to manually shut off


### 78593 Federal Register / Vol. 75, No. 241 / Thursday, December 16, 2010 / Rules and Regulations

the override/jettison pumps at the correct time, either of which could lead to an ignition source inside the center wing tank. This condition, in combination with flammable fuel vapors, could result in a center fuel tank explosion and consequent loss of the airplane.
Compliance

(f) You are responsible for having the actions required by this AD performed within the compliance times specified, unless the actions have already been done. Installation of Indicator Lights and Replacement of Switches

(g) Within 36 months after the effective date of this AD: For airplanes with a P10 panel installed, add two new indicator lights on the P10 panel to inform the captain and first officer of a low pressure condition in the left and right override/jettison pumps of the center wing tanks, and, for airplanes that do not have the warning panel (P10 panel) installed, add a mounting bracket and two new indicator lights to the Autopilot Flight Director panel; and replace the left and right override/jettison switches on the M154 fuel control module on the P4 panel with improved switches; and do the associated wiring changes. Accomplish these actions by doing all of the applicable actions specified in the Accomplishment Instructions of Boeing Service Bulletin 747–28A2288, Revision 1, dated January 21, 2010, except where that service bulletin states ‘‘ 20–60–00, ’’ the correct sub-section number is ‘‘ 28–60– 06, ’’ and except as described in Table 1 of this AD.



### T ABLE 

### 1—P ART 

### N UMBER 

### C ORRECTION

Part name Part number specified in Figures 22 through 32 of Boeing Service Bulletin 747-28A2288, Revision 1, dated January 21, 2010 Part name of correct part Correct part number

Nut ................................................................ BACN10JC06CD Nut ............................................ .................... BACN10NW1 Bolt ............................................................... BACS12HN06–10 Screw ......................................... .................. BACS12HN04–6 Washer ......................................................... NAS1149D0632J Washer ............................................ ............. NAS1149DN416J

Note 2: For airplanes equipped with certain M154 fuel control modules, paragraph 2.C.2 of Boeing Service Bulletin 747–28A2288, Revision 1, dated January 21, 2010, refers to the BAE Systems service bulletins identified in Table 2 of this AD, as applicable, as additional sources of guidance for replacing the switches.



### T ABLE 

### 2—A DDITIONAL 

### S OURCES OF 

### G UIDANCE

Service bulletin Date

BAE Systems Service Bulletin 65B46124-28-01. February 16, 2006.BAE Systems Service Bulletin 65B46124-28-02. March 28, 2007.

BAE Systems Service Bulletin 65B46124-28-03. March 28, 2007.

BAE Systems Service Bulletin 65B46214-28-01. February 16, 2006.BAE Systems Service Bulletin 65B46214-28-02. March 28, 2007.

BAE Systems Service Bulletin 65B46214-28-03. March 28, 2007.

Maintenance Program Revision

(h) Concurrently with accomplishing the actions required by paragraph (g) of this AD, revise the maintenance program by incorporating Airworthiness Limitation (AWL) No. 28–AWL–22 of Section D of the Boeing 747–100/200/300/SP Airworthiness Limitations (AWLs) and Certification Maintenance Requirements (CMRs), D6– 13747–CMR, Revision March 2008. Where the AWL states ‘‘ 28–31–00, ’’ the correct section number is ‘‘ 28–42–00. ’’
Airplane Flight Manual (AFM) Revision

(i) Concurrently with accomplishing the actions required by paragraph (g) of this AD, revise Section 1, ‘‘ Certificate Limitations, ’’ of the applicable Boeing 747 AFM to include the following statement. This may be done by inserting a copy of this AD into the AFM. ‘‘ When the center tank override jettison pumps are selected off, the amber pump low pressure lights on the Flight Engineer’s panel should illuminate and remain on. If a pump low pressure light on the Flight Engineer’s panel does not illuminate, open the associated pump circuit breaker. ’’

Note 3: When a statement identical to that in paragraph (i) of this AD has been included in the general revisions of the AFM, the general revisions may be inserted into the AFM, and the copy of this AD may be removed from the AFM.

No Alternative Inspections or Inspection Intervals

(j) After accomplishing the action specified in paragraph (h) of this AD, no alternative inspections or inspection intervals may be used unless the inspections or inspection intervals are approved as an AMOC in accordance with the procedures specified in paragraph (l) of this AD.
Terminating Action for Maintenance Program Revision

(k) Incorporating AWL No. 28–AWL–22 into the maintenance program in accordance with paragraph (g) of AD 2008–10–07, Amendment 39–15513, or AD 2008–10–07 R1, Amendment 39–16070, terminates the action required by paragraph (h) of this AD.
Alternative Methods of Compliance (AMOCs)

(l)(1) The Manager, Seattle Aircraft Certification Office (ACO), 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: Douglas Bryant, Aerospace Engineer, Propulsion Branch, ANM–140S, FAA, Seattle ACO, 1601 Lind Avenue SW., Renton, Washington 98057–3356; telephone (425) 917–6505; fax (425) 917–6590. Information may be e-mailed to: 9–ANM–Seattle-ACO– AMOC–Requests@faa.gov

.

(2) To request a different method of compliance or a different compliance time for this AD, follow the procedures in 14 CFR 39.19. Before using any approved AMOC on any airplane to which the AMOC applies, notify your principal maintenance inspector (PMI) or principal avionics inspector (PAI), as appropriate, or lacking a principal inspector, your local Flight Standards District Office. The AMOC approval letter must specifically reference this AD.

Related Information

(m) For more information about this AD, contact Douglas Bryant, Aerospace Engineer, Propulsion Branch, ANM–140S, FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue SW., Renton, Washington 98057– 3356; telephone (425) 917–6505; fax (425) 917–6590; e-mail : douglas.n.bryant@faa.gov.
Material Incorporated by Reference

(n) You must use Boeing Service Bulletin 747–28A2288, Revision 1, dated January 21, 2010; and Boeing 747–100/200/300/SP Airworthiness Limitations (AWLs) and Certification Maintenance Requirements (CMRs), D6–13747–CMR, Revision March 2008; as applicable; to do the actions required by this AD, unless the AD specifies otherwise.

(1) The Director of the Federal Register approved the incorporation by reference Boeing Service Bulletin 747–28A2288, Revision 1, dated January 21, 2010, under 5 U.S.C. 552(a) and 1 CFR part 51.

(2) The Director of the Federal Register previously approved the incorporation by reference of Boeing 747–100/200/300/SP Airworthiness Limitations (AWLs) and Certification Maintenance Requirements (CMRs), D6–13747–CMR, Revision March 2008, on June 12, 2008 (73 FR 25977, May 8, 2008).

(3) 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–


### 78594 Federal Register / Vol. 75, No. 241 / Thursday, December 16, 2010 / Rules and Regulations

5680; e-mail me.boecom@boeing.com ; Internet https://www.myboeingfleet .com.

(4) You may review copies of the 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.

(5) You may also review copies of the service information that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at an NARA facility, call 202–741– 6030, or go to http://www.archives.gov/ federal

_register/code

_ of

_ federal

_regulations/ ibr

_locations.html. Issued in Renton, Washington, on November 18, 2010. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service.
[FR Doc. 2010–30612 Filed 12–15–10; 8:45 am]

**BILLING CODE 4910–13–P**

**DEPARTMENT OF TRANSPORTATION**

**Federal Aviation Administration**

**14 CFR Part 39**

**[Docket No. FAA–2009–0430; Directorate Identifier 2008–NM–148–AD; Amendment**  **39–16540; AD 2010–26–01]**

**RIN 2120–AA64**

**Airworthiness Directives; The Boeing Company Model 777–200 Series**  **Airplanes**

**AGENCY :**  Federal Aviation Administration (FAA), DOT.

**ACTION :**  Final rule.

**SUMMARY :**  We are adopting a new airworthiness directive (AD) for certain Model 777–200 series airplanes. This AD requires installing a new insulation blanket on the latch beam firewall of each thrust reverser (T/R) half. This AD results from an in-flight shutdown dueto an engine fire indication; an undercowl engine fire was extinguished after landing. The cause of the fire was uncontained failure of the starter in the engine core compartment; the fire progressed into the latch beam cavity and was fueled by oil from a damaged integrated drive generator oil line. We are issuing this AD to prevent a fire from entering the cowl or strut area, which could weaken T/R parts and result in reduced structural integrity of the T/R, possible separation of T/R parts during flight, and consequent damage to the airplane and injury to people or damage to property on the ground.

**DATES :**  This AD is effective January 20,
2011. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in the AD as of January 20, 2011.

**ADDRESSES :**  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; e-mail me.boecom@boeing.com ; Internet https://www.myboeingfleet.com

. 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 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 :**  Margaret Langsted, Aerospace Engineer, Propulsion Branch, ANM–140S, FAA, Seattle Aircraft Certification Office, 1601 Lind Avenue SW., Renton, Washington 98057–3356; telephone (425) 917–6500; fax (425) 917–6590.

**SUPPLEMENTARY INFORMATION :** 

Discussion

We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to include an airworthiness directive (AD) that would apply to certain Boeing Model 777–200 series airplanes. That NPRM was published in the Federal Register on May 7, 2009 (74 FR 21284). That NPRM proposed to require installing a new insulation blanket on the latch beam firewall of each thrust reverser (T/R) half.

Relevant Service Information

Since we issued the NPRM, we have reviewed Boeing Alert Service Bulletin 777–78A0066, Revision 2, dated April 8, 2010. Boeing Service Bulletin 777– 78A0066, Revision 1, dated March 12, 2009, was referred to in the original NPRM as the appropriate source of service information for accomplishing the proposed actions. No more work is necessary for airplanes on which Revision 1 of this service bulletin was used for doing the actions. Boeing Alert Service Bulletin 777–78A0066, Revision 2, dated April 8, 2010, moves certain airplanes to Group 1, and contains minor editorial changes.

We have revised paragraphs (c) and (g) of this AD to refer to Revision 2 of Boeing Alert Service Bulletin 777– 78A0066, Revision 2, dated April 8, 2010, and paragraph (h) to add credit for accomplishing the specified actions in accordance with Boeing Service Bulletin 777–78A0066, Revision 1, dated March 12, 2009.

Comments

We gave the public the opportunity to participate in developing this AD. We considered the comments received. Request To Clarify Description of Unsafe Condition

Boeing asked that we clarify the description of the unsafe condition by removing the words ‘‘ or strut ’’ from the identified description. Boeing stated that the unsafe condition, as currently written, is not correct. Boeing did not provide the reason that the description is not correct.

We disagree that the description of the unsafe condition should be clarified by removing ‘‘ or strut ’’ from the description. A fire in the lower latch beam area that burns through an inadequate firewall may propagate into the strut. We have made no change to the AD in this regard. Request To Clarify Applicability

Japan Airlines International (JALI) asked for clarification of the applicability specified in the NPRM. JALI stated that the applicability specifies Model 777–200 series airplanes identified in Boeing Service Bulletin 777–78A0066, Revision 1, dated March 12, 2009. JALI noted that the service bulletin specifies its effectivity as delivered condition, and the proposed rule is considered to be applicable to each T/R half that has been installed on airplanes with the applicable serial numbers. JALI added that the T/R half is a replaceable line unit and the installed airplane and/or engine position will be changed from the delivered condition in the future; the T/R half that is not necessary for doing the requirements in the NPRM may be installed on an airplane identified in the applicability.

JALI stated that, in light of these factors, it is not clear whether compliance with the specified actions has been met. JALI asked that we clarify the applicability either to note that the NPRM does not apply to airplanes on which a T/R is installed with a design change known as ‘‘ Commonality T/R, ’’ which is common to Model 777–300 series airplanes, or to change the