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[Federal Register Volume 75, Number 129 (Wednesday, July 7, 2010)]
[Proposed Rules]
[Pages 38945-38947]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2010-16517]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2010-0678; Directorate Identifier 2010-NM-020-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).

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SUMMARY: We propose to adopt a new airworthiness directive (AD) for 
certain Model 777-200 and -300 series airplanes. This proposed AD would 
require installing new operational software in the cabin management 
system, and loading new software into the mass memory card. This 
proposed AD results from an in-flight entertainment (IFE) systems 
review. We are proposing this AD to ensure that the flightcrew is able 
to turn off electrical power to the IFE system and other non-essential 
electrical systems through a switch in the flight compartment in the 
event of smoke or flames. In the event of smoke or flames in the 
airplane flight deck or passenger cabin, the flightcrew's inability to 
turn off electrical power to the IFE system and other non-essential 
electrical systems could result in the inability to control smoke or 
flames in the airplane flight deck or passenger cabin during a non-
normal or emergency situation.

DATES: We must receive comments on this proposed AD by August 23, 2010.

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 W12-140, 1200 New 
Jersey Avenue, SE., Washington, DC 20590, 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; 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 (telephone 800-647-5527) is in the 
ADDRESSES section. Comments will be available in the AD docket shortly 
after receipt.

FOR FURTHER INFORMATION CONTACT: Joe Salameh, Aerospace Engineer, 
Systems and Equipment Branch, ANM-130S, FAA, Seattle Aircraft 
Certification Office, 1601 Lind Avenue, SW., Renton, Washington 98057-
3356; telephone (425) 917-6454; fax (425) 917-6590.

SUPPLEMENTARY INFORMATION: 

Comments Invited

    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-2010-0678; 
Directorate Identifier 2010-NM-020-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

    In response to numerous reports of smoke or flames in the passenger 
cabin of various models of transport category airplanes, we conducted a 
comprehensive in-flight entertainment (IFE) systems review. Earlier 
investigation of the reports had revealed that the source of the smoke 
and flames

[[Page 38946]]

was from cabin IFE system components, including electronic seat boxes 
mounted under passenger seats, IFR wirings, IFE monitors, cabin 
lighting, wall outlets, and other non-essential cabin electrical 
systems.
    The systems review disclosed that in order to minimize the risk of 
smoke or flames in the passenger cabin, a switch is needed in the 
flight compartment to enable the flightcrew to turn off electrical 
power to the IFE system and other non-essential electrical systems. In 
the event of smoke or flames in the airplane flight deck or passenger 
cabin, the flightcrew's inability to turn off power to the IFE system 
and other non-essential electrical systems, if not corrected, could 
result in the inability to control smoke or flames in the airplane 
flight deck or passenger cabin during a non-normal or emergency 
situation.

Relevant Service Information

    We have reviewed Boeing Service Bulletin 777-23-0175, Revision 2, 
dated October 12, 2006. The service bulletin describes procedures for 
installing new operational software in the cabin management system as 
follows:
     At the cabin system control panel (CSCP), remove the 
installed mass memory card (MMC) 285W0925-1 or 285W0925-2.
     Install the new MMC 285W0925-3.
     Install a new cabin system management unit (CSMU) software 
part number 2313-BCE-01T-03.
     Install a new cabin area control panel (CACP) software 
part number 2313-BCE-01U-02.
     Install a new zone management unit (ZMU) software part 
number 2374-BCE-021-02.
     Install a new overhead electronics unit (OEU) operational 
software (OPS) (12 port) part number 2310-BCE-01V-02, if the airplane 
configuration has OEU hardware 285W0029-5 installed.
     Install a new configuration database (CDB).
     Install the new CDB to the cabin service system.
    Boeing Service Bulletin 777-23-0175, Revision 2, dated October 12, 
2006, specifies prior or concurrent accomplishment of Boeing Component 
Service Bulletin 285W0925-23-02, dated July 11, 2002, which describes 
procedures for loading the new cabin services system central storage 
device software and CSCP OPS into the MMC.

FAA's Determination and Requirements of This Proposed AD

    We are proposing this AD because we evaluated all relevant 
information and determined the unsafe condition described previously is 
likely to exist or develop in other products of these same type 
designs. This proposed AD would require accomplishing the actions 
specified in the service information described previously.

Costs of Compliance

    We estimate that this proposed AD would affect 59 airplanes of U.S. 
registry. The following table provides the estimated costs for U.S. 
operators to comply with this proposed AD.

                                                                 Table--Estimated Costs
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                                                                                                                          Number of U.S.-
                         Action                             Work hours     Average labor       Parts         Cost per       registered      Fleet cost
                                                                           rate per hour                      product        airplanes
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Modification--New software in the cabin management                     4             $85              $0            $340              59         $20,060
 system.................................................
Concurrent modification--New software in the mass memory               1              85               0              85              59           5,015
 card...................................................
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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.
    You can find our regulatory evaluation and the estimated costs of 
compliance in the AD Docket.

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 AD:

The Boeing Company: Docket No. FAA-2010-0678; Directorate Identifier 
2010-NM-020-AD.

Comments Due Date

    (a) We must receive comments by August 23, 2010.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to The Boeing Company Model 777-200 and -300 
series airplanes, certificated in any category; as

[[Page 38947]]

identified in Boeing Service Bulletin 777-23-0175, Revision 2, dated 
October 12, 2006.

Subject

    (d) Air Transport Association (ATA) of America Code 23: 
Communications.

Unsafe Condition

    (e) This AD results from an in-flight entertainment (IFE) 
systems review. We are proposing this AD to minimize the risk of 
smoke or flames in the passenger cabin by installing a switch in the 
flight compartment to enable the flightcrew to turn off electrical 
power to the IFE system and other non-essential electrical systems. 
In the event of smoke or flames in the airplane flight deck or 
passenger cabin, the flightcrew's inability to turn off electrical 
power to the IFE system and other non-essential electrical systems 
could result in the inability to control smoke or flames in the 
airplane flight deck or passenger cabin during a non-normal or 
emergency situation.

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.

Modification

    (g) Within 60 months after the effective date of this AD: 
Replace the mass memory card (MMC) with a new MMC; install new cabin 
system management unit (CSMU) software, cabin area control panel 
(CACP) software, and new zone management unit (ZMU) software; 
install new overhead electronics unit (OEU) operational program 
software, if applicable; install a new configuration database (CDB); 
and install the new CDB to the cabin service system; in accordance 
with the Accomplishment Instructions of Boeing Service Bulletin 777-
23-0175, Revision 2, dated October 12, 2006.

Concurrent Requirement

    (h) Prior to or concurrently with accomplishing the requirements 
of paragraph (g) of this AD, load the new cabin services system 
central storage device software and cabin system control panel 
operational software into the MMC, in accordance with Boeing 
Component Service Bulletin 285W0925-23-02, dated July 11, 2002.

Alternative Methods of Compliance (AMOCs)

    (i)(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: Joe Salameh, Aerospace Engineer, Systems and Equipment Branch, 
ANM-130S, FAA, Seattle Aircraft Certification Office, 1601 Lind 
Avenue, SW., Renton, Washington 98057-3356; telephone (425) 917-
6454; 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.

    Issued in Renton, Washington, on June 29, 2010.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2010-16517 Filed 7-6-10; 8:45 am]
BILLING CODE 4910-13-P
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