[Federal Register Volume 77, Number 38 (Monday, February 27, 2012)]
[Proposed Rules]
[Pages 11416-11418]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2012-4382]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2012-0183; Directorate Identifier 2011-NM-131-AD]
RIN 2120-AA64


Airworthiness Directives; The Boeing Company 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 The Boeing Company Model 737-600, -700, -700C, -800, -900, and 
-900ER series airplanes. This proposed AD was prompted by reports from 
the manufacturer that center overhead stowage (COS) boxes could fall 
from their supports under forward load levels less than the 9G forward 
load requirements as defined by Federal Aviation Regulations. This 
proposed AD would require modifying COS boxes by installing new 
brackets, stiffeners, and hardware as needed. We are proposing this AD 
to prevent detachment of COS boxes at forward load levels less than 9G 
during an emergency landing, which would cause injury to passengers 
and/or crew and could impede subsequent rapid evacuation.

DATES: We must receive comments on this proposed AD by April 12, 2012.

ADDRESSES: You may send comments, using the procedures found in 14 CFR 
11.43 and 11.45, by any of the following methods:
    <bullet<ls-thn-eq> Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments.
    <bullet> Fax: 202-493-2251.
    <bullet<ls-thn-eq> Mail: U.S. Department of Transportation, Docket 
Operations, M-

[[Page 11417]]

30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue 
SE., Washington, DC 20590.
    <bullet> 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 <a href="/cdn-cgi/l/email-protection#e9848cc78b868c8a8684a98b868c80878ec78a8684"><span class="__cf_email__" data-cfemail="e28f87cc808d87818d8fa2808d878b8c85cc818d8f">[email protected]</span></a>; 
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: Patrick Gillespie, Aerospace Engineer, 
Cabin Safety and Environmental Systems Branch, ANM-150S, FAA, Seattle 
Aircraft Certification Office (ACO), 1601 Lind Avenue SW., Renton, WA 
98057-3356; phone: 425-917-6429; fax: 425-917-6590; email: 
<a href="/cdn-cgi/l/email-protection#e2928396908b8189cc858b8e8e8791928b87a2848383cc858d94"><span class="__cf_email__" data-cfemail="99e9f8edebf0faf2b7fef0f5f5fceae9f0fcd9fff8f8b7fef6ef">[email protected]</span></a>.

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-2012-0183; 
Directorate Identifier 2011-NM-131-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 from the manufacturer that COS boxes could fall 
from their supports under forward load levels less than the 9G forward 
load requirements as defined by section 25.561 of the Federal Aviation 
Regulations (14 CFR 25.561). This condition, if not corrected, could 
result in detachment of COS boxes at forward load levels less than 9G 
during an emergency landing, which would cause injury to passengers 
and/or crew and could impede subsequent rapid evacuation.

Relevant Service Information

    We reviewed Boeing Special Attention Service Bulletin 737-25-1641, 
Revision 1, dated August 8, 2011. The service information describes 
procedures for modifying center overhead stowage boxes. The 
modification includes installing new brackets, stiffeners, and hardware 
(bolts, washers, and nuts) as needed.

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 this 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 affects 526 airplanes of U.S. 
registry.
    We estimate the following costs to comply with this proposed AD:

                                                 Estimated Costs
----------------------------------------------------------------------------------------------------------------
                                                                                    Cost per       Cost on U.S.
             Action                        Labor cost             Parts cost        product         operators
----------------------------------------------------------------------------------------------------------------
Modification....................  31 work-hours x $85 per              $6,118           $8,753       $4,604,078
                                   hour = $2,635.
----------------------------------------------------------------------------------------------------------------

    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

[[Page 11418]]

    (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-2012-0183; Directorate Identifier 
2011-NM-131-AD.

(a) Comments Due Date

    We must receive comments by April 12, 2012.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to The Boeing Company Model 737-600, -700, -
700C, -800, -900, and -900ER series airplanes, certificated in any 
category, as identified in Boeing Special Attention Service Bulletin 
737-25-1641, Revision 1, dated August 8, 2011.

(d) Subject

    Joint Aircraft System Component (JASC)/Air Transport Association 
(ATA) of America Code 25: Equipment/Furnishings.

(e) Unsafe Condition

    This AD was prompted by reports from the manufacturer that 
center overhead stowage (COS) boxes could fall from their supports 
under forward load levels less than the 9G forward load requirements 
as defined by Federal Aviation Regulations. We are issuing this AD 
to prevent detachment of COS boxes at forward load levels less than 
9G during an emergency landing, which would cause injury to 
passengers and/or crew and could impede subsequent rapid evacuation.

(f) Compliance

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

(g) Modification and Installation of Center Overhead Stowage Boxes

    Within 60 months after the effective date of this AD, modify the 
COS boxes in accordance with the Accomplishment Instructions of 
Boeing Special Attention Service Bulletin 737-25-1641, Revision 1, 
dated August 8, 2011.

(h) Credit for Previous Actions

    This paragraph provides credit for the modification required by 
paragraph (g) of this AD, if the modification was performed before 
the effective date of this AD using Boeing Special Attention Service 
Bulletin 737-25-1641, dated May 13, 2011.

(i) Alternative Methods of Compliance (AMOCs)

    (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. 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: <a href="/cdn-cgi/l/email-protection#0b32264a454626586e6a7f7f676e264a4844264a46444826596e7a7e6e787f784b6d6a6a256c647d"><span class="__cf_email__" data-cfemail="497064080704641a2c283d3d252c64080a06640804060a641b2c383c2c3a3d3a092f2828672e263f">[email protected]</span></a>.
    (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.
    (3) An AMOC that provides an acceptable level of safety may be 
used for any repair required by this AD if it is approved by the 
Boeing Commercial Airplanes Organization Designation Authorization 
(ODA) that has been authorized by the Manager, Seattle Aircraft 
Certification Office to make those findings.

(j) Related Information

    (1) For more information about this AD, contact Patrick 
Gillespie, Aerospace Engineer, Cabin Safety and Environmental 
Systems Branch, ANM-150S, FAA, Seattle ACO, 1601 Lind Avenue SW., 
Renton, WA 98057-3356; phone: 425-917-6429; fax: 425-917-6590; 
email: <a href="/cdn-cgi/l/email-protection#0f7f6e7b7d666c6421686663636a7c7f666a4f696e6e21686079"><span class="__cf_email__" data-cfemail="7e0e1f0a0c171d1550191712121b0d0e171b3e181f1f50191108">[email protected]</span></a>.
    (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; email 
<a href="/cdn-cgi/l/email-protection#b4d9d19ad6dbd1d7dbd9f4d6dbd1dddad39ad7dbd9"><span class="__cf_email__" data-cfemail="8ae7efa4e8e5efe9e5e7cae8e5efe3e4eda4e9e5e7">[email protected]</span></a>; 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 February 14, 2012.
Kalene C. Yanamura,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2012-4382 Filed 2-24-12; 8:45 am]
BILLING CODE 4910-13-P


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