[Federal Register Volume 81, Number 25 (Monday, February 8, 2016)]
[Proposed Rules]
[Pages 6475-6477]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2016-02193]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2016-0462; Directorate Identifier 2015-NM-144-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 a report of 
wire chafing damage, which caused an electrical arc to an adjacent 
hydraulic tube located on the forward bulkhead of the main landing gear 
(MLG) wheel well, resulting in a hole in a hydraulic tube and 
consequent total loss of system B hydraulic fluid. This proposed AD 
would require an inspection for chafing damage of wire bundles and a 
hydraulic tube in the right side of the MLG wheel well, and corrective 
action if necessary; and installation of clamps between the wire 
bundles and hydraulic tube. We are proposing this AD to prevent chafing 
damage, which could result in electrical arcing that can cause a hole 
in the hydraulic tube and consequent loss of hydraulic fluid, possibly 
resulting in a fire in the MLG wheel well.

DATES: We must receive comments on this proposed AD by March 24, 2016.

ADDRESSES: You may send comments, using the procedures found in 14 CFR 
11.43 and 11.45, by any of the following methods:
    <bullet> Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments.
    <bullet> Fax: 202-493-2251.
    <bullet> 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.
    <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 NPRM, contact Boeing 
Commercial Airplanes, Attention: Data & Services Management, P. O. Box 
3707, MC 2H-65, Seattle, WA 98124-2207; telephone 206-544-5000, 
extension 1; fax 206-766-5680; Internet https://www.myboeingfleet. You 
may view this referenced service information at the FAA, Transport 
Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For information 
on the availability of this material at the FAA, call 425-227-1221. It 
is also available on the Internet at http://www.regulations.gov by 
searching for and locating Docket No. FAA-2016-0462.

Examining the AD Docket

    You may examine the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016-
0462; 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: Sean J. Schauer, Aerospace Engineer, 
Systems and Equipment Branch, ANM-130S, FAA, Seattle Aircraft 
Certification Office (ACO), 1601 Lind Avenue SW., Renton, WA 98057-
3356; phone: 425-917-6479; fax: 425-917-6590; email: 
<a href="/cdn-cgi/l/email-protection#730016121d5d00101b12061601331512125d141c05"><span class="__cf_email__" data-cfemail="76051317185805151e170313043610171758111900">[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-2016-0462; 
Directorate Identifier 2015-NM-144-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 damage to wire W6128-0506-10. The wire 
had chafed and arced to an adjacent hydraulic tube located on the 
forward bulkhead of the MLG wheel well. The chafing and electrical arc 
created a small hole in a system B hydraulic tube and caused damage to 
the wire bundle, which resulted in a ground fault detection on the 
system A electrical motor-driven pump (EMDP). The small hole led to a 
total loss of system B hydraulic fluid and the ground fault resulted in 
removal of power from the system A EMDP and illumination of the system 
A EMDP low power light. An investigation found that there was not 
sufficient separation between the wire bundles W6128, W8122, and the 
adjacent hydraulic tube at that location. This condition, if not 
corrected, could result in electrical arcing that can cause

[[Page 6476]]

a hole in the hydraulic tube and consequent loss of hydraulic fluid, 
possibly resulting in a fire in the MLG wheel well.

Related Service Information Under 1 CFR Part 51

    We reviewed Boeing Alert Service Bulletin 737-29A1119, dated August 
4, 2015. The service information describes procedures for doing an 
inspection for chafing damage of the wire bundles and hydraulic tube in 
the right side of the MLG wheel well, corrective actions, and 
installation of clamps and an optional spacer between the wire bundles 
and hydraulic tube. This service information is reasonably available 
because the interested parties have access to it through their normal 
course of business or by the means identified in the ADDRESSES section.

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. For information on the 
procedures and compliance times, see this service information at http://www.regulations.gov by searching for and locating Docket No. FAA-2016-
0462.
    The phrase ``corrective actions'' is used in this proposed AD. 
``Corrective actions'' are actions that correct or address any 
condition found. Corrective actions in an AD could include, for 
example, repairs.

Costs of Compliance

    We estimate that this proposed AD affects 1,270 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
----------------------------------------------------------------------------------------------------------------
Inspection and Installation.......  2 work-hours x $85 per                 $9             $179         $227,330
                                     hour = $170.
----------------------------------------------------------------------------------------------------------------

    We have received no definitive data that would enable us to provide 
cost estimates for the on-condition actions specified in this proposed 
AD.

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

0
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]

0
2. The FAA amends Sec.  39.13 by adding the following new airworthiness 
directive (AD):

The Boeing Company: Docket No. FAA-2016-0462; Directorate Identifier 
2015-NM-144-AD.

(a) Comments Due Date

    We must receive comments by March 24, 2016.

(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 Alert Service Bulletin 737-
29A1119, dated August 4, 2015.

(d) Subject

    Air Transport Association (ATA) of America Code 29, Hydraulic 
power.

(e) Unsafe Condition

    This AD was prompted by a report of wire chafing damage, which 
caused an electrical arc to an adjacent hydraulic tube located on 
the forward bulkhead of the main landing gear (MLG) wheel well, 
resulting in a hole in a hydraulic tube and consequent total loss of 
system B hydraulic fluid. We are issuing this AD to prevent chafing 
damage, which could result in electrical arcing that can cause a 
hole in the hydraulic tube and consequent loss of hydraulic fluid, 
possibly resulting in a fire in the MLG wheel well.

(f) Compliance

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

(g) Inspection and Corrective Action and Clamp Installation

    Within 24 months after the effective date of this AD: Do the 
actions specified in paragraphs (g)(1) and (g)(2) of this AD:
    (1) Do a detailed inspection for chafing damage of the wire 
bundles and hydraulic tube in the right side of the MLG wheel well, 
and do all applicable corrective actions, in

[[Page 6477]]

accordance with the Accomplishment Instructions of Boeing Alert 
Service Bulletin 737-29A1119, dated August 4, 2015. Do all 
applicable corrective actions before further flight.
    (2) Install new clamps and an optional spacer between the wire 
bundles and hydraulic tube in the right side of the MLG wheel well, 
in accordance with the Accomplishment Instructions of Boeing Alert 
Service Bulletin 737-29A1119, dated August 4, 2015.

(h) 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 paragraph (i)(1) of this AD. 
Information may be emailed to: <a href="/cdn-cgi/l/email-protection#2e17036f6063037d4b4f5a5a424b036f6d61036f63616d037c4b5f5b4b5d5a5d6e484f4f00494158"><span class="__cf_email__" data-cfemail="043d29454a4929576165707068612945474b2945494b47295661757161777077446265652a636b72">[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, modification, or alteration 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 ACO, to make those findings. To be approved, the 
repair method, modification deviation, or alteration deviation must 
meet the certification basis of the airplane and the approval must 
specifically refer to this AD.

(i) Related Information

    (1) For more information about this AD, contact Sean J. Schauer, 
Aerospace Engineer, Systems and Equipment Branch, ANM-130S, FAA, 
Seattle Aircraft Certification Office (ACO), 1601 Lind Avenue SW., 
Renton, WA 98057-3356; phone: 425-917-6479; fax: 425-917-6590; 
email: <a href="/cdn-cgi/l/email-protection#097a6c6867277a6a61687c6c7b496f6868276e667f"><span class="__cf_email__" data-cfemail="b8cbddd9d696cbdbd0d9cdddcaf8ded9d996dfd7ce">[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, WA 98124-2207; telephone 206-544-
5000, extension 1; fax 206-766-5680; Internet https://www.myboeingfleet. You may view this referenced service information 
at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., 
Renton, WA. For information on the availability of this material at 
the FAA, call 425-227-1221.

    Issued in Renton, Washington, on January 27, 2016.
Michael Kaszycki,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2016-02193 Filed 2-5-16; 8:45 am]
 BILLING CODE 4910-13-P


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