[Federal Register Volume 72, Number 131 (Tuesday, July 10, 2007)]
[Proposed Rules]
[Pages 37475-37477]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: E7-13353]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2007-28664; Directorate Identifier 2007-NM-007-AD]
RIN 2120-AA64


Airworthiness Directives; Boeing Model 777-200, -200LR, -300, and 
-300ER Series Airplanes

AGENCY: Federal Aviation Administration (FAA), Department of 
Transportation (DOT).

ACTION: Notice of proposed rulemaking (NPRM).

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SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD) 
for all Boeing Model 777-200, -200LR, -300, and -300ER series 
airplanes. This proposed AD would require a one-time inspection to 
determine the material of the forward and aft gray water drain masts. 
For airplanes having composite gray water drain masts, this proposed AD 
would also require installation of a copper bonding jumper between a 
ground and the clamp on the tube of the forward and aft gray water 
composite drain masts. This proposed AD results from a report of 
charred insulation blankets and burned wires around the forward gray 
water composite drain mast found during an inspection of the forward 
cargo compartment on a Model 767-300F airplane. We are proposing this 
AD to prevent a fire near a composite drain mast and possible 
disruption of the electrical power system due to a lightning strike on 
a composite drain mast, which could result in the loss of several 
functions essential for safe flight.

DATES: We must receive comments on this proposed AD by August 24, 2007.

ADDRESSES: Use one of the following addresses to submit comments on 
this proposed AD.
     DOT Docket Web site: Go to http://dms.dot.gov and follow 
the instructions for sending your comments electronically.
     Government-wide rulemaking Web site: Go to http://www.regulations.gov and follow the instructions for sending your 
comments electronically.
     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.
     Fax: (202) 493-2251.
     Hand Delivery: Room W12-140 on the ground floor of the 
West Building, 1200 New Jersey Avenue SE., Washington, DC, between 9 
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
    Contact Boeing Commercial Airplanes, P.O. Box 3707, Seattle, 
Washington 98124-2207, for the service information identified in this 
proposed AD.

FOR FURTHER INFORMATION CONTACT: Dave Webber, Aerospace Engineer, Cabin 
Safety and Environmental Systems Branch, ANM-150S, FAA, Seattle 
Aircraft Certification Office, 1601 Lind Avenue, SW., Renton, 
Washington 98057-3356; telephone (425) 917-6451; fax (425) 917-6590.

SUPPLEMENTARY INFORMATION:

Comments Invited

    We invite you to submit any relevant written data, views, or 
arguments regarding this proposed AD. Send your comments to an address 
listed in the ADDRESSES section. Include the docket number ``FAA-2007-
28664; Directorate Identifier 2007-NM-007-AD'' at the beginning of your 
comments. We specifically invite comments on the overall regulatory, 
economic, environmental, and energy aspects of the proposed AD. We will 
consider all comments received by the closing date and may amend the 
proposed AD in light of those comments.
    We will post all comments we receive, without change, to http://dms.dot.gov, including any personal information you provide. We will 
also post a report summarizing each substantive verbal contact with FAA 
personnel concerning this proposed AD. Using the search function of 
that web site, anyone can find and read the comments in any of our 
dockets, including the name of the individual who sent the comment (or 
signed the comment on behalf of an association, business, labor union, 
etc.). You may review DOT's complete Privacy Act Statement in the 
Federal Register published on April 11, 2000 (65 FR 19477-78), or you 
may visit http://dms.dot.gov.

Examining the Docket

    You may examine the AD docket on the Internet at http://dms.dot.gov, or in person at the Docket Operations office between 9 
a.m. and 5 p.m., Monday through Friday, except Federal holidays. The 
Docket Operations office (telephone (800) 647-5527) is located on the 
ground floor of the West Building at the street address stated in the 
ADDRESSES section. Comments will be available in the AD docket shortly 
after the Docket Management System receives them.

Discussion

    We have received a report indicating that, during an inspection of 
the forward cargo compartment on a Model 767-300F airplane, an operator 
found charred insulation blankets and burned wires around the forward 
gray water composite drain mast. Additional charring on the insulation 
blankets was noticed several feet away along the routing of the drain 
mast's ground wire and power wires. Analysis of the damaged parts 
revealed that a lightning strike on the composite drain mast caused the 
damage to the wires and insulation blankets. This condition, if not 
corrected, could cause disruption of electrical power and fire and heat 
damage to equipment in the event of a lightning strike on the composite 
drain mast, which could result in the potential loss of several 
functions essential for safe flight.
    A design review of the gray water composite drain mast installation 
on Model 737NG, 757, 767, and 777

[[Page 37476]]

airplanes revealed that the installation of a heavier bonding jumper is 
necessary to provide adequate lightning protection to the gray water 
composite drain mast installation. The subject area on Model 777 
airplanes is almost identical to that on the affected Model 767-300F 
airplane. Therefore, Model 777 airplanes might be subject to the unsafe 
condition revealed on the Model 767-300F airplane. We are currently 
considering additional rulemaking to address the identified unsafe 
condition on Model 737NG, 757, and 767 airplanes.

Relevant Service Information

    We have reviewed Boeing Special Attention Service Bulletin 777-30-
0014, dated July 24, 2006. The service bulletin describes procedures 
for installing a 135-ampere copper bonding jumper between a ground and 
the clamp on the tube of the forward and aft gray water composite drain 
masts.
    Accomplishing the actions specified in the service information is 
intended to adequately address the unsafe condition.

FAA's Determination and Requirements of the Proposed AD

    We have evaluated all pertinent information and identified an 
unsafe condition that is likely to exist or develop on other airplanes 
of this same type design. For this reason, we are proposing this AD, 
which would require accomplishing the actions specified in the service 
information described previously, except as discussed under 
``Difference Between the Proposed AD and the Referenced Service 
Bulletin.''

Difference Between the Proposed AD and the Referenced Service Bulletin

    Operators should note that, although Model 777-200LR series 
airplanes are not included in the effectivity of Boeing Special 
Attention Service Bulletin 777-30-0014, dated July 24, 2006, this 
proposed AD is applicable to those airplanes. This difference has been 
coordinated with Boeing.

Costs of Compliance

    There are about 164 airplanes of the affected design in the 
worldwide fleet. The following table provides the estimated costs for 
U.S. operators to comply with this proposed AD.

                                                                     Estimated Costs
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                                                   Average
              Action                 Work hours   labor rate          Parts            Cost per airplane       Number of U.S.-           Fleet cost
                                                   per hour                                                  registered airplanes
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Inspection to determine gray water            1          $80  None.................  $80..................  20...................  $1,600.
 drain mast material.
Installation of bonding jumper....            4           80  Between $132 and       Between $452 and $594  Up to 20.............  Between $9,040 and
                                                               $274, depending on                                                   $11,880.
                                                               kit and number of
                                                               kits needed (1 or 2).
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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 have 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 that the 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.
    We prepared a regulatory evaluation of the estimated costs to 
comply with this proposed AD and placed it in the AD docket. See the 
ADDRESSES section for a location to examine the regulatory evaluation.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, 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 Federal Aviation Administration (FAA) amends Sec.  39.13 by 
adding the following new airworthiness directive (AD):

Boeing: Docket No. FAA-2007-28664; Directorate Identifier 2007-NM-
007-AD.

Comments Due Date

    (a) The FAA must receive comments on this AD action by August 
24, 2007.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to all Boeing Model 777-200, -200LR, -300, 
and -300ER series airplanes, certificated in any category.

Unsafe Condition

    (d) This AD results from a report of charred insulation blankets 
and burned wires around the forward gray water composite drain mast 
found during an inspection of the forward cargo compartment on a 
Model 767-300F airplane. We are issuing this AD to prevent a fire 
near a composite drain mast and

[[Page 37477]]

possible disruption of the electrical power system due to a 
lightning strike on a composite drain mast, which could result in 
the loss of several functions essential for safe flight.

Compliance

    (e) You are responsible for having the actions required by this 
AD performed within the compliance times specified, unless the 
actions have already been done.

Inspection To Determine Material of Gray Water Drain Mast

    (f) Within 60 months after the effective date of this AD, 
inspect the forward and aft gray water drain masts to determine 
whether the drain mast is made of aluminum or composite material. A 
review of airplane maintenance records is acceptable in lieu of this 
inspection if the material of the forward and aft gray water drain 
masts can be conclusively determined from that review.
    (1) For any aluminum gray water drain mast identified during the 
inspection or records check required by paragraph (f) of this AD, no 
further action is required by this AD for that drain mast only.
    (2) For any composite gray water drain mast identified during 
the inspection or records check required by paragraph (f) of this 
AD, do the actions specified in paragraph (g) of this AD.

Installation of Bonding Jumper

    (g) For any composite gray water drain mast identified during 
the inspection or records check required by paragraph (f) of this 
AD: Within 60 months after the effective date of this AD, install a 
135-ampere copper bonding jumper between a ground and the clamp on 
the tube of the gray water composite drain mast, in accordance with 
the Accomplishment instructions of Boeing Special Attention Service 
Bulletin 777-30-0014, dated July 24, 2006.

Installation of Bonding Jumper Not Necessary for Aluminum Drain Masts

    (h) For airplanes on which the forward composite drain mast has 
been replaced with an aluminum drain mast per Boeing Service 
Bulletin 777-38-0026: Installation of the bonding jumper specified 
in paragraph (g) of this AD is not required for the forward gray 
water drain mast, as specified in Part 1 of the Accomplishment 
Instructions of Boeing Special Attention Service Bulletin 777-30-
0014, dated July 24, 2006.

Alternative Methods of Compliance (AMOCs)

    (i)(1) The Manager, Seattle Aircraft Certification Office, FAA, 
has the authority to approve AMOCs for this AD, if requested in 
accordance with the procedures found in 14 CFR 39.19.
    (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 appropriate principal inspector (PI) in the FAA 
Flight Standards District Office (FSDO), or lacking a PI, your local 
FSDO.

    Issued in Renton, Washington, on June 26, 2007.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. E7-13353 Filed 7-9-07; 8:45 am]
BILLING CODE 4910-13-P