[Federal Register Volume 78, Number 136 (Tuesday, July 16, 2013)]
[Rules and Regulations]
[Pages 42415-42417]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2013-15963]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2013-0302; Directorate Identifier 2013-NM-019-AD;
Amendment 39-17503; AD 2013-13-15]
RIN 2120-AA64
Airworthiness Directives; the Boeing Company Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
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SUMMARY: We are superseding airworthiness directive (AD) 87-02-07,
which applied to all The Boeing Company Model 737-100 and -200 series
airplanes. AD 87-02-07 required replacement of certain underwing fuel
tank access covers with stronger, fire-resistant covers. This new AD
also requires inspecting fuel tank access doors to determine that
impact-resistant access doors are installed in the correct locations,
inspecting application of stencils and index markers of impact-
resistant access doors, doing corrective actions if necessary, revising
the maintenance program, and adding airplanes to the applicability.
This AD was prompted by reports of standard access doors installed
where impact-resistant access doors are required, and reports of
impact-resistant doors without stencils. We are issuing this AD to
prevent foreign object penetration of the wing tank, which could lead
to a fuel leak near ignition sources (engine, hot brakes), consequently
leading to a fuel-fed fire.
DATES: This AD is effective August 20, 2013.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in the AD as of August 20,
2013.
ADDRESSES: 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.com. You may review copies of the referenced service
information at the FAA, Transport Airplane Directate, 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: Suzanne Lucier, Aerospace Engineer,
Propulsion Branch, ANM-140S, FAA, Seattle Aircraft Certification
Office, 1601 Lind Avenue SW., Renton, Washington 98057-3356; phone:
425-917-6438; fax: 425-917-6590; email: [email protected].
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 to supersede AD 87-02-07, Amendment 39-5506 (Docket No. 86-NM-
175-AD; 52 FR 518, January 7, 1987), (``AD 87-02-07''). AD 87-02-07
applied to the specified products. The NPRM published in the Federal
Register on April 10, 2013 (78 FR 21279). The NPRM proposed to continue
to require replacement of certain underwing fuel tank access covers
with stronger, fire-resistant covers. The NPRM also proposed to require
inspecting fuel tank access doors to determine that impact-resistant
access doors are installed in the correct
[[Page 42416]]
locations, inspecting application of stencils and index markers of
impact-resistant access doors, doing corrective actions if necessary,
revising the maintenance program, and adding airplanes to the
applicability.
Comments
We gave the public the opportunity to participate in developing
this AD. We have considered the comment received.
Concurrence With NPRM (78 FR 21279, April 10, 2013)
Boeing stated that it concurs with the content of the NPRM (78 FR
21279, April 10, 2013).
Conclusion
We reviewed the relevant data, considered the comment received, and
determined that air safety and the public interest require adopting
this AD as proposed--except for minor editorial changes. We have
determined that these minor changes:
Are consistent with the intent that was proposed in the
NPRM (78 FR 21279, April 10, 2013) for correcting the unsafe condition;
and
Do not add any additional burden upon the public than was
already proposed in the NPRM (78 FR 21279, April 10, 2013).
Costs of Compliance
We estimate that this AD affects 128 airplanes of U.S. registry.
We estimate the following costs to comply with this AD:
Estimated Costs
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Cost per Cost on U.S.
Action Labor cost Parts cost product operators
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Inspect, replace, and apply stencil 8 work-hours x $85 per $0 $680 $87,040
and index marker. hour = $680.
Revise maintenance program............ 1 work-hour x $85 per 0 85 10,880
hour = $85.
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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 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
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 removing airworthiness directive (AD)
87-02-07, Amendment 39-5506 (Docket No. 86-NM-175-AD; 52 FR 518,
January 7, 1987), and adding the following new AD:
2013-13-15 The Boeing Company: Amendment 39-17503; Docket No. FAA-
2013-0302; Directorate Identifier 2013-NM-019-AD.
(a) Effective Date
This AD is effective August 20, 2013.
(b) Affected ADs
This AD supersedes AD 87-02-07, Amendment 39-5506 (Docket No.
86-NM-175-AD; 52 FR 518, January 7, 1987).
(c) Applicability
This AD applies to The Boeing Company Model 737-100, -200, -
200C, and -300 series airplanes, certified in any category, as
identified in Boeing Service Bulletin 737-28-1286, dated January 10,
2012.
(d) Subject
Joint Aircraft System Component (JASC)/Air Transport Association
(ATA) of America Code 28, Fuel.
(e) Unsafe Condition
This AD was prompted by reports of standard access doors
installed where impact-resistant access doors are required, and
reports of impact-resistant doors without stencils. We are issuing
this AD to prevent foreign object penetration of the wing tank,
which could lead to a fuel leak near ignition sources (engine, hot
brakes), consequently leading to a fuel-fed fire.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Inspection and Corrective Actions
Within 72 months after the effective date of this AD: Do a
general visual inspection of the left-wing and right-wing fuel tank
access doors to determine that impact-resistant access doors are
installed in the correct locations, and an inspection for proper
application of stencils and index markers of impact-resistant access
doors; and do all applicable corrective actions; in accordance with
the Accomplishment Instructions of Boeing Service Bulletin 737-28-
1286, dated January 10, 2012. Do all applicable corrective actions
before further flight.
(h) Maintenance Program Revision
Within 60 days after the effective date of this AD, revise the
maintenance program to incorporate Airworthiness Limitation (AWL)
57-AWL-01, Impact-Resistant Fuel Access Doors, as specified in
Section C.,
[[Page 42417]]
Airworthiness Limitations (AWLs)--Fuel Systems, of the Boeing 737-
100/200/200C/300/400/500 Airworthiness Limitations (AWLs) and
Certification Maintenance Requirements (CMRs), Document D6-38278-
CMR, Revision August 2012.
(i) No Alternative Critical Design Configuration Control Limitations
(CDCCLs)
After accomplishing the revision required by paragraph (h) of
this AD, no alternative CDCCLs may be used unless the CDCCLs are
approved as an alternative method of compliance (AMOC) in accordance
with the procedures specified in paragraph (j) of this AD.
(j) 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: [email protected].
(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 ACO to make
those findings. For a repair method to be approved, the repair must
meet the certification basis of the airplane and the approval must
specifically refer to this AD.
(k) Related Information
For more information about this AD, contact Suzanne Lucier,
Aerospace Engineer, Propulsion Branch, ANM-140S, FAA, Seattle
Aircraft Certification Office, 1601 Lind Avenue SW., Renton,
Washington 98057-3356; phone: 425-917-6438; fax: 425-917-6590;
email: [email protected].
(l) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the service information listed
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do
the actions required by this AD, unless the AD specifies otherwise.
(i) Boeing Service Bulletin 737-28-1286, dated January 10, 2012.
(ii) Boeing 737-100/200/200C/300/400/500 Airworthiness
Limitations (AWLs) and Certification Maintenance Requirements
(CMRs), Document D6-38278-CMR, Revision August 2012.
(3) For Boeing 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.com.
(4) You may view this service information at 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 view this 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/cfr/ibr-locations.html.
Issued in Renton, Washington, on June 21, 2013.
Jeffrey E. Duven,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2013-15963 Filed 7-15-13; 8:45 am]
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