[Federal Register: March 24, 2008 (Volume 73, Number 57)]
[Rules and Regulations]
[Page 15397-15399]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr24mr08-4]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2008-0303; Directorate Identifier 2008-NM-047-AD;
Amendment 39-15441; AD 2008-06-29]
RIN 2120-AA64
Airworthiness Directives; Boeing Model 737-300, -400, and -500
Series Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; request for comments.
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SUMMARY: We are adopting a new airworthiness directive (AD) for all
Boeing Model 737-300, -400, and -500 series airplanes. This AD requires
repetitive inspections of the downstop assemblies on the main tracks of
the No. 2, 3, 4, and 5 slats and the inboard track of the No. 1 and 6
slats to verify if any parts are missing, damaged, or in the wrong
order. This AD also requires other specified actions, and related
investigative and corrective actions if necessary. This AD results from
reports of fuel leaking from a puncture in the slat track housing
(referred to as the ``slat can''). We are issuing this AD to detect and
correct loose or missing parts from the main slat track downstop
assemblies, which could puncture the slat can and result in a fuel leak
and consequent fire.
DATES: This AD is effective April 8, 2008.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of April 8,
2008.
We must receive comments on this AD by May 23, 2008.
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 AD, contact Boeing
Commercial Airplanes, P.O. Box 3707, Seattle, Washington 98124-2207.
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 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: Nancy Marsh, Aerospace Engineer,
Airframe Branch, ANM-120S, FAA, Seattle Aircraft Certification Office,
1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425)
917-6440; fax (425) 917-6590.
SUPPLEMENTARY INFORMATION;
Discussion
Boeing has notified us that it has received numerous reports of
fuel leaking from the slat track housing (referred to as the ``slat
can'') on Boeing Model 737-300, -400, and -500 series airplanes. In all
cases, there were no reports of a fire as a result of the fuel leaks on
these airplane models. In some of the reports, the fuel leak was caused
by loose or broken parts falling off the downstop assembly into the
slat can, which were then subsequently driven into the slat can by the
retracting slat track. This condition, if not corrected, could puncture
the slat can and result in a fuel leak and consequent fire.
Other Related Rulemaking
On August 28, 2007, we issued emergency AD 2007-18-52, amendment
39-15197, to address the same unsafe condition on all Model 737-600, -
700, -700C, -800, -900, and -900ER series airplanes. That AD was
published in the Federal Register on September 21, 2007 (72 FR 53928).
That AD requires repetitive detailed inspections of the slat track
downstop assemblies to verify that proper hardware is installed, one-
time torquing of the nut and bolt, and corrective actions if necessary.
That AD resulted from reports of parts coming off the main slat track
downstop assemblies and a resultant fire. That AD was issued to detect
and correct loose or missing parts from the main slat track downstop
assemblies, which could result in a fuel leak and consequent fire.
Because the main slat track downstop assemblies of Model 737
airplanes are similar in design to those of other Boeing airplane
models, we have been working with the manufacturer to evaluate its
remaining airplane models to determine if a similar unsafe condition
exists on them. As a result, we may consider additional rulemaking as
those evaluations are completed.
Relevant Service Information
We reviewed Boeing Alert Service Bulletin 737-57A1301, dated
February 5, 2008. The service bulletin describes procedures for doing
repetitive detailed inspections of the downstop assemblies on the main
tracks of the No. 2, 3, 4, and 5 slats and the inboard track of the No.
1 and 6 slats to verify if any parts are missing, damaged, or in the
wrong order. The service bulletin specifies that the downstop assembly
may be inspected using a borescope. The service bulletin also describes
procedures for doing other specified actions, and doing related
investigative and corrective actions if necessary. The other specified
actions include a one-time torquing of the nut of the downstop assembly
and a detailed inspection of the bolt to verify that the entire
chamfered portion of the bolt protrudes beyond the outer surface of the
nut. The related investigative action is a detailed inspection of the
inside of the slat can for loose parts and damage to the wall of the
slat can, which is done if any downstop assembly part is missing or
damaged. The corrective actions include the following:
Removing any loose downstop assembly part found in the
slat can.
Replacing any damaged slat can, or contacting Boeing for
repair information.
Replacing any missing or damaged downstop assembly part
with a new or serviceable part.
Removing and reinstalling the downstop assembly if any
downstop assembly parts are in the wrong order, or if the entire
chamfered portion of the bolt does not protrude beyond the outer
surface of the nut after it is torqued.
The service bulletin specifies doing the initial inspection within
90 days and repeating the inspection thereafter at intervals not to
exceed 4,500 flight
[[Page 15398]]
cycles. The service bulletin specifies doing the other specified
actions within 90 days. The service bulletin specifies doing the
related investigative and corrective actions before further flight
after certain findings.
FAA's Determination and Requirements of This AD
We are issuing 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(se) same type
design(s). This AD requires accomplishing the actions specified in the
service information described previously, except as discussed under
``Differences Between the AD and Service Bulletin.''
Differences Between the AD and Service Bulletin
For airplanes on which any downstop assembly part is missing or
damaged, the service bulletin specifies doing a related investigative
action--i.e., a detailed inspection of the inside of the slat can for
loose parts and damage to the wall of the slat can. However, this AD
allows operators to accomplish a borescope inspection of the inside of
the slat can instead of a detailed inspection. We have coordinated this
difference with Boeing.
The service bulletin specifies to contact the manufacturer for
instructions on how to repair certain conditions, but this AD would
require repairing those conditions in one of the following ways:
Using a method that we approve; or
Using data that meet the certification basis of the
airplane, and that have been approved by an Authorized Representative
for the Boeing Commercial Airplanes Delegation Option Authorization
Organization whom we have authorized to make those findings.
Clarification of Slat Can Replacement
Paragraph 3.B.5.a.(2) of the Accomplishment Instructions of the
service bulletin specifies to either replace any damaged slat can or
contact Boeing for repair information if any damaged slat can is found.
Paragraph (f)(3) of this AD specifies, in part, that if an operator
chooses to replace the damaged slat can instead of contacting Boeing
for repair information, the damaged slat can must be replaced with a
new slat can having the same part number.
Interim Action
We consider this AD interim action. The manufacturer is currently
developing a modification that will address the unsafe condition
identified in this AD. Once this modification is developed, approved,
and available, we might consider additional rulemaking.
FAA's Justification and Determination of the Effective Date
Loose or missing parts from the main slat track downstop assemblies
could puncture the slat can and result in a fuel leak and consequent
fire. Because of our requirement to promote safe flight of civil
aircraft and thus, the critical need to assure the structural integrity
of the main slat track downstop assemblies and the short compliance
time involved with this action, this AD must be issued immediately.
Because an unsafe condition exists that requires the immediate
adoption of this AD, we find that notice and opportunity for prior
public comment hereon are impracticable and that good cause exists for
making this amendment effective in less than 30 days.
Comments Invited
This AD is a final rule that involves requirements affecting flight
safety, and we did not provide you with notice and an opportunity to
provide your comments before it becomes effective. However, we invite
you to send any written data, views, or arguments about this AD. Send
your comments to an address listed under the ADDRESSES section. Include
``Docket No. FAA-2008-0303; Directorate Identifier 2008-NM-047-AD'' at
the beginning of your comments. We specifically invite comments on the
overall regulatory, economic, environmental, and energy aspects of this
AD. We will consider all comments received by the closing date and may
amend this 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 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
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), 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.
Adoption of the Amendment
0
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 adding the following new AD:
2008-06-29 Boeing: Amendment 39-15441. Docket No. FAA-2008-0303;
Directorate Identifier 2008-NM-047-AD.
Effective Date
(a) This airworthiness directive (AD) is effective April 8,
2008.
Affected ADs
(b) None.
[[Page 15399]]
Applicability
(c) This AD applies to all Boeing Model 737-300, -400, and -500
series airplanes, certificated in any category.
Unsafe Condition
(d) This AD results from reports of fuel leaking from a puncture
in the slat track housing (referred to as ``slat can''). We are
issuing this AD to detect and correct loose or missing parts from
the main slat track downstop assemblies, which could puncture the
slat can and result in a fuel leak and consequent fire.
Compliance
(e) Comply with this AD within the compliance times specified,
unless already done.
Repetitive Inspections and Corrective Actions
(f) At the applicable time specified in Table 1 of paragraph
1.E. of Boeing Alert Service Bulletin 737-57A1301, dated February 5,
2008, except as provided by paragraph (f)(1) of this AD: Do a
detailed inspection or borescope inspection of the downstop
assemblies on the main tracks of the No. 2, 3, 4, and 5 slats and
the inboard track of the No. 1 and 6 slats to verify if any parts
are missing, damaged, or in the wrong order; and do all the other
specified, related investigative, and corrective actions as
applicable; by accomplishing all of the applicable actions specified
in the Accomplishment Instructions of the service bulletin, except
as provided by paragraphs (f)(2) and (f)(3) of this AD. Repeat the
inspection thereafter at the applicable interval specified in Table
1 of paragraph 1.E. of the service bulletin. Do all applicable
related investigative and corrective actions before further flight.
(1) Where the service bulletin specifies counting the compliance
time from ``* * * the date on the service bulletin,'' this AD
requires counting the compliance time from the effective date of
this AD.
(2) For airplanes on which any downstop assembly part is missing
or damaged, a borescope inspection of the inside of the slat can for
loose parts and damage to the wall of the slat can may be
accomplished in lieu of the detailed inspection of the inside of the
slat can that is specified in the service bulletin.
(3) If any damaged slat can is found during any inspection
required by this AD: Before further flight, either replace the slat
can with a new slat can having the same part number or repair the
slat can using a method approved in accordance with the procedures
specified in paragraph (g) of this AD.
Alternative Methods of Compliance (AMOCs)
(g)(1) The Manager, Seattle Aircraft Certification Office (ACO),
FAA, Attn: Nancy Marsh, Aerospace Engineer, Airframe Branch, ANM-
120S, 1601 Lind Avenue, SW., Renton, Washington 98057-3356;
telephone (425) 917-6440; fax (425) 917-6590; has the authority to
approve AMOCs for this AD, if requested using 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.
(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 an
Authorized Representative for the Boeing Commercial Airplanes
Delegation Option Authorization Organization who 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.
Material Incorporated by Reference
(h) You must use Boeing Alert Service Bulletin 737-57A1301,
dated February 5, 2008, to do the actions required by this AD,
unless the AD specifies otherwise.
(1) The Director of the Federal Register approved the
incorporation by reference of this service information under 5
U.S.C. 552(a) and 1 CFR part 51.
(2) For service information identified in this AD, contact
Boeing Commercial Airplanes, P.O. Box 3707, Seattle, Washington
98124-2207.
(3) You may review copies of the service information
incorporated by reference at the FAA, Transport Airplane
Directorate, 1601 Lind Avenue SW., Renton, Washington; or 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/code_of_federal_
regulations/ibr_locations.html.
Issued in Renton, Washington, on March 11, 2008.
Stephen P. Boyd,
Assistant Manager, Transport Airplane Directorate, Aircraft
Certification Service.
[FR Doc. E8-5702 Filed 3-21-08; 8:45 am]
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