AD 2007-13-13
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Embraer S.A. | ERJ 170-100 LR | Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) ERJ 170 Airplanes |
| aircraft | Embraer S.A. | ERJ 170-100 SE | Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) ERJ 170 Airplanes |
| aircraft | Embraer S.A. | ERJ 170-100 STD | Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) ERJ 170 Airplanes |
| aircraft | Embraer S.A. | ERJ 170-100 SU | Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) ERJ 170 Airplanes |
| aircraft | Embraer S.A. | ERJ 170-200 LR | Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) ERJ 170 Airplanes |
| aircraft | Embraer S.A. | ERJ 170-200 STD | Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) ERJ 170 Airplanes |
| aircraft | Embraer S.A. | ERJ 170-200 SU | Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) ERJ 170 Airplanes |
Unsafe Condition
Obstruction at the cargo compartment fire extinguisher system drier metering unit (DMU) inlet, affecting system effectiveness and making fire extinguishing capability inadequate in case of a fire.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Install a debris strainer at the DMU inlet, in accordance with EMBRAER Service Bulletin 170-26-0002, dated November 11, 2005.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 700 flight hours after the effective date of this AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
EMBRAER Model ERJ 170-100 LR, -100 STD, -100 SE, -100 SU, -200 LR, -200 STD, and -200 SU airplanes, as identified in EMBRAER Service Bulletin 170-26-0002, dated November 11, 2005; certificated in any category.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by an airworthiness authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as an obstruction at the cargo compartment fire extinguisher system drier metering unit (DMU) inlet, affecting the system effectiveness and, consequently, making the fire extinguishing capability at those compartments inadequate should a fire erupt. We are issuing this AD to require actions to correct the unsafe condition on these products.
Document Text
Show stored source text (verify against official source)
[Federal Register Volume 72, Number 125 (Friday, June 29, 2007)]
[Rules and Regulations]
[Pages 35645-35647]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: E7-12221]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2007-27508; Directorate Identifier 2006-NM-252-AD;
Amendment 39-15117; AD 2007-13-13]
RIN 2120-AA64
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A.
(EMBRAER) ERJ 170 Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
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SUMMARY: We are adopting a new airworthiness directive (AD) for the
products listed above. This AD results from mandatory continuing
airworthiness information (MCAI) issued by an airworthiness authority
of another country to identify and correct an unsafe condition on an
aviation product. The MCAI describes the unsafe condition as an
obstruction at the cargo compartment fire extinguisher system drier
metering unit (DMU) inlet, affecting the system effectiveness and,
consequently, making the fire extinguishing capability at those
compartments inadequate should a fire erupt. We are issuing this AD to
require actions to correct the unsafe condition on these products.
DATES: This AD becomes effective August 3, 2007.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of August 3,
2007.
ADDRESSES: You may examine the AD docket on the Internet at <a href="http://dms.dot.gov">http://dms.dot.gov</a> or in person at the U.S. Department of Transportation,
Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200
New Jersey Avenue, SE., Washington, DC.
FOR FURTHER INFORMATION CONTACT: Todd Thompson, Aerospace Engineer,
International Branch, ANM-116, FAA, Transport Airplane Directorate,
1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425)
227-1175; fax (425) 227-1149.
[[Page 35646]]
SUPPLEMENTARY INFORMATION:
Discussion
The FAA is implementing a new process for streamlining the issuance
of ADs related to MCAI. This streamlined process will allow us to adopt
MCAI safety requirements in a more efficient manner and will reduce
safety risks to the public. This process continues to allow all FAA AD
issuance processes to meet legal, economic, Administrative Procedure
Act, and Federal Register requirements. We also continue to meet our
technical decision-making responsibilities to identify and correct
unsafe conditions on U.S.-certificated products.
This AD references the MCAI and related service information that we
considered in forming the engineering basis to correct the unsafe
condition. The AD contains text copied from the MCAI and for this
reason might not follow our plain language principles.
We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 to include an AD that would apply to the specified products.
That NPRM was published in the Federal Register on March 12, 2007 (72
FR 10947). That NPRM proposed to require installation of a debris
strainer at the drier metering unit (DMU) inlet. The MCAI states that
it has been found the occurrence of one case of obstruction at the
cargo compartment fire extinguisher system DMU inlet, affecting the
system effectiveness and, consequently, making the fire extinguishing
capability at those compartments inadequate should a fire erupt.
Comments
We gave the public the opportunity to participate in developing
this AD. We considered the comment received.
Request To Revise Applicability
The airplane manufacturer, EMBRAER, requests that we change the
proposed applicability to refer to certain Model ERJ 170 airplanes
identified in EMBRAER Service Bulletin 170-26-0002, dated November 11,
2005.
We agree to revise the applicability. The service bulletin
identifies only those airplanes that have an affected DMU installed. We
have revised paragraph (c) of this AD to reference the service
bulletin. We have coordinated this change with Ag[ecirc]ncia Nacional
de Avia[ccedil][atilde]o Civil (ANAC).
Conclusion
We reviewed the available data, including the comment received, and
determined that air safety and the public interest require adopting the
AD with the change described previously. We determined that this change
will not increase the economic burden on any operator or increase the
scope of the AD.
Differences Between This AD and the MCAI or Service Information
We have reviewed the MCAI and related service information and, in
general, agree with their substance. But we might have found it
necessary to use different words from those in the MCAI to ensure the
AD is clear for U.S. operators and is enforceable in a U.S. court of
law. In making these changes, we do not intend to differ substantively
from the information provided in the MCAI and related service
information.
We might also have required different actions in this AD from those
in the MCAI in order to follow our FAA policies. Any such differences
are described in a separate paragraph of the AD. These requirements, if
any, take precedence over the actions copied from the MCAI.
Costs of Compliance
We estimate that this AD will affect 75 products of U.S. registry.
We also estimate that it will take about 4 work-hours per product to
comply with this AD. The average labor rate is $80 per work-hour.
Required parts will cost about $0 per product. Where the service
information lists required parts costs that are covered under warranty,
we have assumed that there will be no charge for these parts. As we do
not control warranty coverage for affected parties, some parties may
incur costs higher than estimated here. Based on these figures, we
estimate the cost of this AD to the U.S. operators to be $24,000, or
$320 per product.
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 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.
We prepared a regulatory evaluation of the estimated costs to
comply with this AD and placed it in the AD Docket.
Examining the AD Docket
You may examine the AD docket on the Internet at <a href="http://dms.dot.gov">http://dms.dot.gov</a>; or in person at the Docket Operations office between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD
docket contains the NPRM, the regulatory evaluation, any comments
received, and other information. The street address for the Docket
Operations office (telephone (800) 647-5527) is in the ADDRESSES
section. Comments will be available in the AD docket shortly after
receipt.
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:
2007-13-13 Empresa Brasileira De Aeronautica S.A. (EMBRAER):
Amendment 39-15117. Docket No. FAA-2007-27508; Directorate
Identifier 2006-NM-252-AD.
[[Page 35647]]
Effective Date
(a) This airworthiness directive (AD) becomes effective August
3, 2007.
Affected ADs
(b) None.
Applicability
(c) This AD applies to EMBRAER Model ERJ 170-100 LR, -100 STD, -
100 SE, -100 SU, -200 LR, -200 STD, and -200 SU airplanes, as
identified in EMBRAER Service Bulletin 170-26-0002, dated November
11, 2005; certificated in any category.
Reason
(d) The MCAI states that it has been found the occurrence of one
case of obstruction at the cargo compartment fire extinguisher
system drier metering unit (DMU) inlet, affecting the system
effectiveness and, consequently, making the fire extinguishing
capability at those compartments inadequate should a fire erupt. The
MCAI requires installation of a debris strainer at the DMU inlet.
Actions and Compliance
(e) Unless already done, do the following actions. Within 700
flight hours after the effective date of this AD, install a debris
strainer at the DMU inlet, in accordance with the detailed
instructions and procedures described in EMBRAER Service Bulletin
170-26-0002, dated November 11, 2005.
FAA AD Differences
Note: This AD differs from the MCAI and/or service information
as follows: No Differences.
Other FAA AD Provisions
(f) The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
has the authority to approve AMOCs for this AD, if requested using
the procedures found in 14 CFR 39.19. Send information to ATTN: Todd
Thompson, Aerospace Engineer, International Branch, ANM-116, FAA,
Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton,
Washington 98057-3356; telephone (425) 227-1175; fax (425) 227-1149.
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.
(2) Airworthy Product: For any requirement in this AD to obtain
corrective actions from a manufacturer or other source, use these
actions if they are FAA-approved. Corrective actions are considered
FAA-approved if they are approved by the State of Design Authority
(or their delegated agent). You are required to assure the product
is airworthy before it is returned to service.
(3) Reporting Requirements: For any reporting requirement in
this AD, under the provisions of the Paperwork Reduction Act, the
Office of Management and Budget (OMB) has approved the information
collection requirements and has assigned OMB Control Number 2120-
0056.
Related Information
(g) Refer to MCAI Brazilian Airworthiness Directive 2006-01-03,
effective February 7, 2006; and EMBRAER Service Bulletin 170-26-
0002, dated November 11, 2005; for related information.
Material Incorporated by Reference
(h) You must use EMBRAER Service Bulletin 170-26-0002, dated
November 11, 2005, 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
Empresa Brasileira de Aeronautica S.A. (EMBRAER), P.O. Box 343--CEP
12.225, Sao Jose dos Campos--SP, Brazil.
(3) You may review copies 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: <a href="http://www.archives.gov/federal-register/cfr/ibr-locations.html">http://www.archives.gov/federal-register/cfr/ibr-locations.html</a>.
Issued in Renton, Washington, on June 18, 2007.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E7-12221 Filed 6-28-07; 8:45 am]
BILLING CODE 4910-13-P
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