AD 2013-03-13
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Embraer S.A. | ERJ 170-100 LR | Airworthiness Directives; Embraer S.A. Airplanes |
| aircraft | Embraer S.A. | ERJ 170-100 SE | Airworthiness Directives; Embraer S.A. Airplanes |
| aircraft | Embraer S.A. | ERJ 170-100 STD | Airworthiness Directives; Embraer S.A. Airplanes |
| aircraft | Embraer S.A. | ERJ 170-100 SU | Airworthiness Directives; Embraer S.A. Airplanes |
| aircraft | Embraer S.A. | ERJ 170-200 LR | Airworthiness Directives; Embraer S.A. Airplanes |
| aircraft | Embraer S.A. | ERJ 170-200 STD | Airworthiness Directives; Embraer S.A. Airplanes |
| aircraft | Embraer S.A. | ERJ 170-200 SU | Airworthiness Directives; Embraer S.A. Airplanes |
| aircraft | Embraer S.A. | ERJ 190-100 ECJ | Airworthiness Directives; Embraer S.A. Airplanes |
| aircraft | Embraer S.A. | ERJ 190-100 IGW | Airworthiness Directives; Embraer S.A. Airplanes |
| aircraft | Embraer S.A. | ERJ 190-100 LR | Airworthiness Directives; Embraer S.A. Airplanes |
| aircraft | Embraer S.A. | ERJ 190-100 STD | Airworthiness Directives; Embraer S.A. Airplanes |
| aircraft | Embraer S.A. | ERJ 190-200 IGW | Airworthiness Directives; Embraer S.A. Airplanes |
| aircraft | Embraer S.A. | ERJ 190-200 LR | Airworthiness Directives; Embraer S.A. Airplanes |
| aircraft | Embraer S.A. | ERJ 190-200 STD | Airworthiness Directives; Embraer S.A. Airplanes |
Unsafe Condition
Reports of the cockpit door falling off the hinges when it is being opened or closed.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace the striker and quick-release pin of the passive lock of the cockpit door. Replace the upper and lower hinges of the cockpit door.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 1,500 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 S.A. Model ERJ 170 and ERJ 190 airplanes, as identified in specific service bulletins.
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 certain Embraer S.A. Model ERJ 170 and ERJ 190 airplanes. This AD was prompted by reports of the cockpit door falling off the hinges when it is being opened or closed. This AD requires replacing the striker and quick- release pin of the passive lock of the cockpit door, and replacing the upper and lower hinges of the cockpit door. We are issuing this AD to prevent the cockpit door from falling off the hinges, which could cause injury to airplane occupants.
Applicability Source Text
Show captured applicability text from the source AD
(c) Applicability
This AD applies to the airplanes identified in paragraphs (c)(1)
and (c)(2) of this AD.
(1) Embraer S.A. Model ERJ 170-100 LR, -100 STD, -100 SE., and -
100 SU airplanes;
[[Page 9802]]
and Model ERJ 170-200 LR, -200 SU, and -200 STD airplanes;
certificated in any category; as identified in EMBRAER Service
Bulletin 170-52-0055, Revision 01, dated August 1, 2011.
(2) Embraer S.A. Model ERJ 190-100 STD, -100 LR, -100 ECJ, and -
100 IGW airplanes; and Model ERJ 190-200 STD, -200 LR, and -200 IGW
airplanes; certificated in any category; as identified in EMBRAER
Service Bulletin 190-52-0038, Revision 01, dated August 1, 2011, and
EMBRAER Service Bulletin 190LIN-52-0020, dated August 1, 2011.
Document Text
Show stored source text (verify against official source)
[Federal Register Volume 78, Number 29 (Tuesday, February 12, 2013)]
[Rules and Regulations]
[Pages 9800-9802]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2013-02902]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2012-1223; Directorate Identifier 2012-NM-154-AD;
Amendment 39-17348; AD 2013-03-13]
RIN 2120-AA64
Airworthiness Directives; Embraer S.A. Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: We are adopting a new airworthiness directive (AD) for certain
[[Page 9801]]
Embraer S.A. Model ERJ 170 and ERJ 190 airplanes. This AD was prompted
by reports of the cockpit door falling off the hinges when it is being
opened or closed. This AD requires replacing the striker and quick-
release pin of the passive lock of the cockpit door, and replacing the
upper and lower hinges of the cockpit door. We are issuing this AD to
prevent the cockpit door from falling off the hinges, which could cause
injury to airplane occupants.
DATES: This AD becomes effective March 19, 2013.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of March 19,
2013.
ADDRESSES: You may examine the AD docket on the Internet at <a href="http://www.regulations.gov">http://www.regulations.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: Cindy Ashforth, Aerospace Engineer,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
1601 Lind Avenue SW., Renton, WA 98057-3356; telephone (425) 227-2768;
fax (425) 227-1149.
SUPPLEMENTARY INFORMATION:
Discussion
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 December 6, 2012 (77
FR 72776). That NPRM proposed to correct an unsafe condition for the
specified products. The Mandatory Continuing Airworthiness Information
(MCAI) states:
This [Ag[ecirc]ncia Nacional de Avia[ccedil][atilde]o Civil
(ANAC)] AD was prompted by reports of cockpit door falling off the
hinges when it is being opened or closed. If not corrected, this
condition may cause injury to the occupants.
* * * * *
You may obtain further information by examining the MCAI in the AD
docket.
Comments
We gave the public the opportunity to participate in developing
this AD. We considered the comment received. The Air Line Pilots
Association, International (ALPA) supports the intent of the NPRM (77
FR 72776, December 6, 2012).
Conclusion
We reviewed the available data, including the comment received, and
determined that air safety and the public interest require adopting the
AD as proposed--except for minor editorial changes. We have determined
that these minor changes:
<bullet> Are consistent with the intent that was proposed in the
NPRM (77 FR 72776, December 6, 2012) for correcting the unsafe
condition; and
<bullet> Do not add any additional burden upon the public than was
already proposed in the NPRM (77 FR 72776, December 6, 2012).
Costs of Compliance
We estimate that this AD will affect 253 products of U.S. registry.
We also estimate that it will take about 6 work-hours per product to
comply with the basic requirements of this AD. The average labor rate
is $85 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 $129,030 or $510 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 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.
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://www.regulations.gov">http://www.regulations.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 (77 FR 72776, December 6,
2012), 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
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:
2013-03-13 Embraer S.A.: Amendment 39-17348. Docket No. FAA-2012-
1223; Directorate Identifier 2012-NM-154-AD.
(a) Effective Date
This airworthiness directive (AD) becomes effective March 19,
2013.
(b) Affected ADs
None.
(c) Applicability
This AD applies to the airplanes identified in paragraphs (c)(1)
and (c)(2) of this AD.
(1) Embraer S.A. Model ERJ 170-100 LR, -100 STD, -100 SE., and -
100 SU airplanes;
[[Page 9802]]
and Model ERJ 170-200 LR, -200 SU, and -200 STD airplanes;
certificated in any category; as identified in EMBRAER Service
Bulletin 170-52-0055, Revision 01, dated August 1, 2011.
(2) Embraer S.A. Model ERJ 190-100 STD, -100 LR, -100 ECJ, and -
100 IGW airplanes; and Model ERJ 190-200 STD, -200 LR, and -200 IGW
airplanes; certificated in any category; as identified in EMBRAER
Service Bulletin 190-52-0038, Revision 01, dated August 1, 2011, and
EMBRAER Service Bulletin 190LIN-52-0020, dated August 1, 2011.
(d) Subject
Air Transport Association (ATA) of America Code 52, Doors.
(e) Reason
This AD was prompted by reports of the cockpit door falling off
the hinges when it is being opened or closed. We are issuing this AD
to prevent the cockpit door from falling off the hinges, which could
cause injury to airplane occupants.
(f) Compliance
You are responsible for having the actions required by this AD
performed within the compliance times specified, unless the actions
have already been done.
(g) Required Actions and Compliance Time
Within 1,500 flight hours after the effective date of this AD,
do the actions specified in paragraphs (g)(1) and (g)(2) of this AD.
(1) Replace the striker and quick-release pin of the passive
lock of the cockpit door, in accordance with Part I of the
Accomplishment Instructions of the applicable service bulletin
specified in paragraph (g)(1)(i), (g)(1)(ii), or (g)(1)(iii) of this
AD.
(i) EMBRAER Service Bulletin 170-52-0055, Revision 01, dated
August 1, 2011 (for Model ERJ 170 airplanes).
(ii) EMBRAER Service Bulletin 190-52-0038, Revision 01, dated
August 1, 2011 (for Model ERJ 190 airplanes except for Model ERJ
190-100 ECJ airplanes).
(iii) EMBRAER Service Bulletin 190LIN-52-0020, dated August 1,
2011 (for Model ERJ 190-100 ECJ airplanes).
(2) Replace the cockpit door upper and lower hinges in
accordance with Part III of the Accomplishment Instructions of the
applicable service bulletin specified in paragraph (g)(2)(i),
(g)(2)(ii), or (g)(2)(iii) of this AD.
(i) EMBRAER Service Bulletin 170-52-0055, Revision 01, dated
August 1, 2011 (for Model ERJ 170 airplanes).
(ii) EMBRAER Service Bulletin 190-52-0038, Revision 01, dated
August 1, 2011 (for Model ERJ 190 airplanes except for Model ERJ
190-100 ECJ airplanes).
(iii) EMBRAER Service Bulletin 190LIN-52-0020, dated August 1,
2011 (for Model ERJ 190-100 ECJ airplanes).
(h) Credit for Previous Actions
This paragraph provides credit for actions required by paragraph
(g)(1) of this AD, if those actions were performed before the
effective date of this AD using EMBRAER Service Bulletin 170-52-
0055, dated February 10, 2011 (for Model ERJ 170 airplanes); or
EMBRAER Service Bulletin 190-52-0038, dated February 10, 2011 (for
Model ERJ 190 airplanes except for Model ERJ 190-100 ECJ airplanes);
which are not incorporated by reference in this AD.
(i) Other FAA AD Provisions
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. 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 International Branch, send it to ATTN: Cindy
Ashforth, Aerospace Engineer, International Branch, ANM-116,
Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton,
WA 98057-3356; telephone (425) 227-2768; fax (425) 227-1149.
Information may be emailed to: <a href="/cdn-cgi/l/email-protection#b1889cf0fffc9c8080879cf0fcfef29ce3f4e0e4f4e2e5e2f1d7d0d09fd6dec7"><span class="__cf_email__" data-cfemail="b88195f9f6f59589898e95f9f5f7fb95eafde9edfdebecebf8ded9d996dfd7ce">[email protected]</span></a>.
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. The AMOC approval letter must specifically reference this
AD.
(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.
(j) Related Information
Refer to MCAI Brazilian Airworthiness Directives 2012-08-02 and
2012-08-03, both effective September 5, 2012, and the service
bulletins identified in paragraphs (j)(1), (j)(2), and (j)(3) of
this AD, for related information.
(1) EMBRAER Service Bulletin 170-52-0055, Revision 01, dated
August 1, 2011.
(2) EMBRAER Service Bulletin 190-52-0038, Revision 01, dated
August 1, 2011.
(3) EMBRAER Service Bulletin 190LIN-52-0020, dated August 1,
2011.
(k) 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) EMBRAER Service Bulletin 170-52-0055, Revision 01, dated
August 1, 2011.
(ii) EMBRAER Service Bulletin 190-52-0038, Revision 01, dated
August 1, 2011.
(iii) EMBRAER Service Bulletin 190LIN-52-0020, dated August 1,
2011.
(3) For service information identified in this AD contact
Embraer S.A., Technical Publications Section (PC 060), Av.
Brigadeiro Faria Lima, 2170--Putim--12227-901 S[atilde]o Jose dos
Campos--SP--BRASIL; telephone +55 12 3927-5852 or +55 12 3309-0732;
fax +55 12 3927-7546; email <a href="/cdn-cgi/l/email-protection#1b7f72686f6972795b7e7679697a7e6935787476357969"><span class="__cf_email__" data-cfemail="0d69647e797f646f4d68606f7f6c687f236e6260236f7f">[email protected]</span></a>; Internet <a href="http://www.flyembraer.com">http://www.flyembraer.com</a>.
(4) You may review copies of the 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.
(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: <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 February 1, 2013.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2013-02902 Filed 2-11-13; 8:45 am]
BILLING CODE 4910-13-P
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