[Federal Register Volume 77, Number 180 (Monday, September 17, 2012)]
[Rules and Regulations]
[Pages 57003-57005]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2012-22041]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2011-1167; Directorate Identifier 2011-NM-058-AD;
Amendment 39-17189; AD 2012-18-12]
RIN 2120-AA64
Airworthiness Directives; Airbus 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 certain
Airbus Model A318, A319, and A320 series airplanes. This AD was
prompted by a report of a torn out aspirator due to the aspirator
interfering with the extrusion lip of the off-wing escape slide (OWS)
enclosure during the initial stage of the deployment sequence. This AD
requires modifying the OWS enclosures on both sides. We are issuing
this AD to prevent both off-wing exits from being inoperative, which,
during an emergency, would impair the safe evacuation of occupants,
possibly resulting in personal injuries.
DATES: This AD becomes effective October 22, 2012.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of October 22,
2012.
ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov 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.
[[Page 57004]]
FOR FURTHER INFORMATION CONTACT: Sanjay Ralhan, Aerospace Engineer,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
1601 Lind Avenue SW., Renton, Washington 98057-3356; telephone (425)
227-1405; fax (425) 227-1149.
SUPPLEMENTARY INFORMATION:
Discussion
We issued a supplemental notice of proposed rulemaking (SNPRM) to
amend 14 CFR part 39 to include an AD that would apply to the specified
products. That SNPRM was published in the Federal Register on June 11,
2012 (77 FR 34283). That SNPRM proposed to correct an unsafe condition
for the specified products. The MCAI states:
One operator has reported a torn out aspirator following
scheduled (for on-ground testing purposes) deployment of the Left
Hand (LH) OWS [off-wing escape slide].
Investigations have revealed that the aspirator of the off-wing
ramp/slide system interferes with the extrusion lip of the OWS
enclosure during the initial stage of the deployment sequence.
This condition, if not corrected, could result in both LH and
Right Hand (RH) off-wing exits being unserviceable which, during an
emergency, would impair the safe evacuation of occupants, possibly
resulting in personal injuries.
For the reasons described above, this [European Aviation Safety
Agency (EASA)] AD requires the modification of the OWS enclosures on
both sides.
* * * * *
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 received no comments on the SNPRM (77 FR 34283, June 11,
2012) or on the determination of the cost to the public.
Conclusion
We reviewed the available data 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:
Are consistent with the intent that was proposed in the
SNPRM (77 FR 34283, June 11, 2012) for correcting the unsafe condition;
and
Do not add any additional burden upon the public than was
already proposed in the SNPRM (77 FR 34283, June 11, 2012).
Costs of Compliance
We estimate that this AD will affect about 694 products of U.S.
registry. We also estimate that it will take about 14 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 $825,860, or $1,190 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 http://www.regulations.gov; 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 (76 FR 67625, November 2,
2011), SNPRM (77 FR 34283, June 11, 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:
2012-18-12 Airbus: Amendment 39-17189. Docket No. FAA-2011-1167;
Directorate Identifier 2011-NM-058-AD.
(a) Effective Date
This airworthiness directive (AD) becomes effective October 22,
2012.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Airbus Model A318-111, -112, -121, and -122
airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and -133
airplanes; and Model A320-111, -211, -212, -214, -231, -232, and -233
airplanes; certificated in any category; all manufacturer serial
numbers; except for airplanes on which off-wing escape slides (OWS)
having part number (P/N) D31865-111 and P/N D31865-112 are installed.
(d) Subject
Air Transport Association (ATA) of America Code 25: Equipment/
furnishings.
[[Page 57005]]
(e) Reason
This AD was prompted by a report of a torn out aspirator due to the
aspirator interfering with the extrusion lip of the OWS enclosure
during the initial stage of the deployment sequence. We are issuing
this AD to prevent both off-wing exits from being inoperative, which,
during an emergency, would impair the safe evacuation of occupants,
possibly resulting in personal injuries.
(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) Modification
Within 36 months after the effective date of this AD, modify both
left-hand and right-hand OWS enclosures, in accordance with the
instructions in Airbus Service Bulletin A320-25-1649, dated February
16, 2010.
(h) Parts Installation Prohibition
After accomplishing the modification required by paragraph (g) of
this AD, no person may install an OWS having P/N D31865-109, P/N
D31865-110, P/N D31865-209, or P/N D31865-210 on that airplane.
(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, 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: Sanjay Ralhan, Aerospace Engineer, International Branch, ANM-116,
Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton,
Washington 98057-3356; telephone 425-227-1405; fax 425-227-1149.
Information may be emailed to: [email protected]. 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 European Aviation Safety Agency Airworthiness
Directive 2010-0210, dated October 21, 2010 (corrected October 27,
2010); and Airbus Service Bulletin A320-25-1649, dated February 16,
2010; for related information.
(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) Airbus Service Bulletin A320-25-1649, dated February 16, 2010.
(ii) Reserved.
(3) For service information identified in this AD, contact Airbus,
Airworthiness Office--EAS, 1 Rond Point Maurice Bellonte, 31707 Blagnac
Cedex, France; telephone +33 5 61 93 36 96; fax +33 5 61 93 44 51;
email [email protected]; Internet http://www.airbus.com.
(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: http://www.archives.gov/federal-register/cfr/index.html. http://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued in Renton, Washington, on August 31, 2012.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2012-22041 Filed 9-14-12; 8:45 am]
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