Federal Register, Volume 75 Issue 226 (Wednesday, November 24, 2010)

[Federal Register Volume 75, Number 226 (Wednesday, November 24, 2010)]
[Rules and Regulations]
[Pages 71530-71532]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2010-29458]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2010-1155; Directorate Identifier 2010-NM-238-AD;
Amendment 39-16527; AD 2010-24-08]
RIN 2120-AA64

Airworthiness Directives; DASSAULT AVIATION Model MYSTERE-FALCON
50 Airplanes

AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).

ACTION: Final rule; request for comments.

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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) originated by an aviation authority of
another country to identify and correct an unsafe condition on an
aviation product. The MCAI describes the unsafe condition as:

On two occurrences on Myst[egrave]re-Falcon 50 aeroplanes in
service, it was detected that two pipes of the emergency brake
system 2 located near the nose landing gear bearing were
swapped.
The swapping of these two pipes implies that when the Left Hand
(LH) brake pedal is depressed, the Right Hand (RH) brake unit is
activated, and conversely, when the RH brake pedal is depressed, the
LH brake unit is actuated. This constitutes an unsafe condition,
which may go unnoticed as the condition is latent until the
emergency brake system 2 is used. This condition, if not
corrected, could ultimately lead to a runway excursion of the
aeroplane.
* * * * *

This AD requires actions that are intended to address the unsafe
condition described in the MCAI.

DATES: This AD becomes effective December 9, 2010.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in the AD as of December 9,
2010.
We must receive comments on this AD by January 10, 2011.

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 W12-40, 1200 New
Jersey Avenue, SE., Washington, DC, between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.

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 this AD, 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.

FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aerospace Engineer,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425)
227-1137; fax (425) 227-1149.

SUPPLEMENTARY INFORMATION:

Discussion

The European Aviation Safety Agency (EASA), which is the Technical
Agent for the Member States of the European Community, has issued EASA
Emergency Airworthiness Directive 2010-0208-E, dated October 12, 2010
(referred to after this as ``the MCAI''), to correct an unsafe
condition for the specified products. The MCAI states:

On two occurrences on Myst[egrave]re-Falcon 50 aeroplanes in
service, it was detected that

[[Page 71531]]

two pipes of the emergency brake system 2 located near the
nose landing gear bearing were swapped.
The swapping of these two pipes implies that when the Left Hand
(LH) brake pedal is depressed, the Right Hand (RH) brake unit is
activated, and conversely, when the RH brake pedal is depressed, the
LH brake unit is actuated. This constitutes an unsafe condition,
which may go unnoticed as the condition is latent until the
emergency brake system 2 is used. This condition, if not
corrected, could ultimately lead to a runway excursion of the
aeroplane.
For the reasons described above, this [EASA] AD requires an
[general visual] inspection of the main landing gear braking system
and, in case of findings, proper re-installation of the emergency
brake system 2 pipes. This [EASA] AD also requires painting
the affected pipes for clear identification in order to avoid
mistakes while reinstalling them after maintenance.

You may obtain further information by examining the MCAI in the AD
docket.

Relevant Service Information

DASSAULT AVIATION has issued Service Bulletin F50-515, dated
October 12, 2010. The actions described in this service information are
intended to correct the unsafe condition identified in the MCAI.

FAA's Determination and Requirements of this AD

This product has been approved by the aviation authority of another
country, and is approved for operation in the United States. Pursuant
to our bilateral agreement with the State of Design Authority, we have
been notified of the unsafe condition described in the MCAI and service
information referenced above. We are issuing this AD because we
evaluated all pertinent information and determined the unsafe condition
exists and is likely to exist or develop on other products of the same
type design.

Differences Between the 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 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 FAA policies. Any such differences are
highlighted in a Note within the AD.

FAA's Determination of the Effective Date

An unsafe condition exists that requires the immediate adoption of
this AD. The FAA has found that the risk to the flying public justifies
waiving notice and comment prior to adoption of this rule because this
unsafe condition could result in a high speed runway excursion when the
brakes are applied. Therefore, we determined that notice and
opportunity for public comment before issuing this AD are impracticable
and that good cause exists for making this amendment effective in fewer
than 30 days.

Comments Invited

This AD is a final rule that involves requirements affecting flight
safety, and we did not precede it by notice and opportunity for public
comment. We invite you to send any written relevant data, views, or
arguments about this AD. Send your comments to an address listed under
the ADDRESSES section. Include ``Docket No. FAA-2010-1155; Directorate
Identifier 2010-NM-238-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

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 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); 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.

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:

2010-24-08 Dassault Aviation: Amendment 39-16527. Docket No. FAA-
2010-1155; Directorate Identifier 2010-NM-238-AD.

Effective Date

(a) This airworthiness directive (AD) becomes effective December
9, 2010.

Affected ADs

(b) None.

Applicability

(c) This AD applies to DASSAULT AVIATION Model MYSTERE-FALCON 50
airplanes, certificated in any category, all serial numbers.

Subject

(d) Air Transport Association (ATA) of America Code 32: Landing
Gear.

Reason

(e) The mandatory continued airworthiness information (MCAI)
states:

[[Page 71532]]

Compliance

(f) You are responsible for having the actions required by this
AD performed within the compliance times specified, unless the
actions have already been done.

Actions

(g) Within 7 days after the effective date of this AD, do a
general visual inspection for correct installation (as defined in
Dassault Service Bulletin F50-515, dated October 12, 2010) of the
emergency brake system number 2, in accordance with the
Accomplishment Instructions of Dassault Service Bulletin F50-515,
dated October 12, 2010, except that work required by this AD can
only be done by persons prescribed in 14 CFR 43.3 and 43.7.
(h) If the emergency brake system number 2 is found installed
incorrectly during the inspection required by paragraph (g) of this
AD: Before further flight, install the emergency brake system number
2 correctly, in accordance with the Accomplishment Instructions of
Dassault Service Bulletin F50-515, dated October 12, 2010.

FAA AD Differences

Note 1: This AD differs from the MCAI and/or service information
as follows:
(1) European Aviation Safety Agency (EASA) AD 2010-0208-E, dated
October 12, 2010, has a compliance time of ``before the next flight
after the effective date of this AD.'' This AD requires that the
actions be done within 7 days after the effective date of this AD.
(2) EASA AD 2010-0208-E, dated October 12, 2010, allows the
flightcrew to inspect the emergency brake system number 2 specified
in accordance with Dassault Service Bulletin F50-515, dated October
12, 2010. However, this AD requires the inspection to be performed
by certificated maintenance personnel.

(3) EASA AD 2010-0208-E, dated October 12, 2010, requires
painting the pipes end of the emergency brake system number 2 and
related unions within 7 months after the effective date of that AD.
This AD does not require painting the pipes end of the emergency
brake system number 2 and related unions. We might consider
additional rulemaking to require this action in the future.

Other FAA AD Provisions

(i) 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: Tom
Rodriguez, Aerospace Engineer, International Branch, ANM-116,
Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton,
Washington 98057-3356; telephone (425) 227-1137; fax (425) 227-1149.
Before using any approved AMOC on any airplane to which the AMOC
applies, notify your principal maintenance inspector (PMI) or
principal avionics inspector (PAI), as appropriate, or lacking a
principal inspector, your local Flight Standards 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.
(3) Reporting Requirements: For any reporting requirement in
this AD, under the provisions of the Paperwork Reduction Act (44
U.S.C. 3501 et seq.), the Office of Management and Budget (OMB) has
approved the information collection requirements and has assigned
OMB Control Number 2120-0056.

Related Information

(j) Refer to MCAI EASA AD 2010-0208-E, dated October 12, 2010;
and Dassault Service Bulletin F50-515, dated October 12, 2010; for
related information.

Material Incorporated by Reference

(k) You must use Dassault Service Bulletin F50-515, dated
October 12, 2010, 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
Dassault Falcon Jet, P.O. Box 2000, South Hackensack, New Jersey
07606; telephone 201-440-6700; Internet http://www.dassaultfalcon.com.
(3) You may review copies of the service information at the 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.
(4) You may also review copies of the 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/code_of_federal_regulations/ibr_locations.html.

Issued in Renton, Washington on November 15, 2010.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2010-29458 Filed 11-23-10; 8:45 am]
BILLING CODE 4910-13-P