[Federal Register Volume 76, Number 120 (Wednesday, June 22, 2011)]
[Rules and Regulations]
[Pages 36283-36285]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2011-15368]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2011-0259; Directorate Identifier 2010-NM-196-AD;
Amendment 39-16730; AD 2011-13-07]
RIN 2120-AA64
Airworthiness Directives; Dassault Aviation Model FALCON 7X
Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
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SUMMARY: We are superseding an existing airworthiness directive (AD)
that applies to 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:
Several occurrences of untimely radio-altimeter lock-up have
been reported, where the failed radio-altimeter indicated a negative
distance to the ground despite the aircraft was flying at medium or
high altitude.
A locked radio-altimeter 1 leads to untimely inhibition
of warnings that could be displayed along with certain abnormal
conditions while the avionic system switches into landing mode
during altitude cruise.
* * * * *
[Untimely radio altimeter lock-up] may cause the crew to be
unaware of possible system failures that could require urgent crew's
actions.
* * * * *
We are issuing this AD to require actions to correct the unsafe
condition on these products.
DATES: This AD becomes effective July 27, 2011.
ADDRESSES: You may examine the AD docket on the Internet at http://
[[Page 36284]]
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.
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
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 29, 2011 (76
FR 17364), and proposed to supersede AD 2010-02-02, Amendment 39-16173
(75 FR 1697, January 13, 2010). That NPRM proposed to correct an unsafe
condition for the specified products. The MCAI states:
Several occurrences of untimely radio-altimeter lock-up have
been reported, where the failed radio-altimeter indicated a negative
distance to the ground despite the aircraft was flying at medium or
high altitude.
A locked radio-altimeter 1 leads to untimely inhibition
of warnings that could be displayed along with certain abnormal
conditions while the avionic system switches into landing mode
during altitude cruise.
* * * * *
[Untimely radio altimeter lock-up] may cause the crew to be
unaware of possible system failures that could require urgent crew's
actions.
To address this unsafe condition, [EASA] AD 2009-0208 was issued
on 13 October 2009 [which corresponds with FAA AD 2010-02-02]. It
mandated application of a new abnormal Airplane Flight Manual (AFM)
procedure when radio-altimeter 1 lock-up occurs and
prohibited dispatch of the aeroplane with any radio-altimeter
inoperative.
Since AD 2009-0208 was issued, Easy avionics load 10 has been
developed with change M0566 or Service Bulletin (SB) Falcon 7X
n[deg]100 that brings new features to display a ``RA miscompare''
flag on both Primary Display Units (PDU) and accepts a commanded
system reversion to the correct radio-altimeter output.
EASA AD 2009-0208R1 is issued to allow not deactivating radio-
altimeter 1 in case lock-up conditions occur in flight for
aeroplanes on which M0566 or SB Falcon 7X n[deg]100 has been
embodied.
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 NPRM 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.
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 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 highlighted in a Note within the AD.
Costs of Compliance
We estimate that this AD will affect about 24 products of U.S.
registry.
The actions that are required by AD 2010-02-02 and retained in this
AD take about 1 work-hour per product, at an average labor rate of $85
per work-hour. Based on these figures, the estimated cost of the
currently required actions is $85 per product.
We estimate that it will take about 1 work-hour per product to
comply with the new basic requirements of this AD. The average labor
rate is $85 per work-hour. Based on these figures, we estimate the cost
of this AD to the U.S. operators to be $2,040, or $85 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 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.
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, 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 removing Amendment 39-16173 (75 FR
1697, January 13, 2010) and adding the following new AD:
[[Page 36285]]
2011-13-07 Dassault Aviation: Amendment 39-16730. Docket No. FAA-
2011-0259; Directorate Identifier 2010-NM-196-AD.
Effective Date
(a) This airworthiness directive (AD) becomes effective July 27,
2011.
Affected ADs
(b) This AD supersedes AD 2010-02-02, Amendment 39-16173.
Applicability
(c) This AD applies to Dassault Aviation Model FALCON 7X
airplanes, certificated in any category, all serial numbers.
Subject
(d) Air Transport Association (ATA) of America Code 34:
Navigation.
Reason
(e) The mandatory continuing airworthiness information (MCAI)
states:
Several occurrences of untimely radio-altimeter lock-up have
been reported, where the failed radio-altimeter indicated a negative
distance to the ground despite the aircraft was flying at medium or
high altitude.
A locked radio-altimeter 1 leads to untimely inhibition
of warnings that could be displayed along with certain abnormal
conditions while the avionic system switches into landing mode
during altitude cruise.
* * * * *
[Untimely radio altimeter lock-up] may cause the crew to be
unaware of possible system failures that could require urgent crew's
actions.
* * * * *
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.
Restatement of Requirements of AD 2010-02-02, With Revised Affected
Airplanes
(g) For airplanes on which modification M0566 or Dassault
Service Bulletin Falcon 7X-100 has not been accomplished: Within 14
days after January 28, 2010 (the effective date of AD 2010-02-02),
revise the Limitations Section of the Dassault Falcon 7X Airplane
Flight Manual (AFM) to include the following statement. This may be
done by inserting a copy of this AD in the AFM.
``If radio-altimeter 1 lock-up conditions occur in
flight, power off radio-altimeter 1, in accordance with the
instructions of Falcon 7X AFM procedure 3-140-65.
Dispatch of the airplane with any radio-altimeter inoperative is
prohibited.''
Note 1: When a statement identical to that in paragraph (g) of
this AD has been included in the general revisions of the AFM, the
general revisions may be inserted into the AFM, and the copy of this
AD may be removed from the AFM.
New Requirements of This AD
(h) For airplanes on which M0566 or Dassault Service Bulletin
Falcon 7X-100 has been accomplished: Within 14 days after the
effective date of this AD, revise the Limitations Section of the
Dassault Falcon 7X AFM to include the following statement. This may
be done by inserting a copy of this AD in the AFM. Doing this
revision terminates the requirements of paragraph (g) of this AD.
``If radio-altimeter 1 lock-up conditions occur in
flight, revert to the correct radio-altimeter output, in accordance
with the instructions of Falcon 7X AFM procedure 3-140-65B and 3-
140-70A.
Dispatch of the airplane with any radio-altimeter inoperative is
prohibited.''
Note 2: When a statement identical to that in paragraph (h) of
this AD has been included in the general revisions of the AFM, the
general revisions may be inserted into the AFM, and the copy of this
AD may be removed from the AFM.
FAA AD Differences
Note 3: This AD differs from the MCAI and/or service
information as follows: No differences.
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. 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: 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.
Information may be e-mailed 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.
Related Information
(j) Refer to MCAI European Aviation Safety Agency (EASA)
Airworthiness Directive 2009-0208R1, dated June 2, 2010, for related
information.
Material Incorporated by Reference
(k) None.
Issued in Renton, Washington, on June 14, 2011.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2011-15368 Filed 6-21-11; 8:45 am]
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