[Federal Register: January 30, 2003 (Volume 68, Number 20)]
[Proposed Rules]
[Page 4739-4741]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr30ja03-20]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2001-NM-269-AD]
RIN 2120-AA64
Airworthiness Directives; Dassault Model Falcon 900 EX and
Mystere-Falcon 900 Series Airplanes
AGENCY: Federal Aviation Administration, DOT.
ACTION: Notice of proposed rulemaking (NPRM).
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SUMMARY: This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to certain Dassault Model Falcon 900
EX and Mystere-Falcon 900 series airplanes. This proposal would require
installing an attachment support assembly for the fire extinguishing
piping in the baggage compartment. This action is necessary to prevent
distortion of the fire extinguishing discharge nozzle as a result of
the nozzle not being secure, which could result in poor diffusion of
the fire extinguishing agent in the event of a fire in the baggage
compartment. This action is intended to address the identified unsafe
condition.
DATES: Comments must be received by March 3, 2003.
ADDRESSES: Submit comments in triplicate to the Federal Aviation
Administration (FAA), Transport Airplane Directorate, ANM-114,
Attention: Rules Docket No. 2001-NM-269-AD, 1601 Lind Avenue, SW.,
Renton, Washington 98055-4056. Comments may be inspected at this
location between 9 a.m. and 3 p.m., Monday through Friday, except
Federal holidays. Comments may be submitted via fax to (425) 227-1232.
Comments may also be sent via the Internet using the following address:
9-anm-nprmcomment@faa.gov. Comments sent via fax or the Internet must
contain ``Docket No. 2001-NM-269-AD'' in the subject line and need not
be submitted in triplicate. Comments sent via the Internet as attached
electronic files must be formatted in Microsoft Word 97 for Windows or
ASCII text.
The service information referenced in the proposed rule may be
obtained from Dassault Falcon Jet, PO Box 2000, South Hackensack, New
Jersey 07606. This information may be examined at the FAA, Transport
Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington.
[[Page 4740]]
FOR FURTHER INFORMATION CONTACT: Dan Rodina, Aerospace Engineer,
International Branch, ANM-116, FAA, Transport Airplane Directorate,
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425)
227-2125; fax (425) 227-1149.
SUPPLEMENTARY INFORMATION:
Comments Invited
Interested persons are invited to participate in the making of the
proposed rule by submitting such written data, views, or arguments as
they may desire. Communications shall identify the Rules Docket number
and be submitted in triplicate to the address specified above. All
communications received on or before the closing date for comments,
specified above, will be considered before taking action on the
proposed rule. The proposals contained in this action may be changed in
light of the comments received.
Submit comments using the following format:
[sbull] Organize comments issue-by-issue. For example, discuss a
request to change the compliance time and a request to change the
service bulletin reference as two separate issues.
[sbull] For each issue, state what specific change to the proposed
AD is being requested.
[sbull] Include justification (e.g., reasons or data) for each
request.
Comments are specifically invited on the overall regulatory,
economic, environmental, and energy aspects of the proposed rule. All
comments submitted will be available, both before and after the closing
date for comments, in the Rules Docket for examination by interested
persons. A report summarizing each FAA-public contact concerned with
the substance of this proposal will be filed in the Rules Docket.
Commenters wishing the FAA to acknowledge receipt of their comments
submitted in response to this action must submit a self-addressed,
stamped postcard on which the following statement is made: ``Comments
to Docket Number 2001-NM-269-AD.'' The postcard will be date stamped
and returned to the commenter.
Availability of NPRMs
Any person may obtain a copy of this NPRM by submitting a request
to the FAA, Transport Airplane Directorate, ANM-114, Attention: Rules
Docket No. 2001-NM-269-AD, 1601 Lind Avenue, SW., Renton, Washington
98055-4056.
Discussion
The Direction G[eacute]n[eacute]rale de l'Aviation Civile (DGAC),
which is the airworthiness authority for France, notified the FAA that
an unsafe condition may exist on certain Dassault Model Falcon 900 EX
and Model Mystere-Falcon 900 series airplanes. The DGAC advises of a
reported case where, after the fire extinguisher for the baggage
compartment discharged, the discharge nozzle for the fire extinguishing
piping through which the fire extinguishing agent passes, was found
damaged. Distortion of the discharge nozzle occurred at the bulkhead
feedthrough at frame 30 because the nozzle was not secure. This
condition, if not corrected, could result in poor diffusion of the fire
extinguishing agent in the event of a fire in the baggage compartment.
Explanation of Relevant Service Information
Dassault has issued Service Bulletins F900EX-142 (for Model Falcon
900 EX series airplanes) and F900-279 (for Model Mystere-Falcon 900
series airplanes), both dated June 7, 2001, including Service Bulletins
Compliance page, which describe procedures for installing an attachment
support assembly for the fire extinguishing piping in the baggage
compartment, and submitting a compliance report to Dassault.
Accomplishment of the actions specified in the applicable service
bulletin is intended to adequately address the identified unsafe
condition. The DGAC classified these service bulletins as mandatory and
issued French airworthiness directive 2001-192-034(B), dated May 16,
2001, in order to assure the continued airworthiness of these airplanes
in France.
FAA's Conclusions
These airplane models are manufactured in France and are type
certificated for operation in the United States under the provisions of
section 21.29 of the Federal Aviation Regulations (14 CFR 21.29) and
the applicable bilateral airworthiness agreement. Pursuant to this
bilateral airworthiness agreement, the DGAC has kept the FAA informed
of the situation described above. The FAA has examined the findings of
the DGAC, reviewed all available information, and determined that AD
action is necessary for products of this type design that are
certificated for operation in the United States.
Explanation of Requirements of Proposed Rule
Since an unsafe condition has been identified that is likely to
exist or develop on other airplanes of the same type design registered
in the United States, the proposed AD would require accomplishment of
the actions specified in the applicable service bulletin described
previously.
Differences Between Proposed Rule and Service Bulletin
Operators should note that, although the Accomplishment
Instructions of the referenced service bulletin describe procedures for
completing and submitting a compliance report, this proposed AD would
not require such reporting.
Cost Impact
The FAA estimates that 150 airplanes of U.S. registry would be
affected by this proposed AD, that it would take approximately 3 work
hours per airplane to accomplish the proposed actions, and that the
average labor rate is $60 per work hour. Required parts would be
provided by the manufacturer at no cost to the operators. Based on
these figures, the cost impact of the proposed AD on U.S. operators is
estimated to be $27,000, or $180 per airplane.
The cost impact figure discussed above is based on assumptions that
no operator has yet accomplished any of the proposed requirements of
this AD action, and that no operator would accomplish those actions in
the future if this proposed AD were not adopted. The cost impact
figures discussed in AD rulemaking actions represent only the time
necessary to perform the specific actions actually required by the AD.
These figures typically do not include incidental costs, such as the
time required to gain access and close up, planning time, or time
necessitated by other administrative actions.
Regulatory Impact
The regulations proposed herein would 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. Therefore, it
is determined that this proposal would not have federalism implications
under Executive Order 13132.
For the reasons discussed above, I certify that this proposed
regulation (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) if promulgated, will not have a significant economic impact,
positive or negative, on a substantial number of small entities under
the criteria of the Regulatory
[[Page 4741]]
Flexibility Act. A copy of the draft regulatory evaluation prepared for
this action is contained in the Rules Docket. A copy of it may be
obtained by contacting the Rules Docket at the location provided under
the caption ADDRESSES.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Safety.
The Proposed Amendment
Accordingly, pursuant to the authority delegated to me by the
Administrator, the Federal Aviation Administration proposes to amend
part 39 of the Federal Aviation Regulations (14 CFR part 39) as
follows:
PART 39--AIRWORTHINESS DIRECTIVES
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]
2. Section 39.13 is amended by adding the following new
airworthiness directive:
Dassault Aviation: Docket 2001-NM-269-AD.
Applicability: Model Falcon 900 EX and Mystere-Falcon 900 series
airplanes, certificated in any category; excluding those airplanes
on which the modification specified in Dassault Service Bulletin
F900EX-142 (Modification F900 EX M3368), or Dassault Service
Bulletin F900-279 (Modification MF900 M3368); both dated June 7,
2001; as applicable; has been done.
Note 1: This AD applies to each airplane identified in the
preceding applicability provision, regardless of whether it has been
otherwise modified, altered, or repaired in the area subject to the
requirements of this AD. For airplanes that have been modified,
altered, or repaired so that the performance of the requirements of
this AD is affected, the owner/operator must request approval for an
alternative method of compliance in accordance with paragraph (b) of
this AD. The request should include an assessment of the effect of
the modification, alteration, or repair on the unsafe condition
addressed by this AD; and, if the unsafe condition has not been
eliminated, the request should include specific proposed actions to
address it.
Compliance: Required as indicated, unless accomplished
previously.
To prevent distortion of the fire extinguishing discharge nozzle
as a result of the nozzle not being secure, which could result in
poor diffusion of the fire extinguishing agent in the event of a
fire in the baggage compartment, accomplish the following:
Installation
(a) Within 7 months or 330 flight hours after the effective date
of this AD, whichever comes first, install an attachment support
assembly for the fire extinguishing piping in the baggage
compartment per paragraphs 2.A. through 2.C. of the Accomplishment
Instructions of Dassault Service Bulletin F900EX-142 (for Model
Falcon 900 EX series airplanes); or Dassault Service Bulletin F900-
279 (for Model Mystere-Falcon F900 series airplanes); both dated
June 7, 2001; including Service Bulletins Compliance page; as
applicable.
Alternative Methods of Compliance
(b) An alternative method of compliance or adjustment of the
compliance time that provides an acceptable level of safety may be
used if approved by the Manager, International Branch, ANM-116,
Transport Airplane Directorate, FAA. Operators shall submit their
requests through an appropriate FAA Principal Maintenance Inspector,
who may add comments and then send it to the Manager, International
Branch, ANM-116.
Note 2: Information concerning the existence of approved
alternative methods of compliance with this AD, if any, may be
obtained from the International Branch, ANM-116.
Special Flight Permits
(c) Special flight permits may be issued in accordance with
sections 21.197 and 21.199 of the Federal Aviation Regulations (14
CFR 21.197 and 21.199) to operate the airplane to a location where
the requirements of this AD can be accomplished.
Note 3: The subject of this AD is addressed in French
airworthiness directive 2001-192-034(B), dated May 16, 2001.
Issued in Renton, Washington, on January 24, 2003.
Ali Bahrami,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 03-2148 Filed 1-29-03; 8:45 am]
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