Published 2001-11-26 · Federal Register document 01-29342
Airworthiness Directives; Dassault Model Mystere-Falcon 50 Series Airplanes
Publication summary
This amendment adopts a new airworthiness directive (AD) that is applicable to certain Dassault Model Mystere-Falcon 50 series airplanes. This action requires revising the Airplane Flight Manual to prohibit flight operation under reduced vertical separation minimum (RVSM). This action is necessary to prevent near misses or collision with other aircraft during flight, due to incorrect altitude information.
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Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:03.835669+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2001-8d66ddb74aa17366
- Source row
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- Raw source SHA-256
- 8d66ddb74aa17366596c5f6ccb4e6d04532df19ae027b6fa003379bdedb52c7e
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2001-24-03
- Effective date printed in this edition
- 2001-12-11
Some source clauses remain unstructured. Read the complete publication for conditions that have not been interpreted here.
Read 2 complete recorded clauses
Applicability wording · Applicability
Applicability: Model Mystere-Falcon 50 series airplanes having serial numbers 11, 16, 67, 107, 128, 138, 175, 183, 184, 185, 190, 222, and 225; certificated in any category.
Exact source excerpt. Text positions 8768–8948, end exclusive, in the original decoded publication. SHA-256: c412f7afa4c70c96f12490e7572cb2ec9b0daf39250f6daaa50bb33e25a2829c
Compliance and requirements
Compliance: Required as indicated, unless accomplished
previously.
To prevent near misses or collision with other aircraft during
flight, due to incorrect altitude information, accomplish the
following:
Airplane Flight Manual (AFM) Revision
(a) Within 10 days after the effective date of this AD, revise
the Limitations Section of the FAA-approved AFM to include the
following (this may be accomplished by inserting a copy of this AD
in the AFM):
``The reduced vertical separation minimum (RVSM) approval is
suspended until testing and corrective actions, if necessary, are
accomplished in accordance with a method approved by the Manager,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
or by the Direction Generale de l'Aviation Civile (DGAC).''
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.
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 1: 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 2: The subject of this AD is addressed in French
airworthiness directive T2001-524-037(B), effective date, October
27, 2001.
Effective Date
(d) This amendment becomes effective on December 11, 2001.
Exact source excerpt. Text positions 8948–10832, end exclusive, in the original decoded publication. SHA-256: 52fa8a56090297d1abd71a0d28f299dd5d7d1240def35aef5f221a585c99792a
No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.
Find all recorded historical references to AD 2001-24-03 · 0 printed reference observations in this pinned collection.
These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.
Why these observations are shown
They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.
Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: 055e5b69448ef4a510ba801d28c6bbe7e8d0d2dbf5ec9294f61339a83751feff. Source manifest: 0a7ba88de2c24b107b884519f5eb012d6a33a0417c681b79b6198d05b25eafc1.
Official source · 2001-11-26
Publication text
This is the complete recorded text of this dated publication.
Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.
Read the complete official publication text
[Federal Register Volume 66, Number 227 (Monday, November 26, 2001)]
[Rules and Regulations]
[Pages 58933-58934]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 01-29342]
[[Page 58933]]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2001-NM-330-AD; Amendment 39-12519; AD 2001-24-03]
RIN 2120-AA64
Airworthiness Directives; Dassault Model Mystere-Falcon 50 Series
Airplanes
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule; request for comments.
-----------------------------------------------------------------------
SUMMARY: This amendment adopts a new airworthiness directive (AD) that
is applicable to certain Dassault Model Mystere-Falcon 50 series
airplanes. This action requires revising the Airplane Flight Manual to
prohibit flight operation under reduced vertical separation minimum
(RVSM). This action is necessary to prevent near misses or collision
with other aircraft during flight, due to incorrect altitude
information.
DATES: Effective December 11, 2001.
Comments for inclusion in the Rules Docket must be received on or
before December 26, 2001.
ADDRESSES: Submit comments in triplicate to the Federal Aviation
Administration (FAA), Transport Airplane Directorate, ANM-114,
Attention: Rules Docket No. 2001-NM-330-AD, 1601 Lind Avenue, SW.,
Renton, Washington 98055-4056. Comments may be inspected at this
location between 9:00 a.m. and 3:00 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:
[email protected]. Comments sent via fax or the Internet must
contain ``Docket No. 2001-NM-330-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.
This information may be examined at the FAA, Transport Airplane
Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the
Office of the Federal Register, 800 North Capitol Street, NW., suite
700, Washington, DC.
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: The Direction Generale de l'Aviation Civile
(DGAC), which is the airworthiness authority for France, recently
notified the FAA that an unsafe condition may exist on certain Dassault
Model Mystere-Falcon 50 series airplanes. The DGAC advises that certain
airplanes may exceed the reduced vertical separation minimum (RVSM)
that was established by the International Civil Aviation Organization
(ICAO). The cause of exceeding RVSM is currently under investigation by
the manufacturer. This condition, if not corrected, could result in
flight operation under RVSM, and consequent near misses or collision
with other aircraft.
The DGAC has issued French airworthiness directive T2001-524-
037(B), effective October 27, 2001, in order to assure the continued
airworthiness of these airplanes in France.
FAA's Conclusions
This airplane model is manufactured in France and is 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 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, this AD is being issued to prevent near misses or
collision with other aircraft during flight, due to incorrect altitude
information. This AD requires revising the Airplane Flight Manual to
prohibit flight operation under RVSM until further testing and
corrective actions are accomplished.
Interim Action
This is considered to be interim action until final action is
identified, at which time the FAA may consider further rulemaking.
Determination of Rule's Effective Date
Since a situation exists that requires the immediate adoption of
this regulation, it is found that notice and opportunity for prior
public comment hereon are impracticable, and that good cause exists for
making this amendment effective in less than 30 days.
Comments Invited
Although this action is in the form of a final rule that involves
requirements affecting flight safety and, thus, was not preceded by
notice and an opportunity for public comment, comments are invited on
this rule. Interested persons are invited to comment on this 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 under the caption ADDRESSES. All
communications received on or before the closing date for comments will
be considered, and this rule may be amended in light of the comments
received. Factual information that supports the commenter's ideas and
suggestions is extremely helpful in evaluating the effectiveness of the
AD action and determining whether additional rulemaking action would be
needed.
Submit comments using the following format:
<bullet> 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.
<bullet> For each issue, state what specific change to the AD is
being requested.
<bullet> 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 rule that might
suggest a need to modify the 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 that
summarizes each FAA-public contact concerned with the substance of this
AD will be filed in the Rules Docket.
Commenters wishing the FAA to acknowledge receipt of their comments
submitted in response to this rule must submit a self-addressed,
stamped postcard on which the following statement is made: ``Comments
to Docket Number 2001-NM-330-AD.'' The postcard will be date stamped
and returned to the commenter.
Regulatory Impact
The regulations adopted herein will not have a substantial direct
effect on the States, on the relationship between the national
Government and the States,
[[Page 58934]]
or on the distribution of power and responsibilities among the various
levels of government. Therefore, it is determined that this final rule
does not have federalism implications under Executive Order 13132.
The FAA has determined that this regulation is an emergency
regulation that must be issued immediately to correct an unsafe
condition in aircraft, and that it is not a ``significant regulatory
action'' under Executive Order 12866. It has been determined further
that this action involves an emergency regulation under DOT Regulatory
Policies and Procedures (44 FR 11034, February 26, 1979). If it is
determined that this emergency regulation otherwise would be
significant under DOT Regulatory Policies and Procedures, a final
regulatory evaluation will be prepared and placed in the Rules Docket.
A copy of it, if filed, may be obtained from 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.
Adoption of the Amendment
Accordingly, pursuant to the authority delegated to me by the
Administrator, the Federal Aviation Administration amends 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:
2001-24-03 Dassault Aviation: Amendment 39-12519. Docket 2001-NM-
330-AD.
Applicability: Model Mystere-Falcon 50 series airplanes having
serial numbers 11, 16, 67, 107, 128, 138, 175, 183, 184, 185, 190,
222, and 225; certificated in any category.
Compliance: Required as indicated, unless accomplished
previously.
To prevent near misses or collision with other aircraft during
flight, due to incorrect altitude information, accomplish the
following:
Airplane Flight Manual (AFM) Revision
(a) Within 10 days after the effective date of this AD, revise
the Limitations Section of the FAA-approved AFM to include the
following (this may be accomplished by inserting a copy of this AD
in the AFM):
``The reduced vertical separation minimum (RVSM) approval is
suspended until testing and corrective actions, if necessary, are
accomplished in accordance with a method approved by the Manager,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
or by the Direction Generale de l'Aviation Civile (DGAC).''
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.
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 1: 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 2: The subject of this AD is addressed in French
airworthiness directive T2001-524-037(B), effective date, October
27, 2001.
Effective Date
(d) This amendment becomes effective on December 11, 2001.
Issued in Renton, Washington, on November 19, 2001.
Kalene C. Yanamura,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 01-29342 Filed 11-23-01; 8:45 am]
BILLING CODE 4910-13-U
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