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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.

Why this record is shown

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
results[479]
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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Source SHA-256
4b5d739355676d538ff63fadf62d491a99a69caed51b4917b9960a8546f98908
Text SHA-256
055e5b69448ef4a510ba801d28c6bbe7e8d0d2dbf5ec9294f61339a83751feff

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