Published 2001-06-19 · Federal Register document 01-14724
Airworthiness Directives; Dassault Model Mystere-Falcon 900 and Falcon 900EX Series Airplanes
Publication summary
This amendment adopts a new airworthiness directive (AD), applicable to certain Dassault Model Mystere-Falcon 900 and Falcon 900EX series airplanes, that requires replacement of the protective screens of the underfloor structure boxes at frame 25. This amendment is necessary to prevent water from collecting and freezing in the structure boxes at frame 25, which could result in jamming of the flight controls and consequent reduced controllability of the airplane. This action is intended to address the identified unsafe condition.
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[221]
- Raw source SHA-256
- 8d66ddb74aa17366596c5f6ccb4e6d04532df19ae027b6fa003379bdedb52c7e
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2001-12-09
- Effective date printed in this edition
- 2001-07-24
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 900 series airplanes having
serial numbers 1 through 177 inclusive; and Model Falcon 900EX
series airplanes having serial numbers 1 through 41 inclusive;
certificated in any category.
Note 1: This AD applies to each airplane identified in the
preceding applicability provision, regardless of whether it has been
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.
Exact source excerpt. Text positions 6930–7905, end exclusive, in the original decoded publication. SHA-256: 852031b1365b376b71108783e70838aa8b4b425f0de2a23c1264284f331ca2ee
Compliance and requirements
Compliance: Required as indicated, unless accomplished
previously.
To prevent water from collecting and freezing in the structure
boxes at frame 25, which could result in jamming of the flight
controls and consequent reduced controllability of the airplane,
accomplish the following:
Screen Replacement
(a) Within 6 months after the effective date of this AD: Remove
the existing protective screens that are riveted to the center beam
and are also bonded to the frame and to the bottom of the underfloor
structure boxes at frame 25, and install new wider-mesh screens that
are riveted to the center beam and bonded to the frame only.
Accomplish the actions in accordance with Dassault Falcon 900
Service Bulletin 0232, dated March 1999, or Dassault Service
Bulletin F900-232, Revision 1, dated November 12, 1999 (for Model
Mystere-Falcon 900 series airplanes); or Dassault Falcon 900EX
Service Bulletin 0093, dated March 1999, or Dassault Service
Bulletin F900EX-93, Revision 1, dated November 12, 1999 (for Model
Falcon 900EX series airplanes); 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, FAA,
Transport Airplane Directorate. 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.
Incorporation by Reference
(d) The actions shall be done in accordance with Dassault Falcon
900 Service Bulletin 0232, dated March 1999; Dassault Service
Bulletin F900-232, Revision 1, dated November 12, 1999; Dassault
Falcon 900EX Service Bulletin 0093, dated March 1999; or Dassault
Service Bulletin F900EX-93, Revision 1, dated November 12, 1999; as
applicable. This incorporation by reference was approved by the
Director of the Federal Register in accordance with 5 U.S.C. 552(a)
and 1 CFR part 51. Copies may be obtained from Dassault Falcon Jet,
P.O. Box 2000, South Hackensack, New Jersey 07606. Copies may be
inspected 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.
Note 3: The subject of this AD is addressed in French
airworthiness directive 1999-446-028(B), dated November 3, 1999.
Effective Date
(e) This amendment becomes effective on July 24, 2001.
Exact source excerpt. Text positions 7905–10937, end exclusive, in the original decoded publication. SHA-256: b84805afb862e657ef40d2a489b4b68a5994c1a57e0eafe4f3bde4e57b3876bd
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 2001-12-09 · 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: 7dce6d900705e9021b41aeb5b60dc6937b61ce96d521fa78ffa1b1febd613542. Source manifest: 5eeeedc0bbd9e6f73fda1e64a9e376c1c7479b6804f43f2de9a404a57f3cf358.
Official source · 2001-06-19
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 118 (Tuesday, June 19, 2001)]
[Rules and Regulations]
[Pages 32896-32897]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 01-14724]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2000-NM-291-AD; Amendment 39-12264; AD 2001-12-09]
RIN 2120-AA64
Airworthiness Directives; Dassault Model Mystere-Falcon 900 and
Falcon 900EX Series Airplanes
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: This amendment adopts a new airworthiness directive (AD),
applicable to certain Dassault Model Mystere-Falcon 900 and Falcon
900EX series airplanes, that requires replacement of the protective
screens of the underfloor structure boxes at frame 25. This amendment
is necessary to prevent water from collecting and freezing in the
structure boxes at frame 25, which could result in jamming of the
flight controls and consequent reduced controllability of the airplane.
This action is intended to address the identified unsafe condition.
DATES: Effective July 24, 2001.
The incorporation by reference of certain publications listed in
the regulations is approved by the Director of the Federal Register as
of July 24, 2001.
ADDRESSES: The service information referenced in this AD may be
obtained from Dassault Falcon Jet, P.O. Box 2000, South Hackensack, New
Jersey 07606. This information may be examined at the Federal Aviation
Administration (FAA), Transport Airplane Directorate, Rules Docket,
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: Norman B. Martenson, Manager,
International Branch, ANM-116, FAA, Transport Airplane Directorate,
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425)
227-2110; fax (425) 227-1149.
SUPPLEMENTARY INFORMATION: A proposal to amend part 39 of the Federal
Aviation Regulations (14 CFR part 39) to include an airworthiness
directive (AD) that is applicable to certain Dassault Model Mystere-
Falcon 900 and Falcon 900EX series airplanes was published in the
Federal Register on October 30, 2000 (65 FR 64636). That action
proposed to require replacement of the protective screens of the
underfloor structure boxes at frame 25.
Comments
Interested persons have been afforded an opportunity to participate
in the making of this amendment. Due consideration has been given to
the single comment received.
Request To Revise Service Information
The manufacturer has advised the FAA that, since the issuance of
the proposed rule, it has issued Dassault Service Bulletin F900-232,
Revision 1, dated November 12, 1999 (for Model Mystere-Falcon 900
series airplanes); and Dassault Service Bulletin F900EX-93, Revision 1,
dated November 12, 1999 (for Model Falcon 900EX series airplanes); and
requests that the final rule be revised to require accomplishment of
the actions in accordance with these new revisions of the service
bulletins. The FAA agrees with the manufacturer's request. We have
reviewed and approved Revision 1 of these service bulletins, and find
that they are essentially identical to the original versions (which
were cited as the appropriate sources of service information for
accomplishment of the actions in the proposed rule). The final rule has
been revised to require accomplishment of the actions in accordance
with either the original issue or Revision 1 of the applicable service
bulletin.
Conclusion
After careful review of the available data, including the comment
noted above, the FAA has determined that air safety and the public
interest require the adoption of the rule with the changes described
previously. The FAA has determined that these changes will neither
increase the economic burden on any operator nor increase the scope of
the AD.
Cost Impact
The FAA estimates that 127 Dassault Model Mystere-Falcon 900 and
Falcon 900EX series airplanes of U.S. registry will be affected by this
AD, that it will take approximately 5 work hours per airplane to
accomplish the required actions, and that the average labor rate is $60
per work hour. Required parts will cost approximately $128 per
airplane. Based on these figures, the cost impact of the AD on U.S.
operators is estimated to be $54,356, or $428 per airplane.
The cost impact figure discussed above is based on assumptions that
no operator has yet accomplished any of the requirements of this AD
action, and that no operator would accomplish those actions in the
future if this AD were not adopted. The cost impact
[[Page 32897]]
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 adopted herein 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. Therefore, it
is determined that this final rule does not have federalism
implications under Executive Order 13132.
For the reasons discussed above, I certify that this action (1) is
not a ``significant regulatory action'' under Executive Order 12866;
(2) is not a ``significant rule'' under 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. A final evaluation has been prepared for this action
and it is contained in the Rules Docket. A copy of it 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, Incorporation by
reference, 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:
2001-12-09 Dassault Aviation: Amendment 39-12264. Docket 2000-NM-
291-AD.
Applicability: Model Mystere-Falcon 900 series airplanes having
serial numbers 1 through 177 inclusive; and Model Falcon 900EX
series airplanes having serial numbers 1 through 41 inclusive;
certificated in any category.
Note 1: This AD applies to each airplane identified in the
preceding applicability provision, regardless of whether it has been
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 water from collecting and freezing in the structure
boxes at frame 25, which could result in jamming of the flight
controls and consequent reduced controllability of the airplane,
accomplish the following:
Screen Replacement
(a) Within 6 months after the effective date of this AD: Remove
the existing protective screens that are riveted to the center beam
and are also bonded to the frame and to the bottom of the underfloor
structure boxes at frame 25, and install new wider-mesh screens that
are riveted to the center beam and bonded to the frame only.
Accomplish the actions in accordance with Dassault Falcon 900
Service Bulletin 0232, dated March 1999, or Dassault Service
Bulletin F900-232, Revision 1, dated November 12, 1999 (for Model
Mystere-Falcon 900 series airplanes); or Dassault Falcon 900EX
Service Bulletin 0093, dated March 1999, or Dassault Service
Bulletin F900EX-93, Revision 1, dated November 12, 1999 (for Model
Falcon 900EX series airplanes); 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, FAA,
Transport Airplane Directorate. 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.
Incorporation by Reference
(d) The actions shall be done in accordance with Dassault Falcon
900 Service Bulletin 0232, dated March 1999; Dassault Service
Bulletin F900-232, Revision 1, dated November 12, 1999; Dassault
Falcon 900EX Service Bulletin 0093, dated March 1999; or Dassault
Service Bulletin F900EX-93, Revision 1, dated November 12, 1999; as
applicable. This incorporation by reference was approved by the
Director of the Federal Register in accordance with 5 U.S.C. 552(a)
and 1 CFR part 51. Copies may be obtained from Dassault Falcon Jet,
P.O. Box 2000, South Hackensack, New Jersey 07606. Copies may be
inspected 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.
Note 3: The subject of this AD is addressed in French
airworthiness directive 1999-446-028(B), dated November 3, 1999.
Effective Date
(e) This amendment becomes effective on July 24, 2001.
Issued in Renton, Washington, on June 6, 2001.
Donald L. Riggin,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 01-14724 Filed 6-18-01; 8:45 am]
BILLING CODE 4910-13-U
Why this text is shown
The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T04:29:02.627006+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.
Open the captured official edition
- Source SHA-256
- 4c9bec07599e854cab27e11042474343c23e06d76b05d1afa60aed46d3abbd25
- Text SHA-256
- 7dce6d900705e9021b41aeb5b60dc6937b61ce96d521fa78ffa1b1febd613542
Return to the full metadata catalog · Search complete publication text · Explore retained publication text and evidence
Coverage and limits
These are dated publication metadata, recorded clauses and literal source observations. Word, model-label, header and reference matches do not establish current legal effect, manufacturer/model identity, aircraft applicability, installed configuration or compliance.
The collection uses 33 explicit annual source snapshots. Source captures and operative-text qualifications have separate states. Missing information remains unknown.