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Published 2018-10-01 · Federal Register document 2018-21099

Airworthiness Directives; Dassault Aviation Airplanes

Publication summary

We are adopting a new airworthiness directive (AD) for all Dassault Aviation Model MYSTERE-FALCON 200 airplanes. This AD was prompted by a determination that more restrictive maintenance requirements and airworthiness limitations are necessary. This AD requires revising the maintenance or inspection program, as applicable, to incorporate new or more restrictive maintenance requirements and airworthiness limitations. We are issuing this AD to address the unsafe condition on these products.

Why this record is shown

Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:58.123663+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2018-258c65fa72d503e0
Source row
results[289]
Raw source SHA-256
258c65fa72d503e0b0dfb928a28beb1793ddc7dd9218bce0413e53dfe11d78fb

Final-rule publication

Recorded publication clauses

AD identifier printed in this edition
2018-19-26
Effective date printed in this edition
2018-11-05
Read 11 complete recorded clauses
Effective Date
(a) Effective Date

    This AD is effective November 5, 2018.

Exact source excerpt. Text positions 9865–9929, end exclusive, in the original decoded publication. SHA-256: 97dbb59a5383cf9b1f8cd1d04b9cb277dda6ef21ffa24349333c9056bddbf200

Affected ADs
(b) Affected ADs

    None.

Exact source excerpt. Text positions 9929–9958, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0

Applicability wording · Applicability
(c) Applicability

    This AD applies to all Dassault Aviation Model MYSTERE-FALCON 
200 airplanes, certificated in any category.

Exact source excerpt. Text positions 9958–10090, end exclusive, in the original decoded publication. SHA-256: 7a9598b577de6f9f1297a63fb532488b29ee1f73cdd9488e0cf863fd8d453311

Subject
(d) Subject

    Air Transport Association (ATA) of America Code 05, Time Limits/
Maintenance Checks.

Exact source excerpt. Text positions 10090–10193, end exclusive, in the original decoded publication. SHA-256: b15263823fded4455be00ff56d3a178d819d56a04f0615355cdb43771d1bcef9

Reason
(e) Reason

    This AD was prompted by a determination that more restrictive 
maintenance requirements and airworthiness limitations are 
necessary. We are issuing this AD to address fatigue cracking, 
damage, and corrosion in principal structural elements; such fatigue 
cracking, damage, and corrosion could result in reduced structural 
integrity of the airplane.

Exact source excerpt. Text positions 10193–10562, end exclusive, in the original decoded publication. SHA-256: 39e9dc1f54c008c5881ce13bda9807d2731f225a987bb986d8007adea90b7e8d

Compliance
(f) Compliance

    Comply with this AD within the compliance times specified, 
unless already done.

Exact source excerpt. Text positions 10562–10664, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3

Maintenance or Inspection Program Revision
(g) Maintenance or Inspection Program Revision

    Within 90 days after the effective date of this AD, revise the 
maintenance or inspection program, as applicable, to incorporate 
Chapter 5-40-00, Airworthiness Limitations, Revision 17, dated 
December 20, 2017, of the Dassault Falcon 200 Maintenance Manual. 
The initial compliance time for accomplishing the actions is at the 
applicable time specified in Chapter 5-40-00, Airworthiness 
Limitations, Revision 17, dated December 20, 2017, of the Dassault 
Falcon 200 Maintenance Manual; or within 90 days after the effective 
date of this AD; whichever occurs later.

Exact source excerpt. Text positions 10664–11287, end exclusive, in the original decoded publication. SHA-256: f1d665c60044c5677083fe6e403425ad9b9a4450738199fa0f90321f3f254d00

No Alternative Actions or Intervals
(h) No Alternative Actions or Intervals

    After the maintenance or inspection program has been revised as 
required by paragraph (g) of this AD, no alternative actions (e.g., 
inspections) or intervals may be used unless the actions or 
intervals are approved as an alternative method of compliance (AMOC) 
in accordance with the procedures specified in paragraph (i)(1) of 
this AD.

Exact source excerpt. Text positions 11287–11675, end exclusive, in the original decoded publication. SHA-256: 6b398e570636759821adc1aecaa481b74488289d9ceb46cfcedd04be35ba0d50

Other FAA AD Provisions
(i) Other FAA AD Provisions

    The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager, The 
Manager, International Section, Transport Standards Branch, 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 Section, send it to the attention of 
the person identified in paragraph (j)(2) of this AD. Information 
may be emailed 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.
    (2) Contacting the Manufacturer: For any requirement in this AD 
to obtain corrective actions from a manufacturer, the action must be 
accomplished using a method approved by the Manager, International 
Section, Transport Standards Branch, FAA; or the European Aviation 
Safety Agency (EASA); or Dassault Aviation's EASA Design 
Organization Approval (DOA). If approved by the DOA, the approval 
must include the DOA-authorized signature.

Exact source excerpt. Text positions 11675–12987, end exclusive, in the original decoded publication. SHA-256: 6f97d859a63a44fda6ff1375cee0ff4713936b423c1e4a28a4cf58525a241b46

Related Information
(j) Related Information

    (1) Refer to Mandatory Continuing Airworthiness Information 
(MCAI) EASA AD 2018-0009, dated January 15, 2018, for related 
information. This MCAI may be found in the AD docket on the internet 
at http://www.regulations.gov by searching for and locating Docket 
No. FAA-2018-0549.
    (2) For more information about this AD, contact Tom Rodriguez, 
Aerospace Engineer, International Section, Transport Standards 
Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone 
and fax 206-231-3226.

Exact source excerpt. Text positions 12987–13520, end exclusive, in the original decoded publication. SHA-256: 17f60939db8b4cd70c04d130afaba0890d929ae0b2248e497beb9ac72adc62d9

Material Incorporated by Reference
(k) Material Incorporated by Reference

    (1) The Director of the Federal Register approved the 
incorporation by reference (IBR) of the service information listed 
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
    (2) You must use this service information as applicable to do 
the actions required by this AD, unless this AD specifies otherwise.
    (i) Chapter 5-40-00, Airworthiness Limitations, Revision 17, 
dated December 20, 2017, of the Dassault Falcon 200 Maintenance 
Manual.
    (ii) Reserved.
    (3) For service information identified in this AD, contact 
Dassault Falcon Jet Corporation, Teterboro Airport, P.O. Box 2000, 
South Hackensack, NJ 07606; telephone 201-440-6700; internet http://www.dassaultfalcon.com.
    (4) You may view this service information at the FAA, Transport 
Standards Branch, 2200 South 216th St., Des Moines, WA. For 
information on the availability of this material at the FAA, call 
206-231-3195.
    (5) You may view this service information that is incorporated 
by reference at the National Archives and Records Administration 
(NARA). For information on the availability of this material at 
NARA, call 202-741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.

Exact source excerpt. Text positions 13520–14775, end exclusive, in the original decoded publication. SHA-256: 09387649139e5dfb11245d1dcd737524a021d482b1258984f117993dd185099a

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 2018-19-26 · 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: d9a40c3b2f1f04385cd505f93bc5a39e28ccdb6a5ff07258c2f6da5cd6be3f38. Source manifest: 8c7059d0329d4c82df5cffd3226b77a3f5a9011c6e7016a27977e9d2635a3495.

Official source · 2018-10-01

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 83, Number 190 (Monday, October 1, 2018)]
[Rules and Regulations]
[Pages 49275-49277]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2018-21099]


-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2018-0549; Product Identifier 2018-NM-014-AD; Amendment 
39-19427; AD 2018-19-26]
RIN 2120-AA64


Airworthiness Directives; Dassault Aviation Airplanes

AGENCY: Federal Aviation Administration (FAA), Department of 
Transportation (DOT).

ACTION: Final rule.

-----------------------------------------------------------------------

SUMMARY: We are adopting a new airworthiness directive (AD) for all 
Dassault Aviation Model MYSTERE-FALCON 200 airplanes. This AD was 
prompted by a determination that more restrictive maintenance 
requirements and airworthiness limitations are necessary. This AD 
requires revising the maintenance or inspection program, as applicable, 
to incorporate new or more restrictive maintenance requirements and 
airworthiness limitations. We are issuing this AD to address the unsafe 
condition on these products.

DATES: This AD is effective November 5, 2018.
    The Director of the Federal Register approved the incorporation by 
reference of a certain publication listed in this AD as of November 5, 
2018.

ADDRESSES: For service information identified in this final rule, 
contact Dassault Falcon Jet Corporation, Teterboro Airport, P.O. Box 
2000, South Hackensack, NJ 07606; telephone 201-440-6700; internet 
http://www.dassaultfalcon.com. You may view this service information at 
the FAA, Transport Standards Branch, 2200 South 216th St., Des Moines, 
WA. For information on the availability of this material at the FAA, 
call 206-231-3195. It is also available on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2018-
0549.

Examining the AD Docket

    You may examine the AD docket on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2018-
0549; or in person at Docket Operations between 9 a.m. and 5 p.m., 
Monday through Friday, except Federal holidays. The AD docket contains 
this final rule, the regulatory evaluation, any comments received, and 
other information. The address for Docket Operations (phone: 800-647-
5527) is

[[Page 49276]]

U.S. Department of Transportation, Docket Operations, M-30, West 
Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE, 
Washington, DC 20590.

FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aerospace Engineer, 
International Section, Transport Standards Branch, FAA, 2200 South 
216th St., Des Moines, WA 98198; telephone and fax 206-231-3226.

SUPPLEMENTARY INFORMATION: 

Discussion

    We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR 
part 39 by adding an AD that would apply to all Dassault Aviation Model 
MYSTERE-FALCON 200 airplanes. The NPRM published in the Federal 
Register on June 22, 2018 (83 FR 29056). The NPRM was prompted by a 
determination that more restrictive maintenance requirements and 
airworthiness limitations are necessary. The NPRM proposed to require 
revising the maintenance or inspection program, as applicable, to 
incorporate new or more restrictive maintenance requirements and 
airworthiness limitations.
    We are issuing this AD to address fatigue cracking, damage, and 
corrosion in principal structural elements; such fatigue cracking, 
damage, and corrosion could result in reduced structural integrity of 
the airplane.
    The European Aviation Safety Agency (EASA), which is the Technical 
Agent for the Member States of the European Union, has issued EASA AD 
2018-0009, dated January 15, 2018 (referred to after this as the 
Mandatory Continuing Airworthiness Information, or ``the MCAI''), to 
correct an unsafe condition for all Dassault Aviation Model MYSTERE-
FALCON 200 airplanes. The MCAI states:

    The airworthiness limitations for Dassault Myst[egrave]re Falcon 
200 aeroplanes, which are approved by EASA, are currently defined 
and published in AMM [aircraft maintenance manual] ALS 
[airworthiness limitations section] Chapter 5-40. These instructions 
have been identified as mandatory for continued airworthiness.
    Failure to accomplish these instructions could result in an 
unsafe condition.
    EASA previously issued AD 2008-0221 (later corrected), requiring 
the actions described in Dassault Myst[egrave]re Falcon 200 AMM 
Chapter 5-40 (DMD 18740A) at Revision 14. Since that [EASA] AD was 
issued, Dassault published the ALS, containing new and/or more 
restrictive maintenance tasks.
    For the reason described above, this [EASA] AD takes over the 
requirements for Myst[egrave]re Falcon 200 aeroplanes from EASA AD 
2008-0221 and requires accomplishment of the actions specified in 
the ALS.

    You may examine the MCAI in the AD docket on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2018-
0549.

Comments

    We gave the public the opportunity to participate in developing 
this final rule. We received no comments on the NPRM or on the 
determination of the cost to the public.

Conclusion

    We reviewed the relevant data and determined that air safety and 
the public interest require adopting this final rule as proposed, 
except for minor editorial changes. We have determined that these minor 
changes:
    <bullet> Are consistent with the intent that was proposed in the 
NPRM for addressing the unsafe condition; and
    <bullet> Do not add any additional burden upon the public than was 
already proposed in the NPRM.

Related Service Information Under 1 CFR Part 51

    Dassault Aviation has issued Chapter 5-40-00, Airworthiness 
Limitations, Revision 17, dated December 20, 2017, of the Dassult 
Falcon 200 Maintenance Manual. The service information describes 
mandatory maintenance tasks that operators must perform at specified 
intervals. This service information is reasonably available because the 
interested parties have access to it through their normal course of 
business or by the means identified in the ADDRESSES section.

Costs of Compliance

    We estimate that this AD affects 9 airplanes of U.S. registry. We 
estimate the following costs to comply with this AD:
    We have determined that revising the maintenance or inspection 
program takes an average of 90 work-hours per operator, although we 
recognize that this number may vary from operator to operator. In the 
past, we have estimated that this action takes 1 work-hour per 
airplane. Since operators incorporate maintenance or inspection program 
changes for their affected fleet(s), we have determined that a per-
operator estimate is more accurate than a per-airplane estimate. 
Therefore, we estimate the total cost per operator to be $7,650 (90 
work-hours x $85 per work-hour).

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.
    This AD is issued in accordance with authority delegated by the 
Executive Director, Aircraft Certification Service, as authorized by 
FAA Order 8000.51C. In accordance with that order, issuance of ADs is 
normally a function of the Compliance and Airworthiness Division, but 
during this transition period, the Executive Director has delegated the 
authority to issue ADs applicable to transport category airplanes and 
associated appliances to the Director of the System Oversight Division.

Regulatory Findings

    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 that 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),
    (3) Will not affect intrastate aviation in Alaska, and
    (4) 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.

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,

[[Page 49277]]

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 adding the following new airworthiness 
directive (AD):

2018-19-26 Dassault Aviation: Amendment 39-19427; Docket No. FAA-
2018-0549; Product Identifier 2018-NM-014-AD.

(a) Effective Date

    This AD is effective November 5, 2018.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to all Dassault Aviation Model MYSTERE-FALCON 
200 airplanes, certificated in any category.

(d) Subject

    Air Transport Association (ATA) of America Code 05, Time Limits/
Maintenance Checks.

(e) Reason

    This AD was prompted by a determination that more restrictive 
maintenance requirements and airworthiness limitations are 
necessary. We are issuing this AD to address fatigue cracking, 
damage, and corrosion in principal structural elements; such fatigue 
cracking, damage, and corrosion could result in reduced structural 
integrity of the airplane.

(f) Compliance

    Comply with this AD within the compliance times specified, 
unless already done.

(g) Maintenance or Inspection Program Revision

    Within 90 days after the effective date of this AD, revise the 
maintenance or inspection program, as applicable, to incorporate 
Chapter 5-40-00, Airworthiness Limitations, Revision 17, dated 
December 20, 2017, of the Dassault Falcon 200 Maintenance Manual. 
The initial compliance time for accomplishing the actions is at the 
applicable time specified in Chapter 5-40-00, Airworthiness 
Limitations, Revision 17, dated December 20, 2017, of the Dassault 
Falcon 200 Maintenance Manual; or within 90 days after the effective 
date of this AD; whichever occurs later.

(h) No Alternative Actions or Intervals

    After the maintenance or inspection program has been revised as 
required by paragraph (g) of this AD, no alternative actions (e.g., 
inspections) or intervals may be used unless the actions or 
intervals are approved as an alternative method of compliance (AMOC) 
in accordance with the procedures specified in paragraph (i)(1) of 
this AD.

(i) Other FAA AD Provisions

    The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager, The 
Manager, International Section, Transport Standards Branch, 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 Section, send it to the attention of 
the person identified in paragraph (j)(2) of this AD. Information 
may be emailed 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.
    (2) Contacting the Manufacturer: For any requirement in this AD 
to obtain corrective actions from a manufacturer, the action must be 
accomplished using a method approved by the Manager, International 
Section, Transport Standards Branch, FAA; or the European Aviation 
Safety Agency (EASA); or Dassault Aviation's EASA Design 
Organization Approval (DOA). If approved by the DOA, the approval 
must include the DOA-authorized signature.

(j) Related Information

    (1) Refer to Mandatory Continuing Airworthiness Information 
(MCAI) EASA AD 2018-0009, dated January 15, 2018, for related 
information. This MCAI may be found in the AD docket on the internet 
at http://www.regulations.gov by searching for and locating Docket 
No. FAA-2018-0549.
    (2) For more information about this AD, contact Tom Rodriguez, 
Aerospace Engineer, International Section, Transport Standards 
Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone 
and fax 206-231-3226.

(k) Material Incorporated by Reference

    (1) The Director of the Federal Register approved the 
incorporation by reference (IBR) of the service information listed 
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
    (2) You must use this service information as applicable to do 
the actions required by this AD, unless this AD specifies otherwise.
    (i) Chapter 5-40-00, Airworthiness Limitations, Revision 17, 
dated December 20, 2017, of the Dassault Falcon 200 Maintenance 
Manual.
    (ii) Reserved.
    (3) For service information identified in this AD, contact 
Dassault Falcon Jet Corporation, Teterboro Airport, P.O. Box 2000, 
South Hackensack, NJ 07606; telephone 201-440-6700; internet http://www.dassaultfalcon.com.
    (4) You may view this service information at the FAA, Transport 
Standards Branch, 2200 South 216th St., Des Moines, WA. For 
information on the availability of this material at the FAA, call 
206-231-3195.
    (5) You may view this service information that is incorporated 
by reference at the National Archives and Records Administration 
(NARA). For information on the availability of this material at 
NARA, call 202-741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.


    Issued in Des Moines, Washington, on September 14, 2018.
John P. Piccola,
Acting Director, System Oversight Division, Aircraft Certification 
Service.
[FR Doc. 2018-21099 Filed 9-28-18; 8:45 am]
 BILLING CODE 4910-13-P


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65baa0cd7fb4d6f541a03ad49769f4b80c7e45016de7a04d9e35b130d9380f57
Text SHA-256
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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.

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