Published 2017-05-09 · Federal Register document 2017-08829
Airworthiness Directives; Dassault Aviation Airplanes
Publication summary
We are superseding Airworthiness Directive (AD) 2013-03-12 for all Dassault Aviation Model MYSTERE-FALCON 50 airplanes. AD 2013-03-12 required revising the maintenance program to incorporate certain maintenance requirements and airworthiness limitations. This AD requires revising the maintenance or inspection program, as applicable, to incorporate new or revised maintenance requirements and airworthiness limitations. This AD was prompted by issuance of a revision to the airplane maintenance manual (AMM) that introduces new or more restrictive maintenance requirements and/or 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 2026-09-03T22:23:54.997910+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2017-90ba553c3b802c53
- Source row
- results[115]
- Raw source SHA-256
- 90ba553c3b802c5316e8d18f30db5da9f7731a87f58278ec2965f199ef4375e9
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2017-09-03
- Effective date printed in this edition
- 2017-06-13
Read 14 complete recorded clauses
Effective Date
(a) Effective Date
This AD is effective June 13, 2017.
Exact source excerpt. Text positions 11178–11239, end exclusive, in the original decoded publication. SHA-256: 8484db96fdbc56f167a8b93890b3cc12ecda4e87ad4253068750efbee2d91430
Affected ADs
(b) Affected ADs
(1) This AD replaces AD 2013-03-12, Amendment 39-17347 (78 FR
9798, February 12, 2013) (``AD 2013-03-12'').
(2) This AD affects AD 2010-26-05, Amendment 39-16544 (75 FR
79952, December 21, 2010) (``AD 2010-26-05''), and AD 2012-02-18,
Amendment 39-16941 (77 FR 12175, February 29, 2012) (``AD-2012-02-
18'').
Exact source excerpt. Text positions 11239–11578, end exclusive, in the original decoded publication. SHA-256: 3b4f28c4184f93a1f2a7bb8c3a027084e605efd8028fabd47e89228c30e43951
Applicability wording · Applicability
(c) Applicability
This AD applies to Dassault Aviation Model MYSTERE-FALCON 50
airplanes, certificated in any category, all manufacturer serial
numbers.
Exact source excerpt. Text positions 11578–11739, end exclusive, in the original decoded publication. SHA-256: 4dfb38f9e11e119cdcc4b38232362e6d16fecb34564379ea5c8864c7e3c7c15a
Subject
(d) Subject
Air Transport Association (ATA) of America Code 05, Periodic
inspections.
Exact source excerpt. Text positions 11739–11832, end exclusive, in the original decoded publication. SHA-256: 2b4e613bae3b2dacd9370156cd68848eb90a2c19c5f0e0b6cabbb356c3ac6e58
Reason
(e) Reason
This AD was prompted by a manufacturer revision to the airplane
maintenance manual (AMM) that introduces new or more restrictive
maintenance requirements and/or airworthiness limitations. We are
issuing this AD to prevent reduced structural integrity of the
airplane.
Exact source excerpt. Text positions 11832–12121, end exclusive, in the original decoded publication. SHA-256: 4e1a928cb0e983960c6ad21c3b66a45033f2bf7948f34ea5ac2e6ccd639d4ce1
Compliance
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
Exact source excerpt. Text positions 12121–12223, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3
Retained Maintenance Program Revision, With No Changes
(g) Retained Maintenance Program Revision, With No Changes
This paragraph restates the requirements of paragraph (g) of AD
2013-03-12, with no changes. Within 30 days after March 19, 2013
(the effective date of AD 2013-03-12): Revise the maintenance
program to incorporate all airworthiness limitations and maintenance
tasks specified in Section 05-40/00,
[[Page 21469]]
Airworthiness Limitations, of Chapter 5-40, Airworthiness
Limitations, of the Dassault Falcon 50/50EX Maintenance Manual,
Revision 21, dated June 2011. The initial compliance times for the
tasks are at the applicable times specified in Section 05-40/00,
Airworthiness Limitations, of Chapter 5-40, Airworthiness
Limitations, of the Dassault Falcon 50/50EX Maintenance Manual,
Revision 21, dated June 2011, or within 30 days after March 19,
2013, whichever occurs later.
Exact source excerpt. Text positions 12223–13083, end exclusive, in the original decoded publication. SHA-256: 12ccf5a2a54d8a282572c730eb2fd7ba36f54dbb0ea72764c5bcc22592768b1d
Retained Provision Regarding Alternative Actions, Intervals, and Critical Design Configuration Control Limitations (CDCCLs), With New Exception
(h) Retained Provision Regarding Alternative Actions, Intervals, and
Critical Design Configuration Control Limitations (CDCCLs), With New
Exception
This paragraph restates the requirements of paragraph (h) of AD
2013-03-12, with a new exception. Except as required by paragraph
(i) of this AD: After accomplishing the revisions required by
paragraph (g) of this AD, no alternative actions (e.g.,
inspections), intervals, and/or CDCCLs may be used other than those
specified in Section 05-40/00, Airworthiness Limitations, of Chapter
5-40, Airworthiness Limitations, of the Dassault Falcon 50/50EX
Maintenance Manual, Revision 21, dated June 2011, unless the
actions, intervals, and/or CDCCLs are approved as an alternative
methods of compliance (AMOC) in accordance with the procedures
specified in paragraph (l)(1) of this AD.
Exact source excerpt. Text positions 13083–13929, end exclusive, in the original decoded publication. SHA-256: ba472416f489236d89571ff871b23a0c85d78a8a0caf806c81c1b6375cc20f6b
New Maintenance or Inspection Program Revision
(i) New Maintenance or Inspection Program Revision
Within 30 days after the effective date of this AD: Revise the
maintenance or inspection program, as applicable, to incorporate
airworthiness limitations, maintenance tasks, and associated
thresholds and intervals specified in Section 05-40/00,
Airworthiness Limitations, of Chapter 5-40, Airworthiness
Limitations, of the Erratum to Dassault Falcon 50/50EX Maintenance
Manual, Revision 23, dated July 2015. The initial compliance times
for the tasks are at the applicable times specified in Section 05-
40/00, Airworthiness Limitations, of Chapter 5-40, Airworthiness
Limitations, of the Erratum to Dassault Falcon 50/50EX Maintenance
Manual, Revision 23, dated July 2015, or within 30 days after the
effective date of this AD, whichever occurs later. Accomplishing the
revision of the maintenance or inspection program required by this
paragraph terminates the requirements of paragraph (g) of this AD.
Exact source excerpt. Text positions 13929–14903, end exclusive, in the original decoded publication. SHA-256: 6dc0a081fd12aa7873310a6fdc9c37002665982957f16b39090e76af81cdf063
New Provision Regarding Alternative Actions and Intervals
(j) New Provision Regarding Alternative Actions and Intervals
After the maintenance or inspection program has been revised as
required by paragraph (i) of this AD, no alternative actions (e.g.,
inspections) or intervals may be used unless the actions and
intervals are approved as an AMOC in accordance with the procedures
specified in paragraph (l)(1) of this AD.
Exact source excerpt. Text positions 14903–15278, end exclusive, in the original decoded publication. SHA-256: 54eed2fb47e2d50c94e92c00db8b1474a0b738a50bd2cdb942ce8b6f762dd3c4
Terminating Action for Certain ADs
(k) Terminating Action for Certain ADs
Accomplishing the actions required by paragraph (g) or (i) of
this AD terminates all requirements of AD 2010-26-05 and AD 2012-02-
18 for the Dassault Aviation Model MYSTERE-FALCON 50 airplanes
specified in those ADs.
Exact source excerpt. Text positions 15278–15543, end exclusive, in the original decoded publication. SHA-256: fc4a4a56cd0571ae5c1725b4af8a46ee455bab14d7d82b26e4576b79f3fe386b
Other FAA AD Provisions
(l) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
International Branch, ANM-116, Transport Airplane Directorate, 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 Branch, send it to ATTN: Tom
Rodriguez, Aerospace Engineer, International Branch, ANM-116,
Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton,
WA 98057-3356; telephone 425-227-1137; fax 425-227-1149. 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. The
AMOC approval letter must specifically reference this AD.
(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
Branch, ANM-116, Transport Airplane Directorate, 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 15543–17055, end exclusive, in the original decoded publication. SHA-256: c2649eb13184d17705d8fb47088e2a0cd11248ee2d50bbc17292e34c3a376a1f
Related Information
(m) Related Information
(1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) EASA Airworthiness Directive 2016-0067, dated April 7, 2016,
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-2016-9569.
(2) For more information about this AD, contact Tom Rodriguez,
Aerospace Engineer, International Branch, ANM-116, Transport
Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-
3356; telephone 425-227-1137; fax 425-227-1149. Information may be
emailed to: [email protected].
(3) Service information identified in this AD that is not
incorporated by reference is available at the addresses specified in
paragraphs (n)(5) and (n)(6) of this AD.
Exact source excerpt. Text positions 17055–17854, end exclusive, in the original decoded publication. SHA-256: b84b5882f9468e2f0057132fb627759bc08728627b495f5615b0d55937788361
Material Incorporated by Reference
(n) 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.
(3) The following service information was approved for IBR as of
June 13, 2017.
(i) Chapter 5-40, Airworthiness Limitations, of the Erratum to
Dassault Falcon 50/50EX Maintenance Manual, Revision 23, dated July
2015.
(ii) Reserved.
(4) The following service information was approved for IBR on
March 19, 2013 (78 FR 9798, February 12, 2013).
(i) Section 05-40/00, Airworthiness Limitations, of Chapter 5-
40, Airworthiness Limitations, of the Dassault Falcon 50/50EX
Maintenance Manual, Revision 21, dated June 2011.
(ii) Reserved.
(5) 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.
(6) You may view this service information at the FAA, Transport
Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For
information on the availability of this material at the FAA, call
425-227-1221.
(7) 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 17854–19512, end exclusive, in the original decoded publication. SHA-256: 7a4122fa6282cbcff1721eacce52c59b8fbcedd88ccba3c99570421b9a38999c
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 2017-09-03 · 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: e2fbbdc3d40578eafb77c445fd740b9958b1fc3329dea758bbfb1fce8c33a496. Source manifest: 5e1533ea1f0324a636b63a7892da27e626a91bea39d9d88432199f6cab8d4cb4.
Official source · 2017-05-09
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 82, Number 88 (Tuesday, May 9, 2017)]
[Rules and Regulations]
[Pages 21467-21469]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2017-08829]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2016-9569; Directorate Identifier 2016-NM-052-AD;
Amendment 39-18865; AD 2017-09-03]
RIN 2120-AA64
Airworthiness Directives; Dassault Aviation Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: We are superseding Airworthiness Directive (AD) 2013-03-12 for
all Dassault Aviation Model MYSTERE-FALCON 50 airplanes. AD 2013-03-12
required revising the maintenance program to incorporate certain
maintenance requirements and airworthiness limitations. This AD
requires revising the maintenance or inspection program, as applicable,
to incorporate new or revised maintenance requirements and
airworthiness limitations. This AD was prompted by issuance of a
revision to the airplane maintenance manual (AMM) that introduces new
or more restrictive maintenance requirements and/or airworthiness
limitations. We are issuing this AD to address the unsafe condition on
these products.
DATES: This AD is effective June 13, 2017.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of June 13,
2017.
The Director of the Federal Register approved the incorporation by
reference of a certain other publication listed in this AD as of March
19, 2013 (78 FR 9798, February 12, 2013).
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 referenced service
information at the FAA, Transport Airplane Directorate, 1601 Lind
Avenue SW., Renton, WA. For information on the availability of this
material at the FAA, call 425-227-1221. It is also available on the
Internet at http://www.regulations.gov by searching for and locating
Docket No. FAA-2016-9569.
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-2016-
9569; or in person at the Docket Management Facility between 9 a.m. and
5 p.m., Monday through Friday, except Federal holidays. The AD docket
contains this AD, the regulatory evaluation, any comments received, and
other information. The street address for the Docket Office (telephone
800-647-5527) is Docket Management Facility, 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 Branch, ANM-116, Transport Airplane Directorate, FAA,
1601 Lind Avenue SW., Renton, WA 98057-3356; telephone 425-227-1137;
fax 425-227-1149.
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 to supersede AD 2013-03-12, Amendment 39-17347 (78 FR 9798,
February 12, 2013) (``AD 2013-03-12''). AD 2013-03-12 applied to all
Dassault Aviation Model MYSTERE-FALCON 50 airplanes. The NPRM published
in the Federal Register on January 6, 2017 (82 FR 1621). The NPRM was
prompted by the issuance of a revision to the AMM that introduced new
or more restrictive maintenance requirements and/or airworthiness
limitations. The NPRM proposed to require revising the maintenance or
inspection program, as applicable, to incorporate new or revised
maintenance requirements and airworthiness limitations. We are issuing
this AD to prevent 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
Airworthiness Directive 2016-0067, dated April 7, 2016 (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 50 airplanes. The MCAI states:
The airworthiness limitations and maintenance requirements for
the Myst[egrave]re Falcon 50 type design are included in DA
Myst[egrave]re Falcon 50 Aircraft Maintenance Manual (AMM) chapter
5-40 and are approved by EASA.
Failure to implement these limitations or accomplish these tasks
could result in an unsafe condition [reduced structural integrity of
the airplane]. Consequently, compliance with these actions has been
identified as mandatory for continued airworthiness.
Consequently, EASA issued AD 2011-0246 [which corresponds to FAA
AD 2013-03-12] to require accomplishment of the maintenance tasks,
and implementation of the airworthiness limitations, as specified in
DA Myst[egrave]re Falcon 50 AMM chapter 5-40 Revision 21.
Since that [EASA] AD was issued, DA issued revision 23 of the
Mystere Falcon 50 AMM chapter 5-40 (hereafter referred to as `the
ALS' in this [EASA] AD), which introduces new and more restrictive
maintenance requirements and/or airworthiness limitations.
The ALS introduces, among others, the following changes:
--Addition of more detailed data regarding SSIP program,
--Task 53-50-35-220-802 ``Detailed inspection of the frame 35 upper
and lower sections'', replacing Task 53-50-35-220-801,
--Task 55-00-00-270-801 ``Ultrasonic inspection for stress corrosion
in stabilizer hinges'', replacing Task 55-00-00-250-801, and
--Task 78-31-00-250-802 ``Special detailed inspection (fluorescent
penetrant) of thrust reverser door hinge fittings'', replacing Task
78-31-00-250-801.
For the reasons described above, this [EASA] AD, retains the
requirements of EASA AD 2011-0246, which is superseded, and requires
the implementation of the maintenance tasks and airworthiness
limitations, as specified in the ALS.
This AD requires revising the maintenance or inspection program, as
[[Page 21468]]
applicable, to incorporate new or revised maintenance requirements and
airworthiness limitations. 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-2016-9569.
Comments
We gave the public the opportunity to participate in developing
this AD. 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 AD 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 correcting 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
We reviewed Chapter 5-40, Airworthiness Limitations, of the Erratum
to Dassault Falcon 50/50EX Maintenance Manual, Revision 23, dated July
2015. This service information describes maintenance requirements and/
or airworthiness limitations. 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 249 airplanes of U.S. registry.
We estimate the following costs to comply with this AD:
Estimated Costs
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
Maintenance program revision (retained 1 work-hour x $85 per $0 $85 $21,165
action from AD 2013-03-12). hour = $85.
Maintenance or inspection program 1 work-hour x $85 per 0 85 21,165
revision (new action). hour = $85.
----------------------------------------------------------------------------------------------------------------
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.
Regulatory Findings
We determined that 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, 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):
2017-09-03 Dassault Aviation: Amendment 39-18865; Docket No. FAA-
2016-9569; Directorate Identifier 2016-NM-052-AD.
(a) Effective Date
This AD is effective June 13, 2017.
(b) Affected ADs
(1) This AD replaces AD 2013-03-12, Amendment 39-17347 (78 FR
9798, February 12, 2013) (``AD 2013-03-12'').
(2) This AD affects AD 2010-26-05, Amendment 39-16544 (75 FR
79952, December 21, 2010) (``AD 2010-26-05''), and AD 2012-02-18,
Amendment 39-16941 (77 FR 12175, February 29, 2012) (``AD-2012-02-
18'').
(c) Applicability
This AD applies to Dassault Aviation Model MYSTERE-FALCON 50
airplanes, certificated in any category, all manufacturer serial
numbers.
(d) Subject
Air Transport Association (ATA) of America Code 05, Periodic
inspections.
(e) Reason
This AD was prompted by a manufacturer revision to the airplane
maintenance manual (AMM) that introduces new or more restrictive
maintenance requirements and/or airworthiness limitations. We are
issuing this AD to prevent reduced structural integrity of the
airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Retained Maintenance Program Revision, With No Changes
This paragraph restates the requirements of paragraph (g) of AD
2013-03-12, with no changes. Within 30 days after March 19, 2013
(the effective date of AD 2013-03-12): Revise the maintenance
program to incorporate all airworthiness limitations and maintenance
tasks specified in Section 05-40/00,
[[Page 21469]]
Airworthiness Limitations, of Chapter 5-40, Airworthiness
Limitations, of the Dassault Falcon 50/50EX Maintenance Manual,
Revision 21, dated June 2011. The initial compliance times for the
tasks are at the applicable times specified in Section 05-40/00,
Airworthiness Limitations, of Chapter 5-40, Airworthiness
Limitations, of the Dassault Falcon 50/50EX Maintenance Manual,
Revision 21, dated June 2011, or within 30 days after March 19,
2013, whichever occurs later.
(h) Retained Provision Regarding Alternative Actions, Intervals, and
Critical Design Configuration Control Limitations (CDCCLs), With New
Exception
This paragraph restates the requirements of paragraph (h) of AD
2013-03-12, with a new exception. Except as required by paragraph
(i) of this AD: After accomplishing the revisions required by
paragraph (g) of this AD, no alternative actions (e.g.,
inspections), intervals, and/or CDCCLs may be used other than those
specified in Section 05-40/00, Airworthiness Limitations, of Chapter
5-40, Airworthiness Limitations, of the Dassault Falcon 50/50EX
Maintenance Manual, Revision 21, dated June 2011, unless the
actions, intervals, and/or CDCCLs are approved as an alternative
methods of compliance (AMOC) in accordance with the procedures
specified in paragraph (l)(1) of this AD.
(i) New Maintenance or Inspection Program Revision
Within 30 days after the effective date of this AD: Revise the
maintenance or inspection program, as applicable, to incorporate
airworthiness limitations, maintenance tasks, and associated
thresholds and intervals specified in Section 05-40/00,
Airworthiness Limitations, of Chapter 5-40, Airworthiness
Limitations, of the Erratum to Dassault Falcon 50/50EX Maintenance
Manual, Revision 23, dated July 2015. The initial compliance times
for the tasks are at the applicable times specified in Section 05-
40/00, Airworthiness Limitations, of Chapter 5-40, Airworthiness
Limitations, of the Erratum to Dassault Falcon 50/50EX Maintenance
Manual, Revision 23, dated July 2015, or within 30 days after the
effective date of this AD, whichever occurs later. Accomplishing the
revision of the maintenance or inspection program required by this
paragraph terminates the requirements of paragraph (g) of this AD.
(j) New Provision Regarding Alternative Actions and Intervals
After the maintenance or inspection program has been revised as
required by paragraph (i) of this AD, no alternative actions (e.g.,
inspections) or intervals may be used unless the actions and
intervals are approved as an AMOC in accordance with the procedures
specified in paragraph (l)(1) of this AD.
(k) Terminating Action for Certain ADs
Accomplishing the actions required by paragraph (g) or (i) of
this AD terminates all requirements of AD 2010-26-05 and AD 2012-02-
18 for the Dassault Aviation Model MYSTERE-FALCON 50 airplanes
specified in those ADs.
(l) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
International Branch, ANM-116, Transport Airplane Directorate, 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 Branch, send it to ATTN: Tom
Rodriguez, Aerospace Engineer, International Branch, ANM-116,
Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton,
WA 98057-3356; telephone 425-227-1137; fax 425-227-1149. 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. The
AMOC approval letter must specifically reference this AD.
(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
Branch, ANM-116, Transport Airplane Directorate, 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.
(m) Related Information
(1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) EASA Airworthiness Directive 2016-0067, dated April 7, 2016,
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-2016-9569.
(2) For more information about this AD, contact Tom Rodriguez,
Aerospace Engineer, International Branch, ANM-116, Transport
Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-
3356; telephone 425-227-1137; fax 425-227-1149. Information may be
emailed to: [email protected].
(3) Service information identified in this AD that is not
incorporated by reference is available at the addresses specified in
paragraphs (n)(5) and (n)(6) of this AD.
(n) 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.
(3) The following service information was approved for IBR as of
June 13, 2017.
(i) Chapter 5-40, Airworthiness Limitations, of the Erratum to
Dassault Falcon 50/50EX Maintenance Manual, Revision 23, dated July
2015.
(ii) Reserved.
(4) The following service information was approved for IBR on
March 19, 2013 (78 FR 9798, February 12, 2013).
(i) Section 05-40/00, Airworthiness Limitations, of Chapter 5-
40, Airworthiness Limitations, of the Dassault Falcon 50/50EX
Maintenance Manual, Revision 21, dated June 2011.
(ii) Reserved.
(5) 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.
(6) You may view this service information at the FAA, Transport
Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For
information on the availability of this material at the FAA, call
425-227-1221.
(7) 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 Renton, Washington, on April 24, 2017.
Paul Bernado,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2017-08829 Filed 5-8-17; 8:45 am]
BILLING CODE 4910-13-P
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