Published 2019-07-22 · Federal Register document 2019-15447
Airworthiness Directives; ATR-GIE Avions de Transport Régional Airplanes
Publication summary
The FAA is adopting a new airworthiness directive (AD) for certain ATR-GIE Avions de Transport R[eacute]gional Model ATR72 airplanes. This AD was prompted by a determination that new or more restrictive maintenance instructions and airworthiness limitations are necessary. This AD requires revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive maintenance instructions and airworthiness limitations. The FAA is issuing this AD to address the unsafe condition on these products.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:24:01.312311+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2019-66422190cf4fa9dc
- Source row
- results[145]
- Raw source SHA-256
- 66422190cf4fa9dc96bac02b1afe14648e349a1393bef6cf5fbf55644fa2ce43
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2019-13-04
- Effective date printed in this edition
- 2019-08-26
Read 14 complete recorded clauses
Effective Date
(a) Effective Date
This AD is effective August 26, 2019.
Exact source excerpt. Text positions 12175–12238, end exclusive, in the original decoded publication. SHA-256: 204ac7c8ee7d4858065ab4b17d7989eac1c7c4263c959b83fea07a4a0edd9114
Affected ADs
(b) Affected ADs
This AD affects AD 2018-14-11, Amendment 39-19331 (83 FR 34031,
July 19, 2018) (``AD 2018-14-11''); AD 2000-23-26, Amendment 39-
11999 (65 FR 70775, November 28, 2000) (``AD 2000-23-26''); and AD
2008-04-19 R1, Amendment 39-16069 (74 FR 56713, November 3, 2009)
(``AD 2008-04-19 R1'').
Exact source excerpt. Text positions 12238–12550, end exclusive, in the original decoded publication. SHA-256: facd9bf9c60109e9c019b031559cd5df2574acef3d6859ead805df8fe9233b25
Applicability wording · Applicability
(c) Applicability
This AD applies to ATR-GIE Avions de Transport R[eacute]gional
Model ATR72-101, -102, -201, -202, -211, -212, and -212A airplanes,
certificated in any category, with an original airworthiness
certificate or original export certificate of airworthiness issued
on or before January 30, 2018.
Exact source excerpt. Text positions 12550–12868, end exclusive, in the original decoded publication. SHA-256: 757804f281dea44c2b09c64d1feaadb69c4be3bcf4d262aa32c51378b0dcd042
Subject
(d) Subject
Air Transport Association (ATA) of America Code 05, Time Limits/
Maintenance Checks.
Exact source excerpt. Text positions 12868–12971, end exclusive, in the original decoded publication. SHA-256: b15263823fded4455be00ff56d3a178d819d56a04f0615355cdb43771d1bcef9
Reason
(e) Reason
This AD was prompted by a determination that new or more
restrictive maintenance instructions and airworthiness limitations
are necessary. The FAA is issuing this AD to prevent fatigue
cracking and damage in principal structural elements, which could
result in reduced structural integrity of the airplane.
Exact source excerpt. Text positions 12971–13299, end exclusive, in the original decoded publication. SHA-256: 1da0aee978b7e848f8cb9cca2a6f266f542a5d7fa86700ec6b560cd7877a72a1
Compliance
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
Exact source excerpt. Text positions 13299–13401, 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
existing maintenance or inspection program, as applicable, to
incorporate the information specified in ATR ATR72 Time Limits
Document, Revision 16, dated January 30, 2018. The initial
compliance time for doing the tasks is at the time specified in ATR
ATR72 Time Limits Document, Revision 16, dated January 30, 2018, or
within 90 days after the effective date of this AD, whichever occurs
later, except as provided by paragraphs (h) and (i) of this AD.
Exact source excerpt. Text positions 13401–13977, end exclusive, in the original decoded publication. SHA-256: 0b6759ea5c073da2f9bfce88be4d1d5827942bbed76a9044d60670b134bd79ea
Initial Compliance Times for Certain Tasks
(h) Initial Compliance Times for Certain Tasks
For accomplishing airworthiness limitations (AWL) and
certification maintenance requirement (CMR)/maintenance significant
item (MSI) tasks identified in figure 1 to paragraph (h) of this AD,
the initial compliance time is at the applicable time specified in
the airworthiness limitations section (ALS) of the ATR ATR72 Time
Limits Document, Revision 16, dated January 30, 2018, or at the
applicable compliance time in figure 1 to paragraph (h) of this AD,
whichever occurs later.
[GRAPHIC] [TIFF OMITTED] TR22JY19.002
Exact source excerpt. Text positions 13977–14555, end exclusive, in the original decoded publication. SHA-256: fc8fe06d7ef0726e6fc04169eb9aae982f56ebf7c1ca44dcb3849df6d11aaf68
Initial Compliance Time: One-Time Initial Threshold
(i) Initial Compliance Time: One-Time Initial Threshold
For CMR task 220000-5, a one-time initial threshold, as
specified in ATR ATR72 Time Limits Document, Revision 16, dated
January 30, 2018, is allowed as specified in figure 2 to paragraph
(i) of this AD.
[GRAPHIC] [TIFF OMITTED] TR22JY19.003
Exact source excerpt. Text positions 14555–14861, end exclusive, in the original decoded publication. SHA-256: b53591a9aa18951ad30c304b987add66e1857b14ff2d6e4cde232bc7ccdb0bb9
No Alternative Actions and Intervals
(j) No Alternative Actions and Intervals
After the existing maintenance or inspection program has been
revised as required by paragraph (g) of this AD, no alternative
actions (e.g., inspections) and intervals may be used unless the
actions and intervals are approved as an alternative method of
compliance (AMOC) in accordance with the procedures specified in
paragraph (l)(1) of this AD.
Exact source excerpt. Text positions 14861–15261, end exclusive, in the original decoded publication. SHA-256: 410ad7e402b7afd4e5b3707b7d97f6eff080c7c04aa74fdd95697c021b23fc6a
Terminating Action for AD 2018-14-11, AD 2000-23-26, and AD 2008- 04-19 R1
(k) Terminating Action for AD 2018-14-11, AD 2000-23-26, and AD 2008-
04-19 R1
Accomplishing the actions required by this AD terminates all
requirements of AD 2018-14-11, AD 2000-23-26, and AD 2008-04-19 R1.
[[Page 35031]]
Exact source excerpt. Text positions 15261–15492, end exclusive, in the original decoded publication. SHA-256: da3f0f53bc1c208669d53353cfef82b5c9527e73ee249a6c9ef42300ad81935a
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 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 (m)(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 ATR-GIE Avions de Transport
R[eacute]gional's EASA Design Organization Approval (DOA). If
approved by the DOA, the approval must include the DOA-authorized
signature.
Exact source excerpt. Text positions 15492–16818, end exclusive, in the original decoded publication. SHA-256: 8b01bb9518d79ea8f282944dcfae48317c19aa76bc16ce7a776ead923c131c51
Related Information
(m) Related Information
(1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) EASA AD 2018-0184, dated August 28, 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-2018-1069.
(2) For more information about this AD, contact Shahram
Daneshmandi, Aerospace Engineer, International Section, Transport
Standards Branch, FAA, 2200 South 216th St., Des Moines, WA 98198;
telephone and fax 206-231-3220.
Exact source excerpt. Text positions 16818–17356, end exclusive, in the original decoded publication. SHA-256: f30df4748165b97ed8ef13c6a9dd7967dc7034e78c85f78be8ff16c6b10356cd
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.
(i) ATR ATR72 Time Limits Document, Revision 16, dated January
30, 2018.
(ii) [Reserved]
(3) For service information identified in this AD, contact ATR-
GIE Avions de Transport R[eacute]gional, 1 All[eacute]e Pierre
Nadot, 31712 Blagnac Cedex, France; telephone +33 (0) 5 62 21 62 21;
fax +33 (0) 5 62 21 67 18; email aircraft.com">continued.airworthiness@atr-aircraft.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 17356–18618, end exclusive, in the original decoded publication. SHA-256: 26970f1c0a3b20312cc4548d40eec6f565e7b49ef09f50b203995a93b386d477
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 2019-13-04 · 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: 72828e0ad93b41b234826ff84f0915b19d51354cf75b55bd695775d4dfc59698. Source manifest: b287ebf3329ee3ff81f4b7eecca24621f7ec645477956ad9bc80b80f70ae2076.
Official source · 2019-07-22
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 84, Number 140 (Monday, July 22, 2019)]
[Rules and Regulations]
[Pages 35028-35031]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2019-15447]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2018-1069; Product Identifier 2018-NM-128-AD; Amendment
39-19677; AD 2019-13-04]
RIN 2120-AA64
Airworthiness Directives; ATR-GIE Avions de Transport
R[eacute]gional Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain ATR-GIE Avions de Transport R[eacute]gional Model ATR72
airplanes. This AD was prompted by a determination that new or more
restrictive maintenance instructions and airworthiness limitations are
necessary. This AD requires revising the existing maintenance or
inspection program, as applicable, to incorporate new or more
restrictive maintenance instructions and airworthiness limitations. The
FAA is issuing this AD to address the unsafe condition on these
products.
DATES: This AD is effective August 26, 2019.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of August 26,
2019.
ADDRESSES: For service information identified in this final rule,
contact ATR-GIE Avions de Transport R[eacute]gional, 1 All[eacute]e
Pierre Nadot, 31712 Blagnac Cedex, France; telephone +33 (0) 5 62 21 62
21; fax +33 (0) 5 62 21 67 18; email aircraft.com">continued.airworthiness@atr-aircraft.com; internet http://www.atr-aircraft.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-2018-1069.
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-
1069; 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 is 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: Shahram Daneshmandi, Aerospace
Engineer, International Section, Transport Standards Branch, FAA, 2200
South 216th St., Des Moines, WA 98198; telephone and fax 206-231-3220.
SUPPLEMENTARY INFORMATION:
Discussion
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by adding an AD that would apply to all ATR-GIE Avions de
Transport R[eacute]gional Model ATR72 airplanes. The NPRM published in
the Federal Register on February 14, 2019 (84 FR 4012). The NPRM was
prompted by a determination that new or more restrictive maintenance
instructions and airworthiness limitations are necessary. The NPRM
proposed to require revising the existing maintenance or inspection
program, as applicable, to incorporate new or more restrictive
maintenance instructions and airworthiness limitations.
The FAA is issuing this AD to address fatigue cracking and damage
in principal structural elements, which 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
2018-0184, dated August 28, 2018 (referred to after this as the
Mandatory Continuing Airworthiness Information, or ``the MCAI''), to
correct an unsafe condition for all ATR-GIE Avions de Transport
R[eacute]gional Model ATR72 airplanes. The MCAI states:
The airworthiness limitations and certification maintenance
requirements (CMR) for ATR aeroplanes, which are approved by EASA,
are currently defined and published in the TLD [time limits
document]. These instructions have been identified as mandatory for
continued airworthiness.
Failure to accomplish these instructions could result in an
unsafe condition.
Previously, EASA issued AD 2017-0223 (later revised) to require
accomplishment of the actions specified in the TLD at Revision 15.
Since EASA AD 2017-0223R1 [which corresponds to FAA AD 2018-14-
11, Amendment 39-19331 (83 FR 34031, July 19, 2018) (``AD 2018-14-
11'')] was issued, ATR published Revision 16 of the TLD for ATR 72
aeroplanes, introducing new and/or more
[[Page 35029]]
restrictive airworthiness limitations and/or maintenance actions.
For the reasons described above, this [EASA] AD retains the
requirements of EASA AD 2017-0223R1, which is superseded, and
requires accomplishment of the actions specified in the TLD.
This AD requires revising the existing maintenance or inspection
program to incorporate certain maintenance instructions and
airworthiness limitations. The unsafe condition is fatigue cracking and
damage in principal structural elements, which could result in reduced
structural integrity of the airplane. 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-2018-1069.
Comments
The FAA gave the public the opportunity to participate in
developing this final rule. The following presents the comment received
on the NPRM and the FAA's response.
Request To Clarify the Proposed Terminating Action
Empire Airlines requested clarification of the terminating action
specified in the proposed AD. Empire Airlines pointed out that
paragraph (k) of the proposed AD stated that accomplishing the actions
required by the proposed AD would terminate all requirements of AD
2018-14-11. Empire Airlines explained that paragraph (j) of AD 2018-14-
11 states that, accomplishing the actions required by paragraph (g) of
that AD terminates all requirements of AD 2000-23-26, Amendment 39-
11999 (65 FR 70775, November 28, 2000); and AD 2008-04-19 R1, Amendment
39-16069 (74 FR 56713, November 3, 2009). Therefore, Empire Airlines
asked if the terminating action specified in paragraph (j) of AD 2018-
14-11 is still applicable in the proposed AD.
The FAA agrees to provide clarification for the commenter.
Paragraph (k) of the proposed AD stated that accomplishing the proposed
actions would terminate all requirements of AD 2018-14-11, including
paragraph (j) of AD 2018-14-11, which terminates all requirements of AD
2000-23-26 and AD 2008-04-19 R1. However, the FAA's intent is that
paragraph (k) of the proposed AD terminates all requirements of AD
2000-23-26 and AD 2008-04-19 R1, along with AD 2018-14-11. Therefore,
the agency has revised paragraph (k) of this AD to specify that the
actions required by this AD also terminate the requirements of AD 2000-
23-26 and AD 2008-04-19 R1.
Conclusion
The FAA reviewed the relevant data, considered the comments
received, and determined that air safety and the public interest
require adopting this final rule with the changes described previously
and minor editorial changes. The FAA has 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.
The FAA has also determined that these changes will not increase
the economic burden on any operator or increase the scope of this final
rule.
Related Service Information Under 1 CFR Part 51
ATR-GIE Avions de Transport R[eacute]gional has issued ATR72 Time
Limits Document, Revision 16, dated January 30, 2018. This service
information describes preventive maintenance requirements and includes
updated limitations, tasks, thresholds and intervals to be incorporated
into the existing maintenance or inspection program.
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
The FAA estimates that this AD affects 23 airplanes of U.S.
registry. The agency estimates the following costs to comply with this
AD:
The FAA determined that revising the existing maintenance or
inspection program takes an average of 90 work-hours per operator,
although the agency recognizes that this number may vary from operator
to operator. In the past, the FAA has estimated that this action takes
1 work-hour per airplane. Since operators incorporate maintenance or
inspection program changes for their affected fleet(s), the agency has
determined that a per-operator estimate is more accurate than a per-
airplane estimate. Therefore, the FAA estimates 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.
The FAA is 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) Will not affect intrastate aviation in Alaska, 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.
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:
[[Page 35030]]
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):
2019-13-04 ATR-GIE Avions de Transport R[eacute]gional: Amendment
39-19677; Docket No. FAA-2018-1069; Product Identifier 2018-NM-128-
AD.
(a) Effective Date
This AD is effective August 26, 2019.
(b) Affected ADs
This AD affects AD 2018-14-11, Amendment 39-19331 (83 FR 34031,
July 19, 2018) (``AD 2018-14-11''); AD 2000-23-26, Amendment 39-
11999 (65 FR 70775, November 28, 2000) (``AD 2000-23-26''); and AD
2008-04-19 R1, Amendment 39-16069 (74 FR 56713, November 3, 2009)
(``AD 2008-04-19 R1'').
(c) Applicability
This AD applies to ATR-GIE Avions de Transport R[eacute]gional
Model ATR72-101, -102, -201, -202, -211, -212, and -212A airplanes,
certificated in any category, with an original airworthiness
certificate or original export certificate of airworthiness issued
on or before January 30, 2018.
(d) Subject
Air Transport Association (ATA) of America Code 05, Time Limits/
Maintenance Checks.
(e) Reason
This AD was prompted by a determination that new or more
restrictive maintenance instructions and airworthiness limitations
are necessary. The FAA is issuing this AD to prevent fatigue
cracking and damage in principal structural elements, which 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
existing maintenance or inspection program, as applicable, to
incorporate the information specified in ATR ATR72 Time Limits
Document, Revision 16, dated January 30, 2018. The initial
compliance time for doing the tasks is at the time specified in ATR
ATR72 Time Limits Document, Revision 16, dated January 30, 2018, or
within 90 days after the effective date of this AD, whichever occurs
later, except as provided by paragraphs (h) and (i) of this AD.
(h) Initial Compliance Times for Certain Tasks
For accomplishing airworthiness limitations (AWL) and
certification maintenance requirement (CMR)/maintenance significant
item (MSI) tasks identified in figure 1 to paragraph (h) of this AD,
the initial compliance time is at the applicable time specified in
the airworthiness limitations section (ALS) of the ATR ATR72 Time
Limits Document, Revision 16, dated January 30, 2018, or at the
applicable compliance time in figure 1 to paragraph (h) of this AD,
whichever occurs later.
[GRAPHIC] [TIFF OMITTED] TR22JY19.002
(i) Initial Compliance Time: One-Time Initial Threshold
For CMR task 220000-5, a one-time initial threshold, as
specified in ATR ATR72 Time Limits Document, Revision 16, dated
January 30, 2018, is allowed as specified in figure 2 to paragraph
(i) of this AD.
[GRAPHIC] [TIFF OMITTED] TR22JY19.003
(j) No Alternative Actions and Intervals
After the existing maintenance or inspection program has been
revised as required by paragraph (g) of this AD, no alternative
actions (e.g., inspections) and intervals may be used unless the
actions and intervals are approved as an alternative method of
compliance (AMOC) in accordance with the procedures specified in
paragraph (l)(1) of this AD.
(k) Terminating Action for AD 2018-14-11, AD 2000-23-26, and AD 2008-
04-19 R1
Accomplishing the actions required by this AD terminates all
requirements of AD 2018-14-11, AD 2000-23-26, and AD 2008-04-19 R1.
[[Page 35031]]
(l) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): 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 (m)(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 ATR-GIE Avions de Transport
R[eacute]gional'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 AD 2018-0184, dated August 28, 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-2018-1069.
(2) For more information about this AD, contact Shahram
Daneshmandi, Aerospace Engineer, International Section, Transport
Standards Branch, FAA, 2200 South 216th St., Des Moines, WA 98198;
telephone and fax 206-231-3220.
(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.
(i) ATR ATR72 Time Limits Document, Revision 16, dated January
30, 2018.
(ii) [Reserved]
(3) For service information identified in this AD, contact ATR-
GIE Avions de Transport R[eacute]gional, 1 All[eacute]e Pierre
Nadot, 31712 Blagnac Cedex, France; telephone +33 (0) 5 62 21 62 21;
fax +33 (0) 5 62 21 67 18; email aircraft.com">continued.airworthiness@atr-aircraft.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 July 1, 2019.
Michael Kaszycki,
Acting Director, System Oversight Division, Aircraft Certification
Service.
[FR Doc. 2019-15447 Filed 7-19-19; 8:45 am]
BILLING CODE 4910-13-P
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