AD 2018-18-05

We are adopting a new airworthiness directive (AD) for certain ATR-GIE Avions de Transport R[eacute]gional Model ATR42-200, -300, and -320 airplanes. This AD was prompted by a determination that more restrictive maintenance instructions and airworthiness limitations are necessary. This AD requires updating 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.

Final rule.

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):

2018-18-05 ATR-GIE Avions de Transport R[eacute]gional: Amendment 39-19384; Docket No. FAA-2018-0391; Product Identifier 2017-NM-165- AD.

(a) Effective Date

This AD is effective October 5, 2018.

(b) Affected ADs

This AD affects the ADs specified in paragraphs (b)(1), (b)(2), and (b)(3) of this AD.
(1) AD 2000-17-09, Amendment 39-11883 (65 FR 53897, September 6, 2000) (``AD 2000-17-09'').
(2) AD 2008-04-19 R1, Amendment 39-16069 (74 FR 56713, November 3, 2009) (``AD 2008-04-19 R1'').
(3) AD 2015-26-09, Amendment 39-18357 (81FR 1483, January 13, 2016) (``AD 2015-26-09'').

(c) Applicability

This AD applies to ATR-GIE Avions de Transport R[eacute]gional Model ATR42-200, -300, and -320 airplanes, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness dated on or before October 17, 2016.

(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 instructions and airworthiness limitations are necessary. 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) 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 the information specifiedin the Airworthiness Limitations (ALS) and Certification Maintenance Requirements (CMR) sections of ATR ATR42- 200/-300/-320, Time Limits Document (TL), Revision 8, dated October 17, 2016. The initial compliance time for accomplishing the tasks is at the applicable times specified in the ALS and CMR sections of ATR ATR42-200/-300/-320, Time Limits Document (TL), Revision 8, dated October 17, 2016, or within 90 days after the effective date of this AD, whichever occurs later, except as specified in paragraph (h) of this AD.

(h) Initial Compliance Times for Certain CMR Tasks

For the CMR tasks listed in figure 1 to paragraph (h) of this AD, the initial compliance time for accomplishing the tasks is at the applicable time specified in the ALS and CMR sections of ATR ATR42-200/-300/-320, Time Limits Document (TL), Revision 8, dated October 17, 2016, or within the compliance time specified in figure 1 to paragraph (h) of this AD, whichever occurs later.

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(i) No Alternative Actions and Intervals

After the maintenance or inspection program, as applicable, 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 (k)(1) of this AD.

(j) Terminating Action for Certain ADs

Accomplishing the actions required by this AD terminates all requirements of AD 2000-17-09, AD 2008-04-19 R1, and AD 2015-26-09 for ATR--GIE Avions de Transport R[eacute]gional Model ATR42-200, - 300, and -320 airplanes only.

(k) 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 (l)(2) of this AD. Information may be emailed to: 9-ANM-116-AMOC-REQUESTS@faa.gov. 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.

(l) Related Information

(1) Refer to Mandatory Continuing Airworthiness Information (MCAI) EASA AD 2017-0221R1, dated December 15, 2017, 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-2018-0391.
(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 980198; telephone and fax 206-231-3220.

(m) 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 ATR42-200/-300/-320, Time Limits Document (TL), Revision 8, dated October 17, 2016.
(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; 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.
(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.

Discussion

We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply to certain ATR-GIE Avions de Transport R[eacute]gional Model ATR42-200, -300, and -320 airplanes. The NPRM published in the Federal Register on May 9, 2018 (83 FR 21191). The NPRM was prompted by a determination that more restrictive maintenance instructions and airworthiness limitations are necessary. The NPRM proposed to require updating the maintenance or inspection program, as applicable, to incorporate new or more restrictive maintenance requirements and airworthiness limitations.
The European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Union, has issued EASA AD 2017-0221R1, dated December 15, 2017 (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 ATR42-200, -300, and -320 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 ATR42-200/-300/-320 Time Limits (TL) document. These instructions have been identified as mandatory for continued airworthiness.
Failure to accomplish these instructions could result in an unsafe condition.
Consequently, ATR published Revision 8 of the ATR42-200/-300/- 320 TL document, which contains new and/or more restrictive CMRs and airworthiness limitation tasks.
For the reasons described above, this [EASA] AD requires accomplishment of the actions specified in the ATR42-200/-300/-320 TL document Revision 8, hereafter referred to as `the TLD' in this [EASA] AD.
This [EASA] AD, in conjunction with two other [EASA] ADs related to ATR 42-400/-500 (EASA AD 2017-0222) and ATR 72-101/-102/-201/- 202/-211/-212/-212A (EASA AD 2017-0223) aeroplanes, retains the requirements of EASA AD 2009-0242 [which corresponds to FAA AD 2008- 04-19 R1, Amendment 39-16069 (74 FR 56713, November 3, 2009) (``AD 2008-04-19 R1'')] and EASA AD 2012-1093 [which corresponds to FAA AD 2015-26-09, Amendment 39-18357 (81 FR 1483, January 13, 2016) (``AD 2015-26-09'')]. EASA plans, when all these three ADs are effective, to cancel EASA AD 2009-0242 and EASA AD 2012-0193.
This [EASA] AD is revised to provide the correct issue date (17 October 2016) of the TLD. The original [EASA] AD inadvertently referenced the EASA approval date for that document.

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- 0391.

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

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

Related Service Information Under 1 CFR Part 51

ATR-GIE Avions de Transport R[eacute]gional has issued ATR42-200/- 300/-320, Time Limits Document (TL), Revision 8, dated October 17, 2016. This service information describes life limits and maintenance requirements for the affected airplanes. 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 33 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.