82 FR 24027 - Airworthiness Directives; Airbus Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 82, Issue 100 (May 25, 2017)
Federal Aviation Administration
Federal Register Volume 82, Issue 100 (May 25, 2017)
| Page Range | 24027-24030 | |
| FR Document | 2017-10285 |
[Federal Register Volume 82, Number 100 (Thursday, May 25, 2017)] [Rules and Regulations] [Pages 24027-24030] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2017-10285] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2015-0084; Directorate Identifier 2014-NM-181-AD; Amendment 39-18879; AD 2017-10-05] RIN 2120-AA64 Airworthiness Directives; Airbus Airplanes AGENCY: Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule. ----------------------------------------------------------------------- SUMMARY: We are adopting a new airworthiness directive (AD) for certain Airbus Model A300 series airplanes; and Model A300 B4-600, B4-600R, and F4-600R series airplanes, and Model A300 C4-605R Variant F airplanes (collectively called Model A300-600 series airplanes). This AD was prompted by reports indicating that on airplanes that received a certain repair following crack findings, cracks can re-initiate. This AD requires repetitive inspections of the center wing frame (FR) 40 lower outboard radius for cracking, and related investigative and corrective actions if necessary. We are issuing this AD to address the unsafe condition on these products. DATES: This AD is effective June 29, 2017. The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of June 29, 2017. ADDRESSES: For service information identified in this final rule, contact Airbus SAS, Airworthiness Office--EAW, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France; telephone +33 5 61 93 36 96; fax +33 5 61 93 44 51; email [email protected]; Internet http://www.airbus.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-2015- 0084. 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-2015- 0084; or in person at the Docket Management Facility between 9 a.m. [[Page 24028]] 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: Dan Rodina, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356; telephone 425-227-2125; fax 425-227-1149. SUPPLEMENTARY INFORMATION: Discussion We issued a supplemental notice of proposed rulemaking (SNPRM) to amend 14 CFR part 39 by adding an AD that would apply to certain Airbus Model A300 series airplanes; and Model A300 B4-600, B4-600R, and F4- 600R series airplanes, and Model A300 C4-605R Variant F airplanes (collectively called Model A300-600 series airplanes). The SNPRM published in the Federal Register on November 10, 2016 (81 FR 78944) (``the SNPRM''). We preceded the SNPRM with a notice of proposed rulemaking (NPRM) that published in the Federal Register on February 13, 2015 (80 FR 7992) (``the NPRM''). The NPRM proposed to require repetitive inspections for cracking of the FR 40 forward fittings for airplanes previously repaired. The NPRM was prompted by reports indicating that, on airplanes that received a certain repair following crack findings, cracks can re-initiate. The SNPRM proposed to require repetitive rototest, ultrasonic, high frequency eddy current, special detailed, and liquid penetrant inspections, as applicable, of the center wing FR 40 lower outboard radius for cracking, and related investigative and corrective actions if necessary. The SNPRM also proposed to add airplanes to the applicability. We are issuing this AD to detect and correct cracking on the FR 40 forward fittings, 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 Airworthiness Directive 2015-0232R1, dated December 16, 2015 (referred to after this as the Mandatory Continuing Airworthiness Information, or ``the MCAI''), to correct an unsafe condition for certain Airbus Model A300 series airplanes; and Model A300 B4-600, B4-600R, and F4-600R series airplanes, and Model A300 C4-605R Variant F airplanes (collectively called Model A300-600 series airplanes). The MCAI states: Cracks were found on the lower outboard radius of the centre wing frame 40 forward fitting on in-service aeroplanes. This condition, if not detected and corrected, could lead to reduced structural integrity of the aeroplane. To address this unsafe condition, Airbus issued several inspection Service Bulletins (SB) and repair instructions. Consequently, EASA issued AD 2009-0094, which was later superseded by EASA AD 2011-0163 [which corresponds to FAA AD 2012-25-06, Amendment 39-17287 (77 FR 75833, December 26, 2012) (``AD 2012-25- 06'')] and [EASA] AD 2014-0199 [which corresponds to the FAA NPRM], to require repetitive inspections and corrective actions on the affected areas. Since those [EASA] ADs were issued, additional in-service findings induced Airbus to do a new fatigue analysis, using a detailed Finite Element Model study, which resulted in defining new inspection methods. Prompted by these results, Airbus issued SB A300-57-0261, SB A300-57-6117 and SB A300-57-9034 to introduce these inspections. These new inspection SBs supersede and render obsolete inspection SB A300-53-0268 and SB A300-57-6052 and the All Operators Transmissions (AOT) A300-53A0391, AOT A300-57A6111, AOT A300-53W002- 14 and AOT A300-57W003-14. For the reasons described above, EASA issued AD 2015-0232, superseding [Direction G[eacute]n[eacute]rale de l'Aviation Civile] DGAC France AD 1998-038-010(B) R1 [which corresponds to FAA AD 98- 25-07, Amendment 39-10933 (63 FR 68167, December 10, 1998) (``AD 98- 25-07'')] and [DGAC France] AD 2003-189(B), and EASA AD 2011-0163 and [EASA] AD 2014-0199, to require the new inspections of the affected areas within new thresholds and intervals. This [EASA] AD is revised to clarify the compliance time(s), introducing a Note after paragraph (1), and to alleviate the reporting requirements of paragraph (3). Required actions include repetitive rototest, ultrasonic, high frequency eddy current, special detailed, and liquid penetrant inspections, as applicable, of the center wing FR 40 lower outboard radius for cracking, and related investigative and corrective actions if necessary. 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-2015- 0084. Comments We gave the public the opportunity to participate in developing this AD. We received no comments on the SNPRM 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:Are consistent with the intent that was proposed in the SNPRM for correcting the unsafe condition; and Do not add any additional burden upon the public than was already proposed in the SNPRM. Related Service Information Under 1 CFR Part 51 We reviewed the following service information: Airbus Service Bulletin A300-57-6117, dated May 28, 2015. Airbus Service Bulletin A300-57-0261, dated June 11, 2015. The service information describes procedures for repetitive ultrasonic, rototest, high frequency eddy current, special detailed, and liquid penetrant inspections, and related investigative and corrective actions. These documents are distinct since they apply to different airplane models. 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 29 airplanes of U.S. registry. We estimate the following costs to comply with this AD. Estimated Costs ---------------------------------------------------------------------------------------------------------------- Action Labor cost Cost per product Cost on U.S. operators ---------------------------------------------------------------------------------------------------------------- Inspections.......................... Up to 91 work-hours x Up to $7,735 per Up to $224,315 per $85 per hour = $7,735 inspection cycle. inspection cycle. per inspection cycle. Reporting............................ 1 work-hour x $85 per $85.................... $2,465. hour = $85. ---------------------------------------------------------------------------------------------------------------- [[Page 24029]] We have received no definitive data that would enable us to provide cost estimates for the on-condition actions specified in this AD. Paperwork Reduction Act A federal agency may not conduct or sponsor, and a person is not required to respond to, nor shall a person be subject to penalty for failure to comply with a collection of information subject to the requirements of the Paperwork Reduction Act unless that collection of information displays a current valid OMB control number. The control number for the collection of information required by this AD is 2120- 0056. The paperwork cost associated with this AD has been detailed in the Costs of Compliance section of this document and includes time for reviewing instructions, as well as completing and reviewing the collection of information. Therefore, all reporting associated with this AD is mandatory. Comments concerning the accuracy of this burden and suggestions for reducing the burden should be directed to the FAA at 800 Independence Ave. SW., Washington, DC 20591, ATTN: Information Collection Clearance Officer, AES-200. 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): 2017-10-05 Airbus: Amendment 39-18879; Docket No. FAA-2015-0084; Directorate Identifier 2014-NM-181-AD. (a) Effective Date This AD is effective June 29, 2017. (b) Affected ADs This AD affects AD 98-25-07, Amendment 39-10933 (63 FR 68167, December 10, 1998) (``AD 98-25-07''); and AD 2012-25-06, Amendment 39-17287 (77 FR 75833, December 26, 2012) (``AD 2012-25-06''). (c) Applicability This AD applies to the Airbus airplanes, certificated in any category, identified in paragraphs (c)(1) through (c)(5) of this AD, except airplanes on which Airbus Modification 10221 has been embodied in production. (1) Model A300 B2-1A, B2-1C, B2K-3C, B2-203, B4-2C, B4-103, and B4-203 airplanes. (2) Model A300 B4-601, B4-603, B4-620, and B4-622 airplanes. (3) Model A300 B4-605R and B4-622R airplanes. (4) Model A300 F4-605R and F4-622R airplanes. (5) Model A300 C4-605R Variant F airplanes. (d) Subject Air Transport Association (ATA) of America Code 57, Wings. (e) Reason This AD was prompted by reports of cracks on the lower outboard radius of the center wing frame (FR) 40 forward fitting. We are issuing this AD to detect and correct cracking on the FR 40 forward fittings, 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) Repetitive Inspections Except as provided by paragraph (i)(1) of this AD, at the applicable times specified in paragraph 1.E.(2), ``Compliance,'' of Airbus Service Bulletin A300-57-0261, dated June 11, 2015; or Airbus Service Bulletin A300-57-6117, dated May 28, 2015; accomplish rototest, ultrasonic, high frequency eddy current, special detailed, and liquid penetrant inspections, as applicable, of the center wing FR 40 lower outboard radius for cracking, and do all applicable related investigative actions, in accordance with the Accomplishment Instructions of Airbus Service Bulletin A300-57-0261, dated June 11, 2015; or Airbus Service Bulletin A300-57-6117, dated May 28, 2015; as applicable. Do all applicable related investigative actions before further flight. Repeat the inspections thereafter at the applicable times specified in paragraph 1.E. (2), ``Compliance,'' of Airbus Service Bulletin A300-57-0261, dated June 11, 2015; or Airbus Service Bulletin A300-57-6117, dated May 28, 2015. (h) Corrective Actions If, during any inspection required by paragraph (g) of this AD, any crack is found, before further flight, accomplish the applicable corrective actions, in accordance with the Accomplishment Instructions of Airbus Service Bulletin A300-57-0261, dated June 11, 2015; or Airbus Service Bulletin A300-57-6117, dated May 28, 2015; as applicable; except as required by paragraph (i)(2) of this AD. (i) Service Information Exception (1) Where the service information specified in paragraph (g) of this AD specifies a compliance time ``from this service bulletin issuance date,'' this AD requires compliance within the specified compliance time after the effective date of this AD. (2) Where the service information specified in paragraph (h) of this AD specifies to contact Airbus for certain conditions, before further flight, repair using a method approved by the Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA; or the European Aviation Safety Agency (EASA); or Airbus's EASA Design Organization Approval (DOA). (j) No Terminating Action for This AD Accomplishing a corrective action required by paragraph (h) of this AD, or accomplishing a preventative action specified in Airbus Service Bulletin A300-57-0260 or A300-57-6116, as applicable, does not terminate the repetitive inspections required by paragraph (g) of this AD. [[Page 24030]] (k) Terminating Action for Certain Requirements of Other ADs (1) Accomplishing the actions required by paragraph (g) of this AD terminates the actions required by paragraphs (a) and (b) of AD 98-25-07. (2) Accomplishing the actions required by paragraph (g) of this AD terminates the actions required by paragraphs (i) and (j) of AD 2012-25-06. (l) Reporting Requirements Within 60 days after any inspection required by paragraph (g) of this AD, or within 60 days after the effective date of this AD, whichever occurs later, report any findings, positive or negative, to Airbus Service Bulletin Reporting Online Application on Airbus World (https://w3.airbus.com/). (m) 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: Dan Rodina, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057- 3356; telephone 425-227-2125; 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. (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 EASA; or Airbus's EASA DOA. If approved by the DOA, the approval must include the DOA-authorized signature. (3) Reporting Requirements: A federal agency may not conduct or sponsor, and a person is not required to respond to, nor shall a person be subject to a penalty for failure to comply with a collection of information subject to the requirements of the Paperwork Reduction Act unless that collection of information displays a current valid OMB Control Number. The OMB Control Number for this information collection is 2120-0056. Public reporting for this collection of information is estimated to be approximately 5 minutes per response, including the time for reviewing instructions, completing and reviewing the collection of information. All responses to this collection of information are mandatory. Comments concerning the accuracy of this burden and suggestions for reducing the burden should be directed to the FAA at: 800 Independence Ave. SW., Washington, DC 20591, Attn: Information Collection Clearance Officer, AES-200. (n) Related Information (1) Refer to Mandatory Continuing Airworthiness Information (MCAI) EASA Airworthiness Directive 2015-0232R1, dated December 16, 2015, 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-2015-0084. (2) Service information identified in this AD that is not incorporated by reference is available at the addresses specified in paragraphs (o)(3) and (o)(4) of this AD. (o) 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) Airbus Service Bulletin A300-57-0261, dated June 11, 2015. (ii) Airbus Service Bulletin A300-57-6117, dated May 28, 2015. (3) For service information identified in this AD, contact Airbus SAS, Airworthiness Office--EAW, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France; telephone +33 5 61 93 36 96; fax +33 5 61 93 44 51; email [email protected]; Internet http://www.airbus.com. (4) 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. (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 Renton, Washington, on May 2, 2017. Michael Kaszycki, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2017-10285 Filed 5-24-17; 8:45 am] BILLING CODE 4910-13-P
![Federal Register / Vol. 82, No. 100 / Thursday, May 25, 2017 / Rules and Regulations 24027
(i) Exception to Service Information identified in an RC step, must be done to DEPARTMENT OF TRANSPORTATION
Specifications comply with the AD. If a step or substep is
Although Boeing Alert Service Bulletin labeled ‘‘RC Exempt,’’ then the RC Federal Aviation Administration
737–53A1343, dated March 25, 2016, requirement is removed from that step or
specifies to contact Boeing for repair substep. An AMOC is required for any 14 CFR Part 39
instructions, and specifies that action as deviations to RC steps, including substeps
‘‘RC’’ (Required for Compliance), this AD [Docket No. FAA–2015–0084; Directorate
and identified figures.
requires repair before further flight using a Identifier 2014–NM–181–AD; Amendment
(ii) Steps not labeled as RC may be 39–18879; AD 2017–10–05]
method approved in accordance with the
deviated from using accepted methods in
procedures specified in paragraph (l) of this
accordance with the operator’s maintenance RIN 2120–AA64
AD.
or inspection program without obtaining
(j) AD Provisions for Part 26 Supplemental approval of an AMOC, provided the RC steps, Airworthiness Directives; Airbus
Inspections including substeps and identified figures, can Airplanes
Table 5 of paragraph 1.E., ‘‘Compliance,’’ still be done as specified, and the airplane
of Boeing Alert Service Bulletin 737– AGENCY: Federal Aviation
can be put back in an airworthy condition. Administration (FAA), Department of
53A1343, dated March 25, 2016, specifies
post-modification airworthiness limitation (m) Related Information Transportation (DOT).
inspections in compliance with 14 CFR For more information about this AD, ACTION: Final rule.
25.571(a)(3) at the modified locations, which
contact Jennifer Tsakoumakis, Aerospace
support compliance with 14 CFR SUMMARY: We are adopting a new
121.1109(c)(2) or 129.109(b)(2). As Engineer, Airframe Branch, ANM–120L,
FAA, Los Angeles ACO, 3960 Paramount
airworthiness directive (AD) for certain
airworthiness limitations, these inspections Airbus Model A300 series airplanes;
are required by maintenance and operational Boulevard, Lakewood, CA 90712–4137;
rules. It is therefore unnecessary to mandate phone: 562–627–5264; fax: 562–627–5210; and Model A300 B4–600, B4–600R, and
them in this AD. Deviations from these email: jennifer.tsakoumakis@faa.gov. F4–600R series airplanes, and Model
inspections require FAA approval, but do not A300 C4–605R Variant F airplanes
require an alternative method of compliance. (n) Material Incorporated by Reference (collectively called Model A300–600
(k) Terminating Action for Certain (1) The Director of the Federal Register series airplanes). This AD was prompted
Requirements of AD 2015–16–08 approved the incorporation by reference by reports indicating that on airplanes
(IBR) of the service information listed in this that received a certain repair following
Accomplishing the modification required
by paragraph (g) of this AD terminates the paragraph under 5 U.S.C. 552(a) and 1 CFR crack findings, cracks can re-initiate.
inspections required by paragraphs (g) and part 51. This AD requires repetitive inspections
(h) of AD 2015–16–08 for the modified area (2) You must use this service information of the center wing frame (FR) 40 lower
only. as applicable to do the actions required by outboard radius for cracking, and
(l) Alternative Methods of Compliance
this AD, unless the AD specifies otherwise. related investigative and corrective
(AMOCs) (i) Boeing Alert Service Bulletin 737– actions if necessary. We are issuing this
53A1343, dated March 25, 2016. AD to address the unsafe condition on
(1) The Manager, Los Angeles Aircraft
(ii) Reserved. these products.
Certification Office (ACO), FAA, has the
authority to approve AMOCs for this AD, if (3) For Boeing service information DATES: This AD is effective June 29,
requested using the procedures found in 14 identified in this AD, contact Boeing 2017.
CFR 39.19. In accordance with 14 CFR 39.19, Commercial Airplanes, Attention: The Director of the Federal Register
send your request to your principal inspector Contractual & Data Services (C&DS), 2600 approved the incorporation by reference
or local Flight Standards District Office, as Westminster Blvd., MC 110–SK57, Seal
appropriate. If sending information directly
of certain publications listed in this AD
Beach, CA 90740–5600; telephone: 562–797–
to the manager of the ACO, send it to the as of June 29, 2017.
1717; Internet: https://
attention of the person identified in www.myboeingfleet.com. ADDRESSES: For service information
paragraph (m) of this AD. Information may be identified in this final rule, contact
(4) You may view this service information
emailed to: 9-ANM-LAACO-AMOC- Airbus SAS, Airworthiness Office—
Requests@faa.gov. at the FAA, Transport Airplane Directorate,
1601 Lind Avenue SW., Renton, WA. For EAW, 1 Rond Point Maurice Bellonte,
(2) Before using any approved AMOC,
notify your appropriate principal inspector, information on the availability of this 31707 Blagnac Cedex, France; telephone
or lacking a principal inspector, the manager material at the FAA, call 425–227–1221. +33 5 61 93 36 96; fax +33 5 61 93 44
of the local flight standards district office/ (5) You may view this service information 51; email account.airworth-eas@
certificate holding district office. that is incorporated by reference at the airbus.com; Internet http://
(3) An AMOC that provides an acceptable National Archives and Records www.airbus.com. You may view this
level of safety may be used for any repair, Administration (NARA). For information on referenced service information at the
modification, or alteration required by this the availability of this material at NARA, call FAA, Transport Airplane Directorate,
AD if it is approved by the Boeing 1601 Lind Avenue SW., Renton, WA.
202–741–6030, or go to: http://
Commercial Airplanes Organization
Designation Authorization (ODA) that has www.archives.gov/federal-register/cfr/ibr- For information on the availability of
been authorized by the Manager, Los Angeles locations.html. this material at the FAA, call 425–227–
ACO, to make those findings. To be 1221. It is also available on the Internet
Issued in Renton, Washington, on May 10,
approved, the repair method, modification at http://www.regulations.gov by
2017.
deviation, or alteration deviation must meet searching for and locating Docket No.
the certification basis of the airplane, and the Michael Kaszycki, FAA–2015–0084.
approval must specifically refer to this AD. Acting Manager, Transport Airplane
(4) Except as required by paragraph (i) of Directorate, Aircraft Certification Service. Examining the AD Docket
this AD: For service information that [FR Doc. 2017–10265 Filed 5–24–17; 8:45 am] You may examine the AD docket on
contains steps that are labeled as Required
for Compliance (RC), the provisions of BILLING CODE 4910–13–P the Internet at http://
paragraphs (l)(4)(i) and (l)(4)(ii) of this AD www.regulations.gov by searching for
apply. and locating Docket No. FAA–2015–
(i) The steps labeled as RC, including 0084; or in person at the Docket
substeps under an RC step and any figures Management Facility between 9 a.m.
VerDate Sep<11>2014 15:57 May 24, 2017 Jkt 241001 PO 00000 Frm 00029 Fmt 4700 Sfmt 4700 E:\FR\FM\25MYR1.SGM 25MYR1](https://thefederalregister.org/doc/82_FR_24127/page/1.svg)
![24028 Federal Register / Vol. 82, No. 100 / Thursday, May 25, 2017 / Rules and Regulations
and 5 p.m., Monday through Friday, The European Aviation Safety Agency current, special detailed, and liquid
except Federal holidays. The AD docket (EASA), which is the Technical Agent penetrant inspections, as applicable, of
contains this AD, the regulatory for the Member States of the European the center wing FR 40 lower outboard
evaluation, any comments received, and Union, has issued EASA Airworthiness radius for cracking, and related
other information. The street address for Directive 2015–0232R1, dated December investigative and corrective actions if
the Docket Office (telephone 800–647– 16, 2015 (referred to after this as the necessary.
5527) is Docket Management Facility, Mandatory Continuing Airworthiness You may examine the MCAI in the
U.S. Department of Transportation, Information, or ‘‘the MCAI’’), to correct AD docket on the Internet at http://
Docket Operations, M–30, West an unsafe condition for certain Airbus www.regulations.gov by searching for
Building Ground Floor, Room W12–140, Model A300 series airplanes; and Model and locating Docket No. FAA–2015–
1200 New Jersey Avenue SE., A300 B4–600, B4–600R, and F4–600R 0084.
Washington, DC 20590. series airplanes, and Model A300 C4–
Comments
FOR FURTHER INFORMATION CONTACT: Dan 605R Variant F airplanes (collectively
Rodina, Aerospace Engineer, called Model A300–600 series We gave the public the opportunity to
International Branch, ANM–116, airplanes). The MCAI states: participate in developing this AD. We
Transport Airplane Directorate, FAA, Cracks were found on the lower outboard received no comments on the SNPRM or
1601 Lind Avenue SW., Renton, WA radius of the centre wing frame 40 forward on the determination of the cost to the
98057–3356; telephone 425–227–2125; fitting on in-service aeroplanes. public.
This condition, if not detected and
fax 425–227–1149. corrected, could lead to reduced structural Conclusion
SUPPLEMENTARY INFORMATION: integrity of the aeroplane. We reviewed the relevant data and
To address this unsafe condition, Airbus determined that air safety and the
Discussion issued several inspection Service Bulletins
(SB) and repair instructions. Consequently,
public interest require adopting this AD
We issued a supplemental notice of EASA issued AD 2009–0094, which was later as proposed except for minor editorial
proposed rulemaking (SNPRM) to superseded by EASA AD 2011–0163 [which changes. We have determined that these
amend 14 CFR part 39 by adding an AD corresponds to FAA AD 2012–25–06, minor changes:
that would apply to certain Airbus Amendment 39–17287 (77 FR 75833, • Are consistent with the intent that
Model A300 series airplanes; and Model December 26, 2012) (‘‘AD 2012–25–06’’)] and was proposed in the SNPRM for
A300 B4–600, B4–600R, and F4–600R [EASA] AD 2014–0199 [which corresponds correcting the unsafe condition; and
to the FAA NPRM], to require repetitive
series airplanes, and Model A300 C4– inspections and corrective actions on the • Do not add any additional burden
605R Variant F airplanes (collectively affected areas. upon the public than was already
called Model A300–600 series Since those [EASA] ADs were issued, proposed in the SNPRM.
airplanes). The SNPRM published in the additional in-service findings induced Airbus
to do a new fatigue analysis, using a detailed
Related Service Information Under 1
Federal Register on November 10, 2016
Finite Element Model study, which resulted CFR Part 51
(81 FR 78944) (‘‘the SNPRM’’). We
preceded the SNPRM with a notice of in defining new inspection methods. We reviewed the following service
Prompted by these results, Airbus issued SB information:
proposed rulemaking (NPRM) that A300–57–0261, SB A300–57–6117 and SB
published in the Federal Register on A300–57–9034 to introduce these • Airbus Service Bulletin A300–57–
February 13, 2015 (80 FR 7992) (‘‘the inspections. These new inspection SBs 6117, dated May 28, 2015.
NPRM’’). The NPRM proposed to supersede and render obsolete inspection SB • Airbus Service Bulletin A300–57–
require repetitive inspections for A300–53–0268 and SB A300–57–6052 and 0261, dated June 11, 2015.
cracking of the FR 40 forward fittings for the All Operators Transmissions (AOT) The service information describes
airplanes previously repaired. The A300–53A0391, AOT A300–57A6111, AOT procedures for repetitive ultrasonic,
NPRM was prompted by reports A300–53W002–14 and AOT A300–57W003–
14.
rototest, high frequency eddy current,
indicating that, on airplanes that For the reasons described above, EASA special detailed, and liquid penetrant
received a certain repair following crack issued AD 2015–0232, superseding [Direction inspections, and related investigative
findings, cracks can re-initiate. The Générale de l’Aviation Civile] DGAC France and corrective actions. These
SNPRM proposed to require repetitive AD 1998–038–010(B) R1 [which corresponds documents are distinct since they apply
rototest, ultrasonic, high frequency eddy to FAA AD 98–25–07, Amendment 39–10933 to different airplane models. This
current, special detailed, and liquid (63 FR 68167, December 10, 1998) (‘‘AD 98– service information is reasonably
penetrant inspections, as applicable, of 25–07’’)] and [DGAC France] AD 2003– available because the interested parties
189(B), and EASA AD 2011–0163 and
the center wing FR 40 lower outboard [EASA] AD 2014–0199, to require the new have access to it through their normal
radius for cracking, and related inspections of the affected areas within new course of business or by the means
investigative and corrective actions if thresholds and intervals. identified in the ADDRESSES section.
necessary. The SNPRM also proposed to This [EASA] AD is revised to clarify the
compliance time(s), introducing a Note after Costs of Compliance
add airplanes to the applicability. We
are issuing this AD to detect and correct paragraph (1), and to alleviate the reporting We estimate that this AD affects 29
cracking on the FR 40 forward fittings, requirements of paragraph (3). airplanes of U.S. registry.
which could result in reduced structural Required actions include repetitive We estimate the following costs to
integrity of the airplane. rototest, ultrasonic, high frequency eddy comply with this AD.
ESTIMATED COSTS
Action Labor cost Cost per product Cost on U.S. operators
Inspections ............. Up to 91 work-hours × $85 per hour = Up to $7,735 per inspection cycle ........ Up to $224,315 per inspection cycle.
$7,735 per inspection cycle.
Reporting ............... 1 work-hour × $85 per hour = $85 ....... $85 ........................................................ $2,465.
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![Federal Register / Vol. 82, No. 100 / Thursday, May 25, 2017 / Rules and Regulations 24029
We have received no definitive data 1. Is not a ‘‘significant regulatory (e) Reason
that would enable us to provide cost action’’ under Executive Order 12866; This AD was prompted by reports of cracks
estimates for the on-condition actions 2. Is not a ‘‘significant rule’’ under the on the lower outboard radius of the center
specified in this AD. DOT Regulatory Policies and Procedures wing frame (FR) 40 forward fitting. We are
(44 FR 11034, February 26, 1979); issuing this AD to detect and correct cracking
Paperwork Reduction Act on the FR 40 forward fittings, which could
3. Will not affect intrastate aviation in result in reduced structural integrity of the
A federal agency may not conduct or
sponsor, and a person is not required to Alaska; and airplane.
respond to, nor shall a person be subject 4. Will not have a significant (f) Compliance
to penalty for failure to comply with a economic impact, positive or negative,
on a substantial number of small entities Comply with this AD within the
collection of information subject to the compliance times specified, unless already
requirements of the Paperwork under the criteria of the Regulatory done.
Reduction Act unless that collection of Flexibility Act.
(g) Repetitive Inspections
information displays a current valid List of Subjects in 14 CFR Part 39
OMB control number. The control Except as provided by paragraph (i)(1) of
number for the collection of information Air transportation, Aircraft, Aviation this AD, at the applicable times specified in
safety, Incorporation by reference, paragraph 1.E.(2), ‘‘Compliance,’’ of Airbus
required by this AD is 2120–0056. The Service Bulletin A300–57–0261, dated June
paperwork cost associated with this AD Safety.
11, 2015; or Airbus Service Bulletin A300–
has been detailed in the Costs of Adoption of the Amendment 57–6117, dated May 28, 2015; accomplish
Compliance section of this document rototest, ultrasonic, high frequency eddy
and includes time for reviewing Accordingly, under the authority current, special detailed, and liquid
instructions, as well as completing and delegated to me by the Administrator, penetrant inspections, as applicable, of the
reviewing the collection of information. the FAA amends 14 CFR part 39 as center wing FR 40 lower outboard radius for
Therefore, all reporting associated with follows: cracking, and do all applicable related
this AD is mandatory. Comments investigative actions, in accordance with the
PART 39—AIRWORTHINESS Accomplishment Instructions of Airbus
concerning the accuracy of this burden Service Bulletin A300–57–0261, dated June
and suggestions for reducing the burden DIRECTIVES
11, 2015; or Airbus Service Bulletin A300–
should be directed to the FAA at 800 57–6117, dated May 28, 2015; as applicable.
Independence Ave. SW., Washington, ■ 1. The authority citation for part 39
Do all applicable related investigative actions
DC 20591, ATTN: Information continues to read as follows:
before further flight. Repeat the inspections
Collection Clearance Officer, AES–200. Authority: 49 U.S.C. 106(g), 40113, 44701. thereafter at the applicable times specified in
paragraph 1.E. (2), ‘‘Compliance,’’ of Airbus
Authority for This Rulemaking § 39.13 [Amended] Service Bulletin A300–57–0261, dated June
Title 49 of the United States Code ■ 2. The FAA amends § 39.13 by adding 11, 2015; or Airbus Service Bulletin A300–
specifies the FAA’s authority to issue 57–6117, dated May 28, 2015.
the following new airworthiness
rules on aviation safety. Subtitle I, directive (AD): (h) Corrective Actions
section 106, describes the authority of If, during any inspection required by
2017–10–05 Airbus: Amendment 39–18879;
the FAA Administrator. ‘‘Subtitle VII: Docket No. FAA–2015–0084; Directorate paragraph (g) of this AD, any crack is found,
Aviation Programs,’’ describes in more Identifier 2014–NM–181–AD. before further flight, accomplish the
detail the scope of the Agency’s applicable corrective actions, in accordance
authority. (a) Effective Date with the Accomplishment Instructions of
We are issuing this rulemaking under This AD is effective June 29, 2017. Airbus Service Bulletin A300–57–0261,
the authority described in ‘‘Subtitle VII, dated June 11, 2015; or Airbus Service
(b) Affected ADs Bulletin A300–57–6117, dated May 28, 2015;
Part A, Subpart III, Section 44701:
General requirements.’’ Under that This AD affects AD 98–25–07, Amendment as applicable; except as required by
39–10933 (63 FR 68167, December 10, 1998) paragraph (i)(2) of this AD.
section, Congress charges the FAA with (‘‘AD 98–25–07’’); and AD 2012–25–06,
promoting safe flight of civil aircraft in (i) Service Information Exception
Amendment 39–17287 (77 FR 75833,
air commerce by prescribing regulations December 26, 2012) (‘‘AD 2012–25–06’’). (1) Where the service information specified
for practices, methods, and procedures in paragraph (g) of this AD specifies a
the Administrator finds necessary for (c) Applicability compliance time ‘‘from this service bulletin
safety in air commerce. This regulation This AD applies to the Airbus airplanes, issuance date,’’ this AD requires compliance
is within the scope of that authority certificated in any category, identified in within the specified compliance time after
because it addresses an unsafe condition paragraphs (c)(1) through (c)(5) of this AD, the effective date of this AD.
except airplanes on which Airbus (2) Where the service information specified
that is likely to exist or develop on Modification 10221 has been embodied in in paragraph (h) of this AD specifies to
products identified in this rulemaking production. contact Airbus for certain conditions, before
action. (1) Model A300 B2–1A, B2–1C, B2K–3C, further flight, repair using a method
Regulatory Findings B2–203, B4–2C, B4–103, and B4–203 approved by the Manager, International
airplanes. Branch, ANM–116, Transport Airplane
We determined that this AD will not (2) Model A300 B4–601, B4–603, B4–620, Directorate, FAA; or the European Aviation
have federalism implications under and B4–622 airplanes. Safety Agency (EASA); or Airbus’s EASA
Executive Order 13132. This AD will (3) Model A300 B4–605R and B4–622R Design Organization Approval (DOA).
not have a substantial direct effect on airplanes.
(j) No Terminating Action for This AD
the States, on the relationship between (4) Model A300 F4–605R and F4–622R
airplanes. Accomplishing a corrective action required
the national government and the States, by paragraph (h) of this AD, or accomplishing
(5) Model A300 C4–605R Variant F
or on the distribution of power and airplanes. a preventative action specified in Airbus
responsibilities among the various Service Bulletin A300–57–0260 or A300–57–
levels of government. (d) Subject 6116, as applicable, does not terminate the
For the reasons discussed above, I Air Transport Association (ATA) of repetitive inspections required by paragraph
certify that this AD: America Code 57, Wings. (g) of this AD.
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![24030 Federal Register / Vol. 82, No. 100 / Thursday, May 25, 2017 / Rules and Regulations
(k) Terminating Action for Certain Ave. SW., Washington, DC 20591, Attn: DEPARTMENT OF TRANSPORTATION
Requirements of Other ADs Information Collection Clearance Officer,
(1) Accomplishing the actions required by AES–200. Federal Aviation Administration
paragraph (g) of this AD terminates the
(n) Related Information
actions required by paragraphs (a) and (b) of 14 CFR Part 39
AD 98–25–07. (1) Refer to Mandatory Continuing
(2) Accomplishing the actions required by Airworthiness Information (MCAI) EASA [Docket No. FAA–2016–9550; Directorate
paragraph (g) of this AD terminates the Airworthiness Directive 2015–0232R1, dated Identifier 2016–CE–026–AD; Amendment
actions required by paragraphs (i) and (j) of 39–18894; AD 2017–10–20]
December 16, 2015, for related information.
AD 2012–25–06. This MCAI may be found in the AD docket RIN 2120–AA64
(l) Reporting Requirements on the Internet at http://www.regulations.gov
Within 60 days after any inspection by searching for and locating Docket No. Airworthiness Directives; Piper
required by paragraph (g) of this AD, or FAA–2015–0084. Aircraft, Inc. Airplanes
within 60 days after the effective date of this (2) Service information identified in this
AGENCY: Federal Aviation
AD, whichever occurs later, report any AD that is not incorporated by reference is
findings, positive or negative, to Airbus available at the addresses specified in
Administration (FAA), DOT.
Service Bulletin Reporting Online paragraphs (o)(3) and (o)(4) of this AD. ACTION: Final rule.
Application on Airbus World (https://
w3.airbus.com/). (o) Material Incorporated by Reference SUMMARY: We are adopting a new
(1) The Director of the Federal Register airworthiness directive (AD) for certain
(m) Other FAA AD Provisions
approved the incorporation by reference Piper Aircraft, Inc. Models PA–31, PA–
The following provisions also apply to this 31–300, PA–31–325, and PA–31–350
AD: (IBR) of the service information listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR airplanes. This AD was prompted by
(1) Alternative Methods of Compliance
(AMOCs): The Manager, International part 51. fatigue cracking in the fuselage station
Branch, ANM–116, Transport Airplane (2) You must use this service information (FS) 332.00 bulkhead common to the
Directorate, FAA, has the authority to as applicable to do the actions required by horizontal stabilizer front spar
approve AMOCs for this AD, if requested this AD, unless this AD specifies otherwise. attachment. This AD requires repetitive
using the procedures found in 14 CFR 39.19. (i) Airbus Service Bulletin A300–57–0261, inspections to detect cracks in the
In accordance with 14 CFR 39.19, send your dated June 11, 2015. bulkhead and any necessary repairs.
request to your principal inspector or local (ii) Airbus Service Bulletin A300–57–6117, This AD also provides an optional
Flight Standards District Office, as
dated May 28, 2015. modification if no cracks are found that
appropriate. If sending information directly
to the International Branch, send it to ATTN: (3) For service information identified in will greatly reduce the likelihood of the
Dan Rodina, Aerospace Engineer, this AD, contact Airbus SAS, Airworthiness specified cracks. We are issuing this AD
International Branch, ANM–116, Transport Office—EAW, 1 Rond Point Maurice to correct the unsafe condition on these
Airplane Directorate, FAA, 1601 Lind Bellonte, 31707 Blagnac Cedex, France; products.
Avenue SW., Renton, WA 98057–3356; telephone +33 5 61 93 36 96; fax +33 5 61 DATES: This AD is effective June 29,
telephone 425–227–2125; fax 425–227–1149. 93 44 51; email account.airworth-eas@ 2017.
Information may be emailed to: 9-ANM-116- airbus.com; Internet http://www.airbus.com. The Director of the Federal Register
AMOC-REQUESTS@faa.gov. Before using (4) You may view this service information
any approved AMOC, notify your appropriate approved the incorporation by reference
at the FAA, Transport Airplane Directorate, of a certain publication listed in this AD
principal inspector, or lacking a principal 1601 Lind Avenue SW., Renton, WA. For
inspector, the manager of the local flight as of June 29, 2017.
information on the availability of this
standards district office/certificate holding ADDRESSES: For service information
district office. material at the FAA, call 425–227–1221.
(5) You may view this service information identified in this final rule, contact
(2) Contacting the Manufacturer: For any Piper Aircraft, Inc., Customer Service,
requirement in this AD to obtain corrective that is incorporated by reference at the
National Archives and Records 2926 Piper Drive, Vero Beach, Florida
actions from a manufacturer, the action must
be accomplished using a method approved Administration (NARA). For information on 32960; telephone: (877) 879–0275; fax:
by the Manager, International Branch, ANM– the availability of this material at NARA, call none; email: customer.service@
116, Transport Airplane Directorate, FAA; or 202–741–6030, or go to: http:// piper.com; Internet: www.piper.com.
EASA; or Airbus’s EASA DOA. If approved www.archives.gov/federal-register/cfr/ibr- You may view this referenced service
by the DOA, the approval must include the locations.html. information at the FAA, Small Airplane
DOA-authorized signature. Directorate, 901 Locust, Kansas City,
(3) Reporting Requirements: A federal Issued in Renton, Washington, on May 2, Missouri 64106. For information on the
agency may not conduct or sponsor, and a 2017.
availability of this material at the FAA,
person is not required to respond to, nor Michael Kaszycki, call (816) 329–4148. It is also available
shall a person be subject to a penalty for
failure to comply with a collection of
Acting Manager, Transport Airplane on the internet at http://
information subject to the requirements of Directorate, Aircraft Certification Service. www.regulations.gov by searching for
the Paperwork Reduction Act unless that [FR Doc. 2017–10285 Filed 5–24–17; 8:45 am] and locating Docket No. FAA–2016–
collection of information displays a current BILLING CODE 4910–13–P 9550.
valid OMB Control Number. The OMB
Control Number for this information Examining the AD Docket
collection is 2120–0056. Public reporting for You may examine the AD docket on
this collection of information is estimated to the Internet at http://
be approximately 5 minutes per response, www.regulations.gov by searching for
including the time for reviewing instructions,
and locating Docket No. FAA–2016–
completing and reviewing the collection of
information. All responses to this collection 9550; or in person at the Docket
of information are mandatory. Comments Management Facility between 9 a.m.
concerning the accuracy of this burden and and 5 p.m., Monday through Friday,
suggestions for reducing the burden should except Federal holidays. The AD docket
be directed to the FAA at: 800 Independence contains this AD, the regulatory
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Document Created: 2018-11-08 08:53:19
Document Modified: 2018-11-08 08:53:19
| Category | Regulatory Information | |
| Collection | Federal Register | |
| sudoc Class | AE 2.7: GS 4.107: AE 2.106: | |
| Publisher | Office of the Federal Register, National Archives and Records Administration | |
| Section | Rules and Regulations | |
| Action | Final rule. | |
| Dates | This AD is effective June 29, 2017. | |
| Contact | Dan Rodina, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356; telephone 425-227-2125; fax 425-227-1149. | |
| FR Citation | 82 FR 24027 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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