82 FR 5362 - Airworthiness Directives; Airbus Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 82, Issue 11 (January 18, 2017)
Federal Aviation Administration
Federal Register Volume 82, Issue 11 (January 18, 2017)
| Page Range | 5362-5365 | |
| FR Document | 2017-00408 |
[Federal Register Volume 82, Number 11 (Wednesday, January 18, 2017)] [Rules and Regulations] [Pages 5362-5365] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2017-00408] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2015-0831; Directorate Identifier 2014-NM-061-AD; Amendment 39-18778; AD 2017-01-11] 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 all Airbus Model A318 and A319 series airplanes, Model A320-211, -212, - 214, -231, -232, and -233 airplanes, and Model A321 series airplanes. This AD was prompted by a report of a rupture of a main landing gear (MLG) sliding tube axle. This AD requires identification of the part number and serial number of the MLG sliding tubes; inspection of affected chromium plates and sliding tube axles for damage; and replacement of the sliding tube if necessary. We are issuing this AD to address the unsafe condition on these products. DATES: This AD is effective February 22, 2017. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of February 22, 2017. ADDRESSES: For service information identified in this final rule, contact Airbus, Airworthiness Office--EIAS, 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- 0831. 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- 0831; or in person at the Docket Management Facility between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this AD, the regulatory evaluation, any comments received, and other information. The street address for the Docket Office (telephone 800-647-5527) is Docket Management Facility, U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590. FOR FURTHER INFORMATION CONTACT: Sanjay Ralhan, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356; telephone 425-227-1405; 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 all Airbus Model A318 and A319 series airplanes, Model A320-211, -212, -214, -231, -232, and -233 airplanes, and Model A321 series airplanes. The SNPRM published in the Federal Register on June 28, 2016 (81 FR 41886) (``the SNPRM''). We preceded the SNPRM with a notice of proposed rulemaking (NPRM) that published in the Federal Register on April 24, 2015 (80 FR 22939) (``the NPRM''). The NPRM proposed to require an inspection to identify the part number and serial number of the MLG sliding tubes installed on the airplane; an inspection of the axle on certain MLG sliding tubes for damage; and replacement of the sliding tube if necessary. The NPRM was prompted by a report of a rupture of a MLG sliding tube axle. The SNPRM proposed to remove certain service information that does not adequately address the identified unsafe condition and revise the compliance method. We are issuing this AD to detect and correct cracks in the axle and (partial) detachment of the axle and wheel from the sliding tube, which could result in failure of an MLG. The European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Union, has issued EASA Airworthiness Directive 2014-0058, dated March 11, 2014 (referred to after this as the Mandatory Continuing Airworthiness Information, or ``the MCAI''), to correct an unsafe condition for all Airbus Model A318 and A319 series airplanes, Model A320-211, -212, -214, -231, -232, and -233 airplanes, and Model A321 series airplanes. The MCAI states: A main landing gear (MLG) sliding tube axle rupture occurred in service. Investigation of the affected part showed that this failure was due to an abnormal grinding operation during overhaul by a certain maintenance and repair organization located in Singapore. A population of MLG sliding tubes was subsequently identified whose axles may have been subject to this grinding operation, which may have resulted in areas of residual stress on the axles on the MLG sliding tubes. In addition, the MSN [manufacturer serial number] of the aeroplanes which are known to have had the affected parts installed have been identified. This condition, if not detected and corrected, could lead to cracks in the axle and (partial) detachment of axle and wheel from the sliding tube, possibly resulting in failure of a MLG with consequent damage to the aeroplane and injury to occupants. To address this potential unsafe condition, Messier-Bugatti- Dowty, the MLG gear manufacturer, issued Service Bulletin (SB) 200- 32-313 and SB 201-32-62 [both dated February 25, 2013], providing inspection instructions and criteria for removal from service of the affected MLG sliding tubes. For the reasons described above, this [EASA] AD requires a one- time Special Detailed Inspection (SDI) of the axle on the affected MLG sliding tubes and, depending on findings, replacement of the MLG sliding tube. The SDI includes a detailed visual inspection of the chromium plate for damage, and a Barkhausen noise inspection of the sliding tube axles for damage. 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- 0831. 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 [[Page 5363]] Do not add any additional burden upon the public than was already proposed in the SNPRM. Related Service Information Under 1 CFR Part 51 Airbus has issued Service Bulletin A320-32-1416, including Appendix 01, dated March 10, 2014. This service information describes procedures for inspecting MLG axles and brake flanges by doing a detailed visual inspection of the chromium plates for damage, a Barkhausen noise inspection of the sliding tube axles for damage, and replacement of affected parts if necessary. 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 3 airplanes of U.S. registry. We also estimate that it would take about 18 work-hours per product to comply with the basic requirements of this AD. The average labor rate is $85 per work-hour. Based on these figures, we estimate the cost of this AD on U.S. operators to be $4,590, or $1,530 per product. In addition, we estimate that any necessary on-condition actions will take about 3 work-hours, for a cost of $255 per product. We have received no definitive data that would enable us to provide part cost estimates for the on-condition actions specified in this AD. We have no way of determining the number of aircraft that might need these actions. 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): 2017-01-11 Airbus: Amendment 39-18778; Docket No. FAA-2015-0831; Directorate Identifier 2014-NM-061-AD. (a) Effective Date This AD is effective February 22, 2017. (b) Affected ADs None. (c) Applicability This AD applies to the Airbus airplanes identified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, all manufacturer serial numbers. (1) Airbus Model A318-111, -112, -121, and -122 airplanes. (2) Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes. (3) Airbus Model A320-211, -212, -214, -231, -232, and -233 airplanes. (4) Airbus Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes. (d) Subject Air Transport Association (ATA) of America Code 32, Landing gear. (e) Reason This AD was prompted by a report of a rupture of a main landing gear (MLG) sliding tube axle. We are issuing this AD to detect and correct cracks in the axle and (partial) detachment of the axle and wheel from the sliding tube, which could result in failure of an MLG. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) MLG Sliding Tube Part Number and Serial Number Identification Within 3 months after the effective date of this AD: Do an inspection to identify the part number and serial number of the MLG sliding tubes installed on the airplane. A review of airplane maintenance records is acceptable in lieu of this inspection if the part number and serial number of the MLG sliding tubes can be conclusively determined from that review. (h) Identification of Airplanes Not Affected by the Requirements of Paragraph (i) of this AD An airplane with a manufacturer serial number (MSN) not listed in figure 1 to paragraph (h) of this AD is not affected by the requirements of paragraph (i) of this AD, provided it can be determined that no MLG sliding tube having a part number and serial number listed in table 1 to paragraphs (h), (i), (k)(1), (k)(2), (l)(1), and (l)(2) of this AD has been installed on that airplane since first flight of the airplane. Figure 1 to Paragraph (h) of This AD ---------------------------------------------------------------------------------------------------------------- ---------------------------------------------------------------------------------------------------------------- Affected Airplanes Listed by MSN ---------------------------------------------------------------------------------------------------------------- 0179 0214 0296 0412 0558 0604 0607 0668 0704 0720 0726 0731 0754 0771 0799 0828 0841 0855 0909 0914 0925 0939 0986 1028 1030 1041 1070 1083 1093 1098 [[Page 5364]] 1108 1148 1294 1356 2713 2831 ---------------------------------------------------------------------------------------------------------------- Table 1 to Paragraphs (h), (i), (k)(1), (k)(2), (l)(1), and (l)(2) of this AD--Affected MLG Sliding Tubes ------------------------------------------------------------------------ Part No. Serial No. ------------------------------------------------------------------------ 201160302............................................... 78B 201160302............................................... 1016B11 201160302............................................... 1144B 201371302............................................... B4493 201371302............................................... B4513 201371302............................................... SS4359 201371302............................................... B4530 201371302............................................... B4517 201371302............................................... B4568 201371302............................................... B4498 201371302............................................... 4490B 201371302............................................... B202-4598 201371302............................................... B165-4623 201371302............................................... B244-4766 201371302............................................... B267-4794 201371302............................................... B272-4813 201160302............................................... 1108B 201371304............................................... B041-4871 201371304............................................... B045-4869 201371304............................................... B001-4781 201371304............................................... B051-4892 201371304............................................... B110-1952 201371304............................................... B054-4891 201371304............................................... B063-4921 201371304............................................... B071-4911 201371304............................................... B071-4917 201371304............................................... B080-1933 201371304............................................... B117-5010 201371304............................................... B120-4989 201371304............................................... B132-2023 201371304............................................... B114-1956 201371304............................................... B208-2009 201371304............................................... B133-1947 201371304............................................... B154-5037 201371304............................................... B89 4952 201371304............................................... B129-1964 201371304............................................... B227-2010 201371304............................................... B170-5031 201371304............................................... B182-5047 201371304............................................... B239-2053 201371304............................................... B1401-2856 201371304............................................... B1813-3142 201371304............................................... B116-5004 201522353............................................... B011-149 201522350............................................... B014-25 201522350............................................... B019-56 201522350............................................... B019-57 201522350............................................... B021-69 201522350............................................... B022-60 201522353............................................... B03-111 201522353............................................... B03-110 201522353............................................... B112-317 201522353............................................... B174-351 201522353............................................... B179-392 201383350............................................... 4377B 201383350............................................... 4393B 201383350............................................... B1831 201383350............................................... B1832 201383350............................................... SS4355B 201383350............................................... SS4400B ------------------------------------------------------------------------ (i) Inspections For each MLG sliding tube identified as required by paragraph (g) of this AD, having a part number and serial number listed in table 1 to paragraphs (h), (i), (k)(1), (k)(2), (l)(1), and (l)(2) of this AD: Within 3 months after the effective date of this AD, inspect affected MLG axles and brake flanges by doing a detailed visual inspection of the chromium plates for damage, and a Barkhausen noise inspection of the sliding tube axles for damage, in accordance with the Accomplishment Instructions of Airbus Service Bulletin A320-32-1416, including Appendix 01, dated March 10, 2014. For Model A318 series airplanes, use the procedures specified for Model A319 series airplanes in Airbus Service Bulletin A320-32-1416, including Appendix 01, dated March 10, 2014. (j) Corrective Action If, during any inspection required by paragraph (i) of this AD, any damage is detected: Before further flight, replace the MLG sliding tube with a serviceable tube, in accordance with the Accomplishment Instructions of Airbus Service Bulletin A320-32-1416, including Appendix 01, dated March 10, 2014. For Model A318 series airplanes, use the procedures specified for Model A319 series airplanes in Airbus Service Bulletin A320-32-1416, including Appendix 01, dated March 10, 2014. (k) Definition of Serviceable Sliding Tube For the purpose of this AD, a serviceable sliding tube is defined as a sliding tube that meets the criterion in either paragraph (k)(1) or (k)(2) of this AD. (1) A sliding tube having a part number and serial number not listed in table 1 to paragraphs (h), (i), (k)(1), (k)(2), (l)(1), and (l)(2) of this AD. (2) A sliding tube having a part number and serial number listed in table 1 to paragraphs (h), (i), (k)(1), (k)(2), (l)(1), and (l)(2) of this AD that has passed the inspections required by paragraph (i) of this AD. (l) Parts Installation Prohibitions (1) For airplanes that have an MLG sliding tube installed that has a part number and serial number listed in table 1 to paragraphs (h), (i), (k)(1), (k)(2), (l)(1), and (l)(2) of this AD: After an airplane is returned to service following accomplishment of the actions required by paragraphs (g), (h), and (i) of this AD, no person may install on any airplane an MLG sliding tube having a part number and serial number listed in table 1 to paragraphs (h), (i), (k)(1), (k)(2), (l)(1), and (l)(2) of this AD unless that sliding tube has passed the inspection required by paragraph (i) of this AD. (2) For airplanes that, as of the effective date of this AD, do not have an MLG sliding tube installed that has a part number and serial number listed in table 1 to paragraphs (h), (i), (k)(1), (k)(2), (l)(1), and (l)(2) of this AD: No person may install on any airplane an MLG sliding tube having a part number and serial number listed in table 1 to paragraphs (h), (i), (k)(1), (k)(2), (l)(1), and (l)(2) of this AD unless that sliding tube has passed the inspection required by paragraph (i) of this AD. (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: Sanjay Ralhan, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057- 3356; telephone 425-227-1405; fax 425-227-1149. Information may be emailed to: [email protected]. Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/certificate holding district office. The AMOC approval letter must specifically reference this AD. (2) Required for Compliance (RC): If any service information contains procedures or tests that are identified as RC, those procedures and tests must be done to comply with this AD; any procedures or tests that are not identified as RC are recommended. Those procedures and tests that are not identified as RC may be deviated from using accepted methods in accordance with the operator's maintenance or inspection program without obtaining approval of an AMOC, provided the procedures and tests identified as RC can be done and the airplane can be put back in an airworthy condition. Any substitutions or changes to procedures or tests identified as RC require approval of an AMOC. (3) Contacting the Manufacturer: For any requirement in this AD to obtain corrective actions from a manufacturer, the action must be accomplished using a method approved by the Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA; or the European Aviation Safety Agency (EASA); or Airbus's EASA Design Organization Approval (DOA). If approved by the DOA, the approval must include the DOA-authorized signature. (n) Special Flight Permits Special flight permits may be issued in accordance with sections 21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199) to operate the airplane to a location where the airplane can be modified (if the operator elects to do so), provided the MLG remains extended throughout the flight. (o) Related Information Refer to Mandatory Continuing Airworthiness Information (MCAI) EASA [[Page 5365]] Airworthiness Directive 2014-0058, dated March 11, 2014, 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-2015-0831. (p) 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 A320-32-1416, including Appendix 01, dated March 10, 2014. (ii) Reserved. (3) For service information identified in this AD, contact Airbus, Airworthiness Office--EIAS, 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 January 4, 2017. Michael Kaszycki, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2017-00408 Filed 1-17-17; 8:45 am] BILLING CODE 4910-13-P
![5362 Federal Register / Vol. 82, No. 11 / Wednesday, January 18, 2017 / Rules and Regulations
www.archives.gov/federal-register/cfr/ibr- and locating Docket No. FAA–2015– Directive 2014–0058, dated March 11,
locations.html. 0831. 2014 (referred to after this as the
Issued in Kansas City, Missouri, on January Mandatory Continuing Airworthiness
Examining the AD Docket
6, 2017. Information, or ‘‘the MCAI’’), to correct
Melvin Johnson, You may examine the AD docket on an unsafe condition for all Airbus
Manager, Small Airplane Directorate, Aircraft the Internet at http:// Model A318 and A319 series airplanes,
Certification Service. www.regulations.gov by searching for Model A320–211, –212, –214, –231,
[FR Doc. 2017–00502 Filed 1–17–17; 8:45 am] and locating Docket No. FAA–2015– –232, and –233 airplanes, and Model
BILLING CODE 4910–13–P
0831; or in person at the Docket A321 series airplanes. The MCAI states:
Management Facility between 9 a.m. A main landing gear (MLG) sliding tube
and 5 p.m., Monday through Friday, axle rupture occurred in service.
DEPARTMENT OF TRANSPORTATION except Federal holidays. The AD docket Investigation of the affected part showed that
contains this AD, the regulatory this failure was due to an abnormal grinding
Federal Aviation Administration evaluation, any comments received, and operation during overhaul by a certain
other information. The street address for maintenance and repair organization located
14 CFR Part 39 the Docket Office (telephone 800–647– in Singapore. A population of MLG sliding
5527) is Docket Management Facility, tubes was subsequently identified whose
[Docket No. FAA–2015–0831; Directorate axles may have been subject to this grinding
Identifier 2014–NM–061–AD; Amendment U.S. Department of Transportation,
operation, which may have resulted in areas
39–18778; AD 2017–01–11] Docket Operations, M–30, West of residual stress on the axles on the MLG
Building Ground Floor, Room W12–140, sliding tubes. In addition, the MSN
RIN 2120–AA64 1200 New Jersey Avenue SE., [manufacturer serial number] of the
Washington, DC 20590. aeroplanes which are known to have had the
Airworthiness Directives; Airbus
FOR FURTHER INFORMATION CONTACT: affected parts installed have been identified.
Airplanes This condition, if not detected and
Sanjay Ralhan, Aerospace Engineer,
AGENCY: Federal Aviation International Branch, ANM–116, corrected, could lead to cracks in the axle
Administration (FAA), Department of and (partial) detachment of axle and wheel
Transport Airplane Directorate, FAA, from the sliding tube, possibly resulting in
Transportation (DOT). 1601 Lind Avenue SW., Renton, WA failure of a MLG with consequent damage to
ACTION: Final rule. 98057–3356; telephone 425–227–1405; the aeroplane and injury to occupants.
fax 425–227–1149. To address this potential unsafe condition,
SUMMARY: We are adopting a new Messier-Bugatti-Dowty, the MLG gear
SUPPLEMENTARY INFORMATION:
airworthiness directive (AD) for all manufacturer, issued Service Bulletin (SB)
Airbus Model A318 and A319 series Discussion 200–32–313 and SB 201–32–62 [both dated
airplanes, Model A320–211, –212, –214, We issued a supplemental notice of February 25, 2013], providing inspection
–231, –232, and –233 airplanes, and proposed rulemaking (SNPRM) to
instructions and criteria for removal from
Model A321 series airplanes. This AD service of the affected MLG sliding tubes.
amend 14 CFR part 39 by adding an AD For the reasons described above, this
was prompted by a report of a rupture that would apply to all Airbus Model
of a main landing gear (MLG) sliding [EASA] AD requires a one-time Special
A318 and A319 series airplanes, Model Detailed Inspection (SDI) of the axle on the
tube axle. This AD requires A320–211, –212, –214, –231, –232, and affected MLG sliding tubes and, depending
identification of the part number and –233 airplanes, and Model A321 series on findings, replacement of the MLG sliding
serial number of the MLG sliding tubes; airplanes. The SNPRM published in the tube.
inspection of affected chromium plates Federal Register on June 28, 2016 (81
and sliding tube axles for damage; and The SDI includes a detailed visual
FR 41886) (‘‘the SNPRM’’). We preceded inspection of the chromium plate for
replacement of the sliding tube if the SNPRM with a notice of proposed
necessary. We are issuing this AD to damage, and a Barkhausen noise
rulemaking (NPRM) that published in inspection of the sliding tube axles for
address the unsafe condition on these the Federal Register on April 24, 2015
products. damage.
(80 FR 22939) (‘‘the NPRM’’). The You may examine the MCAI in the
DATES: This AD is effective February 22, NPRM proposed to require an AD docket on the Internet at http://
2017. inspection to identify the part number www.regulations.gov by searching for
The Director of the Federal Register and serial number of the MLG sliding and locating Docket No. FAA–2015–
approved the incorporation by reference tubes installed on the airplane; an 0831.
of a certain publication listed in this AD inspection of the axle on certain MLG
as of February 22, 2017. sliding tubes for damage; and Comments
ADDRESSES: For service information replacement of the sliding tube if We gave the public the opportunity to
identified in this final rule, contact necessary. The NPRM was prompted by participate in developing this AD. We
Airbus, Airworthiness Office—EIAS, 1 a report of a rupture of a MLG sliding received no comments on the SNPRM or
Rond Point Maurice Bellonte, 31707 tube axle. The SNPRM proposed to on the determination of the cost to the
Blagnac Cedex, France; telephone +33 5 remove certain service information that public.
61 93 36 96; fax +33 5 61 93 44 51; email does not adequately address the
account.airworth-eas@airbus.com; identified unsafe condition and revise Conclusion
Internet http://www.airbus.com. You the compliance method. We are issuing We reviewed the relevant data and
may view this referenced service this AD to detect and correct cracks in determined that air safety and the
mstockstill on DSK3G9T082PROD with RULES
information at the FAA, Transport the axle and (partial) detachment of the public interest require adopting this AD
Airplane Directorate, 1601 Lind Avenue axle and wheel from the sliding tube, as proposed except for minor editorial
SW., Renton, WA. For information on which could result in failure of an MLG. changes. We have determined that these
the availability of this material at the The European Aviation Safety Agency minor changes:
FAA, call 425–227–1221. It is also (EASA), which is the Technical Agent • Are consistent with the intent that
available on the Internet at http:// for the Member States of the European was proposed in the SNPRM for
www.regulations.gov by searching for Union, has issued EASA Airworthiness correcting the unsafe condition; and
VerDate Sep<11>2014 16:39 Jan 17, 2017 Jkt 241001 PO 00000 Frm 00028 Fmt 4700 Sfmt 4700 E:\FR\FM\18JAR1.SGM 18JAR1](https://thefederalregister.org/doc/82_FR_5373/page/1.svg)
![Federal Register / Vol. 82, No. 11 / Wednesday, January 18, 2017 / Rules and Regulations 5363
• Do not add any additional burden air commerce by prescribing regulations (a) Effective Date
upon the public than was already for practices, methods, and procedures This AD is effective February 22, 2017.
proposed in the SNPRM. the Administrator finds necessary for
safety in air commerce. This regulation (b) Affected ADs
Related Service Information Under 1 None.
is within the scope of that authority
CFR Part 51
because it addresses an unsafe condition (c) Applicability
Airbus has issued Service Bulletin that is likely to exist or develop on
A320–32–1416, including Appendix 01, This AD applies to the Airbus airplanes
products identified in this rulemaking
dated March 10, 2014. This service identified in paragraphs (c)(1) through (c)(4)
action. of this AD, certificated in any category, all
information describes procedures for
inspecting MLG axles and brake flanges Regulatory Findings manufacturer serial numbers.
by doing a detailed visual inspection of (1) Airbus Model A318–111, –112, –121,
We determined that this AD will not
and –122 airplanes.
the chromium plates for damage, a have federalism implications under (2) Airbus Model A319–111, –112, –113,
Barkhausen noise inspection of the Executive Order 13132. This AD will –114, –115, –131, –132, and –133 airplanes.
sliding tube axles for damage, and not have a substantial direct effect on (3) Airbus Model A320–211, –212, –214,
replacement of affected parts if the States, on the relationship between –231, –232, and –233 airplanes.
necessary. This service information is the national government and the States, (4) Airbus Model A321–111, –112, –131,
reasonably available because the or on the distribution of power and –211, –212, –213, –231, and –232 airplanes.
interested parties have access to it responsibilities among the various
through their normal course of business levels of government. (d) Subject
or by the means identified in the For the reasons discussed above, I Air Transport Association (ATA) of
ADDRESSES section. certify that this AD: America Code 32, Landing gear.
1. Is not a ‘‘significant regulatory
Costs of Compliance (e) Reason
action’’ under Executive Order 12866;
We estimate that this AD affects 3 2. Is not a ‘‘significant rule’’ under the This AD was prompted by a report of a
airplanes of U.S. registry. DOT Regulatory Policies and Procedures rupture of a main landing gear (MLG) sliding
We also estimate that it would take (44 FR 11034, February 26, 1979); tube axle. We are issuing this AD to detect
about 18 work-hours per product to 3. Will not affect intrastate aviation in and correct cracks in the axle and (partial)
comply with the basic requirements of Alaska; and detachment of the axle and wheel from the
this AD. The average labor rate is $85 4. Will not have a significant sliding tube, which could result in failure of
per work-hour. Based on these figures, economic impact, positive or negative, an MLG.
we estimate the cost of this AD on U.S. on a substantial number of small entities (f) Compliance
operators to be $4,590, or $1,530 per under the criteria of the Regulatory Comply with this AD within the
product. Flexibility Act. compliance times specified, unless already
In addition, we estimate that any
List of Subjects in 14 CFR Part 39 done.
necessary on-condition actions will take
about 3 work-hours, for a cost of $255 Air transportation, Aircraft, Aviation (g) MLG Sliding Tube Part Number and
per product. We have received no safety, Incorporation by reference, Serial Number Identification
definitive data that would enable us to Safety. Within 3 months after the effective date of
provide part cost estimates for the on- this AD: Do an inspection to identify the part
condition actions specified in this AD. Adoption of the Amendment number and serial number of the MLG
We have no way of determining the Accordingly, under the authority sliding tubes installed on the airplane. A
number of aircraft that might need these delegated to me by the Administrator, review of airplane maintenance records is
actions. the FAA amends 14 CFR part 39 as acceptable in lieu of this inspection if the
follows: part number and serial number of the MLG
Authority for This Rulemaking sliding tubes can be conclusively determined
Title 49 of the United States Code PART 39—AIRWORTHINESS from that review.
specifies the FAA’s authority to issue DIRECTIVES
(h) Identification of Airplanes Not Affected
rules on aviation safety. Subtitle I, by the Requirements of Paragraph (i) of this
section 106, describes the authority of ■ 1. The authority citation for part 39
AD
the FAA Administrator. ‘‘Subtitle VII: continues to read as follows:
An airplane with a manufacturer serial
Aviation Programs,’’ describes in more Authority: 49 U.S.C. 106(g), 40113, 44701.
number (MSN) not listed in figure 1 to
detail the scope of the Agency’s paragraph (h) of this AD is not affected by the
§ 39.13 [Amended]
authority. requirements of paragraph (i) of this AD,
We are issuing this rulemaking under ■ 2. The FAA amends § 39.13 by adding provided it can be determined that no MLG
the authority described in ‘‘Subtitle VII, the following new airworthiness sliding tube having a part number and serial
Part A, Subpart III, Section 44701: directive (AD): number listed in table 1 to paragraphs (h), (i),
General requirements.’’ Under that 2017–01–11 Airbus: Amendment 39–18778; (k)(1), (k)(2), (l)(1), and (l)(2) of this AD has
section, Congress charges the FAA with Docket No. FAA–2015–0831; Directorate been installed on that airplane since first
promoting safe flight of civil aircraft in Identifier 2014–NM–061–AD. flight of the airplane.
FIGURE 1 TO PARAGRAPH (H) OF THIS AD
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Affected Airplanes Listed by MSN
0179 0214 0296 0412 0558 0604
0607 0668 0704 0720 0726 0731
0754 0771 0799 0828 0841 0855
0909 0914 0925 0939 0986 1028
1030 1041 1070 1083 1093 1098
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![Federal Register / Vol. 82, No. 11 / Wednesday, January 18, 2017 / Rules and Regulations 5365
Airworthiness Directive 2014–0058, dated for certain areas of the fuselage, the apply to certain Fokker Services B.V.
March 11, 2014, for related information. This current threshold of an Airworthiness Model F28 Mark 0100 airplanes. The
MCAI may be found in the AD docket on the Limitations Section inspection is NPRM published in the Federal
Internet at http://www.regulations.gov by insufficient to detect early crack Register on September 8, 2016 (81 FR
searching for and locating Docket No. FAA–
2015–0831.
development. This AD requires one time 62029) (‘‘the NPRM’’). The NPRM was
high and low frequency eddy current prompted by an analysis which
(p) Material Incorporated by Reference inspections of the affected fuselage skin determined that, for certain areas of the
(1) The Director of the Federal Register for cracks, and repair if necessary. We fuselage, the current threshold of an
approved the incorporation by reference are issuing this AD to address the unsafe Airworthiness Limitations Section
(IBR) of the service information listed in this condition on these products. inspection is insufficient to detect early
paragraph under 5 U.S.C. 552(a) and 1 CFR crack development. The NPRM
DATES: This AD is effective February 22,
part 51. proposed to require one time high and
(2) You must use this service information 2017.
The Director of the Federal Register low frequency eddy current inspections
as applicable to do the actions required by
this AD, unless this AD specifies otherwise. approved the incorporation by reference of the affected fuselage skin for cracks,
(i) Airbus Service Bulletin A320–32–1416, of a certain publication listed in this AD and repair if necessary. We are issuing
including Appendix 01, dated March 10, as of February 22, 2017. this AD to detect and correct cracks in
2014. ADDRESSES: For service information the fuselage skin; such cracking could
(ii) Reserved. identified in this final rule, contact result in reduced structural integrity of
(3) For service information identified in the fuselage.
Fokker Services B.V., Technical
this AD, contact Airbus, Airworthiness The European Aviation Safety Agency
Office—EIAS, 1 Rond Point Maurice Services Dept., P.O. Box 1357, 2130 EL
Hoofddorp, the Netherlands; telephone: (EASA), which is the Technical Agent
Bellonte, 31707 Blagnac Cedex, France; for the Member States of the European
telephone +33 5 61 93 36 96; fax +33 5 61 +31 (0)88–6280–350; fax: +31 (0)88–
6280–111; email: technicalservices@ Union, has issued EASA Airworthiness
93 44 51; email account.airworth-eas@
airbus.com; Internet http://www.airbus.com. fokker.com; Internet http:// Directive Airworthiness Directive 2016–
(4) You may view this service information www.myfokkerfleet.com. You may view 0029R1, dated November 17, 2016
at the FAA, Transport Airplane Directorate, this referenced service information at (referred to after this as the Mandatory
1601 Lind Avenue SW., Renton, WA. For the FAA, Transport Airplane Continuing Airworthiness Information,
information on the availability of this
Directorate, 1601 Lind Avenue SW., or ‘‘the MCAI’’), to correct an unsafe
material at the FAA, call 425–227–1221. condition for certain Fokker Services
(5) You may view this service information Renton, WA. For information on the
availability of this material at the FAA, B.V. Model F28 Mark 0100 airplanes.
that is incorporated by reference at the The MCAI states:
National Archives and Records call 425–227–1221. It is also available
Administration (NARA). For information on on the Internet at http:// A complementary fatigue and damage
the availability of this material at NARA, call www.regulations.gov by searching for tolerance analysis was accomplished by the
202–741–6030, or go to: http:// and locating Docket No. FAA–2016– design approval holder on the traffic
www.archives.gov/federal-register/cfr/ibr- collision avoidance system (TCAS) antenna
9058. installation on the top of the fuselage
locations.html.
Examining the AD Docket between station (STA) 6805 and STA7305.
Issued in Renton, Washington, on January Based on the results, it was determined that
4, 2017. You may examine the AD docket on for the affected area, the current 58 000 flight
Michael Kaszycki, the Internet at http:// cycles (FC) threshold of Airworthiness
Acting Manager, Transport Airplane www.regulations.gov by searching for Limitations Section (ALS) inspection task
Directorate, Aircraft Certification Service. and locating Docket No. FAA–2016– 533001–00–20 and 533028–00–20 (special
9058; or in person at the Docket detailed inspection of longitudinal lap joints)
[FR Doc. 2017–00408 Filed 1–17–17; 8:45 am]
Management Facility between 9 a.m. is insufficient to timely detect possible crack
BILLING CODE 4910–13–P development.
and 5 p.m., Monday through Friday, This condition, if not detected and
except Federal holidays. The AD docket corrected, could affect the structural integrity
DEPARTMENT OF TRANSPORTATION contains this AD, the regulatory of the fuselage in this area.
evaluation, any comments received, and To address this potential unsafe condition,
Federal Aviation Administration other information. The street address for Fokker Services published Service Bulletin
the Docket Office (telephone 800–647– (SB) SBF100–53–130 to provide inspection
14 CFR Part 39 5527) is Docket Management Facility, instructions.
Consequently, EASA issued AD 2016–0029
U.S. Department of Transportation, to require a one-time inspection of the
[Docket No. FAA–2016–9058; Directorate
Identifier 2016–NM–024–AD; Amendment Docket Operations, M–30, West fuselage skin around the largest TCAS
39–18771; AD 2017–01–04] Building Ground Floor, Room W12–140, antenna external doubler and of the
1200 New Jersey Avenue SE., longitudinal lap joint at stringer (STR) 37
RIN 2120–AA64 Washington, DC 20590. between fuselage STA6805 and STA7305.
FOR FURTHER INFORMATION CONTACT: Tom Since that [EASA] AD was issued, it was
Airworthiness Directives; Fokker discovered that another ALS inspection task,
Rodriguez, Aerospace Engineer,
Services B.V. Airplanes 533028–00–20, is also related to this subject.
International Branch, ANM–116, This [EASA] AD is revised to clarify that the
AGENCY: Federal Aviation Transport Airplane Directorate, FAA, inspection threshold of both ALS inspection
Administration (FAA), Department of 1601 Lind Avenue SW., Renton, WA tasks has been re-assessed. It is expected that
Transportation (DOT). 98057–3356; telephone 425–227–1137; a repetitive inspection task will be included
mstockstill on DSK3G9T082PROD with RULES
fax 425 227 1149. in the ALS, which will cover only the area
ACTION: Final rule.
close to the TCAS antenna installation. For
SUPPLEMENTARY INFORMATION:
SUMMARY: We are adopting a new the remainder of the affected lap joint, no
Discussion change is anticipated and this will therefore
airworthiness directive (AD) for certain continue to be inspected in accordance with
Fokker Services B.V. Model F28 Mark We issued a notice of proposed the existing ALS tasks.
0100 airplanes. This AD was prompted rulemaking (NPRM) to amend 14 CFR This [EASA] AD is still considered to be
by an analysis which determined that, part 39 by adding an AD that would an interim action and further [EASA] AD
VerDate Sep<11>2014 16:39 Jan 17, 2017 Jkt 241001 PO 00000 Frm 00031 Fmt 4700 Sfmt 4700 E:\FR\FM\18JAR1.SGM 18JAR1](https://thefederalregister.org/doc/82_FR_5373/page/4.svg)
Document Created: 2018-02-01 15:19:42
Document Modified: 2018-02-01 15:19:42
| 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 February 22, 2017. | |
| Contact | Sanjay Ralhan, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356; telephone 425-227-1405; fax 425-227-1149. | |
| FR Citation | 82 FR 5362 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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