81 FR 10545 - Airworthiness Directives; Airbus Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 81, Issue 40 (March 1, 2016)
Federal Aviation Administration
Federal Register Volume 81, Issue 40 (March 1, 2016)
| Page Range | 10545-10549 | |
| FR Document | 2016-04288 |
[Federal Register Volume 81, Number 40 (Tuesday, March 1, 2016)] [Proposed Rules] [Pages 10545-10549] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2016-04288] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2016-3983; Directorate Identifier 2015-NM-009-AD] RIN 2120-AA64 Airworthiness Directives; Airbus Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). ----------------------------------------------------------------------- SUMMARY: We propose to adopt a new airworthiness directive (AD) for certain Airbus Model A330-200 Freighter series airplanes; Model A330- 200 and A330-300 series airplanes; Model A340-200 and A340-300 series airplanes; Model A340-500 series airplanes; and Model A340-600 series airplanes. This proposed AD was prompted by a report indicating that, during an operational test of a ram air turbine (RAT), the RAT did not deploy in automatic mode. This proposed AD would require identification of the manufacturer, part number, and serial number of the RAT, and re- identifying and modifying the RAT if necessary. We are proposing this AD to prevent non-deployment of the RAT, which, if preceded by a total engine flame-out, or during a total loss of normal electrical power generation, [[Page 10546]] could result in reduced control of the airplane. DATES: We must receive comments on this proposed AD by April 15, 2016. ADDRESSES: You may send comments, using the procedures found in 14 CFR 11.43 and 11.45, by any of the following methods:Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments. Fax: 202-493-2251. Mail: U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590. Hand Delivery: U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE., Washington, DC, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. For Airbus service information identified in this NPRM, contact Airbus SAS, Airworthiness Office--EAL, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France; telephone +33 5 61 93 36 96; fax +33 5 61 93 45 80; email [email protected]; Internet http://www.airbus.com. For Hamilton Sundstrand service information identified in this AD, contact Hamilton Sundstrand, Technical Publications, Mail Stop 302-9, 4747 Harrison Avenue, P.O. Box 7002, Rockford, IL 61125- 7002; telephone 860-654-3575; fax 860-998-4564; email [email protected]; Internet http://www.hamiltonsundstrand.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. Examining the AD Docket You may examine the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016- 3983; 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 proposed AD, the regulatory evaluation, any comments received, and other information. The street address for the Docket Operations office (telephone 800-647-5527) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt. FOR FURTHER INFORMATION CONTACT: Vladimir Ulyanov, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356; telephone 425-227-1138; fax 425-227-1149. SUPPLEMENTARY INFORMATION: Comments Invited We invite you to send any written relevant data, views, or arguments about this proposed AD. Send your comments to an address listed under the ADDRESSES section. Include ``Docket No. FAA-2016-3983; Directorate Identifier 2015-NM-009-AD'' at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of this proposed AD. We will consider all comments received by the closing date and may amend this proposed AD based on those comments. We will post all comments we receive, without change, to http://www.regulations.gov, including any personal information you provide. We will also post a report summarizing each substantive verbal contact we receive about this proposed AD. Discussion The European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Union, has issued EASA Airworthiness Directive 2015-0008, dated January 15, 2015 (referred to after this as the Mandatory Continuing Airworthiness Information, or ``the MCAI''), to correct an unsafe condition for certain Airbus Model A330-200 Freighter series airplanes; Model A330-200, and A330-300 series airplanes; Model A340-200, and A340-300 series airplanes; Model A340-500 series airplanes; and Model A340-600 series airplanes. The MCAI states: During a scheduled Ram Air Turbine (RAT) operational test on an A330 aeroplane, the RAT did not deploy in automatic mode. The subsequent investigation conducted by the RAT manufacturer Hamilton Sundstrand (HS) and Arkwin Industries, revealed that this failure to deploy was due to an inadequate stroke margin in the manufacturing shimming procedure of the actuator deployment solenoids. This condition, if not corrected, could possibly result in reduced control of the aeroplane, particularly if occurring following a total engine flame out, or during a total loss of normal electrical power generation. Prompted by this unsafe condition, Airbus issued Service Bulletin (SB) A330-29-3126, SB A340-29-4097 and SB A340-29-5025, providing instructions to identify the manufacturer, part number (P/ N) and serial number (s/n) of the RAT actuator, and to modify the shimming procedure for the affected RAT actuator. For the reasons described above, this [EASA] AD requires identification of the affected RAT actuators and, depending on its configuration (modified or not), the accomplishment of applicable corrective actions [modifying the RAT actuator. Additional actions include re-identifying the RAT actuator part number and RAT part number, as applicable.] You may examine the MCAI in the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016- 3983. Related ADs EASA and the FAA have issued additional ADs related to the RAT. FAA AD 2012-21-19, Amendment 39-17235 (77 FR 65812, October 31, 2012, which corresponds to EASA AD 2011-0197, dated October 10, 2011), requires an inspection of the RAT anti-stall valve in the pump housing for correct setting, re-identification of the RAT pump, performing a functional ground test of the RAT, and replacement of the RAT pump or the RAT assembly with a serviceable part if necessary. FAA AD 2012-21-19 is applicable to all Airbus Model A330-200 Freighter series airplanes; Model A330-200 and -300 series airplanes; and Model A340-200 and -300 series airplanes. The FAA also issued AD 2012-21-20, Amendment 39-17236 (77 FR 65799, October 31, 2012), which corresponds to EASA AD 2011-0204, dated October 14, 2011. FAA AD 2012-21-20 requires identification of the supplier, part number, and serial number of the RAT actuator; and re- identification of the RAT actuator and RAT, or replacement of the RAT actuator with a serviceable unit and re-identification of the RAT, if necessary. FAA AD 2012-21-20 is applicable to certain Airbus Model A330-200 Freighter series airplanes, Model A330-200 and -300 series airplanes, and Model A340-200, -300, -500, and -600 series airplanes. In addition, the FAA issued AD 2015-26-02, Amendment 39-18350 (80 FR 81174, December 29, 2015), which corresponds to EASA AD 2013-0274, dated November 15, 2013. FAA AD 2015-26-02 requires, for certain airplanes, identification of the part number, serial number, and standard of the RAT pump, RAT module, RAT actuator, and RAT lower gearbox assembly; and corrective actions if necessary. For certain other airplanes, AD 2015-26-02 requires re-identification or replacement of the RAT module. Related Service Information Under 1 CFR Part 51 Airbus has issued the following service information, which describes [[Page 10547]] procedures for identifying the supplier, part number, and serial number of the installed RAT actuator; modifying the RAT; and re-identifying the RAT actuator and RAT. Service Bulletin A330-29-3126, dated June 12, 2014. Service Bulletin A340-29-4097, dated June 12, 2014. Service Bulletin A340-29-5025, dated June 16, 2014. Hamilton Sundstrand has issued Service Bulletins ERPS06M-29-21, dated May 27, 2014; and ERPS33T-29-7, dated June 6, 2014. This service information describes procedures for identifying the affected RAT actuator and RAT part numbers and serial numbers, modifying affected actuators, and re-identifying affected RAT actuators and RATs. 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. FAA's Determination and Requirements of This Proposed AD This product has been approved by the aviation authority of another country, and is approved for operation in the United States. Pursuant to our bilateral agreement with the State of Design Authority, we have been notified of the unsafe condition described in the MCAI and service information referenced above. We are proposing this AD because we evaluated all pertinent information and determined an unsafe condition exists and is likely to exist or develop on other products of these same type designs. Costs of Compliance We estimate that this proposed AD affects 84 airplanes of U.S. registry. We also estimate that it would take about 1 work-hour per product to comply with the basic requirements of this proposed AD. The average labor rate is $85 per work-hour. Based on these figures, we estimate the cost of this proposed AD on U.S. operators to be $7,140, or $85 per product. In addition, we estimate that any necessary follow-on actions would take about 14 work-hours and require parts costing $427,301, for a cost of $428,491 per product. We have no way of determining the number of aircraft that might need 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 proposed AD would not have federalism implications under Executive Order 13132. This proposed AD would 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 this proposed regulation: 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. The Proposed Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA proposes to amend 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): Airbus: Docket No. FAA-2016-3983; Directorate Identifier 2015-NM- 009-AD. (a) Comments Due Date We must receive comments by April 15, 2016. (b) Affected ADs This AD affects AD 2012-21-19, Amendment 39-17235 (77 FR 65812, October 31, 2012); AD 2012-21-20, Amendment 39-17236 (77 FR 65799, October 31, 2012); and AD 2015-26-02, Amendment 39-18350 (80 FR 81174, December 29, 2015). (c) Applicability This AD applies to the airplanes identified in paragraphs (c)(1) through (c)(7) of this AD, certificated in any category. (1) Airbus Model A330-223F and -243F airplanes, all manufacturer serial numbers; except those on which Airbus Modification 204067 has been embodied in production. (2) Airbus Model A330-201, -202, -203, -223, and -243 airplanes, all manufacturer serial numbers; except those on which Airbus Modification 204067 has been embodied in production. (3) Airbus Model A330-301, -302, -303, -321, -322, -323,- 341, - 342, and -343 airplanes, all manufacturer serial numbers; except those on which Airbus Modification 204067 has been embodied in production. (4) Airbus Model A340-211, -212, and -213, airplanes, all manufacturer serial numbers. (5) Airbus Model A340-311, -312, and -313 airplanes, all manufacturer serial numbers. (6) Airbus Model A340-541 airplanes, all manufacturer serial numbers. (7) Airbus Model A340-642 airplanes, all manufacturer serial numbers. (d) Subject Air Transport Association (ATA) of America Code 29, Hydraulic Power. (e) Reason This AD was prompted by a report indicating that, during an operational test of a ram air turbine (RAT), the RAT did not deploy in automatic mode. We are issuing this AD to prevent non-deployment of the RAT, which, if preceded by a total engine flame-out, or during a total loss of normal electrical power generation, could result in reduced control of the airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Identification and Replacement for Certain Airbus Model A330, and A340-200 and -300 Airplanes For Airbus Model A330-200 Freighter series airplanes, Model A330-200 and -300 series airplanes, and Model A340-200 and -300 series airplanes: Within 30 months after the effective date of this AD, identify the supplier, part number, and serial number of the installed RAT actuator, in accordance with the Accomplishment Instructions of Airbus Service Bulletin A330-29-3126, dated June 12, 2014; or Airbus Service Bulletin A340-29-4097, dated June 12, 2014; as applicable. [[Page 10548]] (1) If the supplier identified is Arkwin Industries, and the identified RAT actuator part number and serial number are listed in Hamilton Sundstrand Service Bulletin ERPS06M-29-21, dated May 27, 2014, and the serial number is included in table 2 of Hamilton Sundstrand Service Bulletin ERPS06M-29-21, dated May 27, 2014, with a description of ``correctly shimmed:'' Within 30 months after the effective date of this AD, re-identify the actuator and the RAT, in accordance with the Accomplishment Instructions of Airbus Service Bulletin A330-29-3126, dated June 12, 2014; or Airbus Service Bulletin A340-29-4097, dated June 12, 2014; as applicable. (2) If the supplier identified is Arkwin Industries, and the identified actuator RAT part number and serial number are listed in Hamilton Sundstrand Service Bulletin ERPS06M-29-21, dated May 27, 2014, and the serial number is included in table 2 of Hamilton Sundstrand Service Bulletin ERPS06M-29-21, dated May 27, 2014, with a description of ``incorrectly shimmed:'' Within 30 months after the effective date of this AD, modify the RAT actuator and re-identify the RAT, in accordance with the Accomplishment Instructions of Airbus Service Bulletin A330-29-3126, dated June 12, 2014; or Airbus Service Bulletin A340-29-4097, dated June 12, 2014; as applicable. (3) If the supplier identified is Arkwin Industries, and the identification plate for the RAT actuator is missing, or the part number and serial number are not listed in Hamilton Sundstrand Service Bulletin ERPS06M-29-21, dated May 27, 2014: Within 30 months after the effective date of this AD, modify the RAT actuator and re- identify the RAT, in accordance with the Accomplishment Instructions of Airbus Service Bulletin A330-29-3126, dated June 12, 2014; or Airbus Service Bulletin A340-29-4097, dated June 12, 2014; as applicable. (h) Identification and Replacement for Certain Airbus Model A340-500 and -600 Airplanes For Airbus Model A340-500 and -600 airplanes: Within 30 months after the effective date of this AD, identify the part number and serial number of the installed RAT actuator, in accordance with the Accomplishment Instructions of Airbus Service Bulletin A340-29-5025, dated June 16, 2014. (1) If the identified RAT actuator part number and serial number are listed in Hamilton Sundstrand Service Bulletin ERPS33T-29-7, dated June 6, 2014, and the serial number is included in table 2 of Hamilton Sundstrand Service Bulletin ERPS33T-29-7, dated June 6, 2014, with a description of ``correctly shimmed:'' Within 30 months after the effective date of this AD, re-identify the actuator and the RAT, in accordance with the Accomplishment Instructions of Airbus Service Bulletin A340-29-5025, dated June 16, 2014. (2) If the identified RAT actuator part number and serial number are listed in Hamilton Sundstrand Service Bulletin ERPS33T-29-7, dated June 6, 2014, and the serial number is included in table 2 of Hamilton Sundstrand Service Bulletin ERPS33T-29-7, dated June 6, 2014, with a description of ``incorrectly shimmed:'' Within 30 months after the effective date of this AD, modify the RAT actuator and re-identify the RAT, in accordance with the Accomplishment Instructions of Airbus Service Bulletin A340-29-5025, dated June 16, 2014. (3) If the identification plate for the RAT actuator is missing, or the part number and serial number are not listed in Hamilton Sundstrand Service Bulletin ERPS33T-29-7, dated June 6, 2014: Within 30 months after the effective date of this AD, modify the RAT actuator and re-identify the RAT, in accordance with the Accomplishment Instructions of Airbus Service Bulletin A340-29-5025, dated June 16, 2014. (i) Terminating Action for Certain Requirements of Other ADs (1) For Airbus Model A330-200 Freighter, A330-200, and A330-300 series airplanes; and Model A340-200 and -300 series airplanes: Accomplishment of the actions required by paragraph (g)(1), (g)(2), or (g)(3) of this AD constitutes compliance with the requirements of paragraph (g)(1) of AD 2012-21-19, Amendment 39-17235 (77 FR 65812, October 31, 2012); paragraph (g) of AD 2012-21-20, Amendment 39- 17236 (77 FR 65799, October 31, 2012); and paragraphs (g), (h), and (i) of AD 2015-26-02, Amendment 39-18350 (80 FR 81174, December 29, 2015), for that airplane only. (2) For Airbus Model A340-500 and -600 series airplanes: Accomplishment of the actions required by paragraphs (h)(1), (h)(2), and (h)(3) of this AD constitutes compliance with the requirements of paragraphs (h)(1) and (h)(2) of AD 2012-21-20, Amendment 39-17236 (77 FR 65799, October 31, 2012); and paragraph (j) of AD 2015-26-02, Amendment 39-18350 (80 FR 81174, December 29, 2015), for that airplane only. (j) Parts Installation Limitations As of the effective date of this AD, no person may install any RAT actuator or any RAT having a part number identified in table 1 to paragraph (j) of this AD, on any airplane, unless it meets the conditions specified in paragraph (j)(1) or (j)(2) of this AD, as applicable. Table 1 to Paragraph (j) of This AD--Affected Part Numbers ------------------------------------------------------------------------ RAT actuator part Affected Airbus airplane models RAT part number number ------------------------------------------------------------------------ Model A330-200 and -300 series 1720934C, 5912958, 5915768 airplanes. 1720934D, 766351A, 768084A, 770379A, 770952C, 770952D, 770952E. Model A330-200 Freighter series 1720934C, 5912958, 5915768 airplanes. 1720934D, 766351A, 768084A, 770379A, 770952C, 770952D, 770952E. Model A340-200 and -300 series 1720934C, 5912958, 5915768 airplanes. 1720934D, 766351A, 768084A, 770379A, 770952C, 770952D, 770952E. Model A340-500 and -600 series 772722H, 772722J, 5912536, 5915769 airplanes. 772722L. ------------------------------------------------------------------------ (1) For Airbus Model A330-200 Freighter series airplanes; Model A330-200, and A330-300 series airplanes; and Model A340-200 and -300 series airplanes: The RAT actuator or RAT has a serial number listed as affected and modified in Hamilton Sundstrand Service Bulletin ERPS06M-29-21, dated May 27, 2014, and the RAT has been re- identified in accordance with the Accomplishment Instructions of Airbus Service Bulletin A330-29-3126, dated June 12, 2014; or Airbus Service Bulletin A340-29-4097, dated June 12, 2014. (2) For Airbus Model A340-500 and -600 series airplanes: The RAT actuator or the RAT has a serial number listed as affected and modified in Hamilton Sundstrand Service Bulletin ERPS33T-29-7, dated June 6, 2014, and the RAT has been re-identified in accordance with the Accomplishment Instructions of Airbus Service Bulletin A340-29- 5025, dated June 16, 2014. (k) 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: Vladimir Ulyanov, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356; telephone 425-227-1138; 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. [[Page 10549]] (2) Contacting the Manufacturer: For any requirement in this AD to obtain corrective actions from a manufacturer, the action must be accomplished using a method approved by the Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA; or the European Aviation Safety Agency (EASA); or Airbus's EASA Design Organization Approval (DOA). If approved by the DOA, the approval must include the DOA-authorized signature. (3) Required for Compliance (RC): If any Airbus 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. (l) Related Information (1) Refer to Mandatory Continuing Airworthiness Information (MCAI) EASA Airworthiness Directive 2015-0008, dated January 15, 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-2016-3983. (2) For Airbus service information identified in this proposed AD, contact Airbus SAS, Airworthiness Office--EAL, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France; telephone +33 5 61 93 36 96; fax +33 5 61 93 45 80; email [email protected]; Internet http://www.airbus.com. For Hamilton Sundstrand service information identified in this AD, contact Hamilton Sundstrand, Technical Publications, Mail Stop 302-9, 4747 Harrison Avenue, P.O. Box 7002, Rockford, IL 61125-7002; telephone 860-654-3575; fax 860-998-4564; email [email protected]; Internet http://www.hamiltonsundstrand.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. Issued in Renton, Washington, on February 19, 2016. Dorr M. Anderson, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2016-04288 Filed 2-29-16; 8:45 am] BILLING CODE 4910-13-P
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agreement with the European (2) Is not a ‘‘significant rule’’ under (f) Alternative Methods of Compliance
Community, EASA has notified us of the DOT Regulatory Policies and (AMOCs)
the unsafe condition described in the Procedures (44 FR 11034, February 26, The Manager, Engine Certification Office,
MCAI and service information 1979), FAA, may approve AMOCs for this AD. Use
referenced above. We are proposing this (3) Will not affect intrastate aviation the procedures found in 14 CFR 39.19 to
NPRM because we evaluated all in Alaska to the extent that it justifies make your request. You may email your
information provided by EASA and request to: ANE-AD-AMOC@faa.gov.
making a regulatory distinction, and
determined the unsafe condition exists (4) Will not have a significant (g) Related Information
and is likely to exist or develop on other economic impact, positive or negative, (1) For more information about this AD,
products of the same type design. This on a substantial number of small entities contact Philip Haberlen, Aerospace Engineer,
NPRM would require removing the pre- under the criteria of the Regulatory Engine Certification Office, FAA, Engine &
modification (mod) TU357 gas generator Flexibility Act. Propeller Directorate, 1200 District Avenue,
module (M03) and replacing with a part Burlington, MA 01803; phone: 781–238–
eligible for installation. List of Subjects in 14 CFR Part 39 7770; fax: 781–238–7199; email:
philip.haberlen@faa.gov.
Costs of Compliance Air transportation, Aircraft, Aviation (2) Refer to MCAI European Aviation
safety, Incorporation by reference, Safety Agency AD 2016–0009, dated January
We estimate that this proposed AD Safety. 13, 2016, for more information. You may
affects 426 engines installed on examine the MCAI in the AD docket on the
helicopters of U.S. registry. We also The Proposed Amendment Internet at http://www.regulations.gov by
estimate that it would take about 40 Accordingly, under the authority searching for and locating it in Docket No.
hours per engine to comply with this delegated to me by the Administrator, FAA–2016–2859.
proposed AD. The average labor rate is the FAA proposes to amend 14 CFR part Issued in Burlington, Massachusetts, on
$85 per hour. Required parts cost about 39 as follows: February 18, 2016.
$16,500 per engine. Based on these Ann C. Mollica,
figures, we estimate the cost of this PART 39—AIRWORTHINESS Acting Manager, Engine & Propeller
proposed AD on U.S. operators to be DIRECTIVES Directorate, Aircraft Certification Service.
$8,477,400. [FR Doc. 2016–04284 Filed 2–29–16; 8:45 am]
■ 1. The authority citation for part 39
Authority for This Rulemaking continues to read as follows: BILLING CODE 4910–13–P
Title 49 of the United States Code Authority: 49 U.S.C. 106(g), 40113, 44701.
specifies the FAA’s authority to issue DEPARTMENT OF TRANSPORTATION
rules on aviation safety. Subtitle I, § 39.13 [Amended]
section 106, describes the authority of ■ 2. The FAA amends § 39.13 by adding Federal Aviation Administration
the FAA Administrator. ‘‘Subtitle VII: the following new airworthiness
Aviation Programs,’’ describes in more directive (AD): 14 CFR Part 39
detail the scope of the Agency’s Turbomeca S.A.: Docket No. FAA–2016– [Docket No. FAA–2016–3983; Directorate
authority. 2859; Directorate Identifier 2016–NE– Identifier 2015–NM–009–AD]
We are issuing this rulemaking under 04–AD.
the authority described in ‘‘Subtitle VII, RIN 2120–AA64
(a) Comments Due Date
Part A, Subpart III, Section 44701:
General requirements.’’ Under that We must receive comments by May 2, Airworthiness Directives; Airbus
2016. Airplanes
section, Congress charges the FAA with
promoting safe flight of civil aircraft in (b) Affected ADs AGENCY: Federal Aviation
air commerce by prescribing regulations None. Administration (FAA), DOT.
for practices, methods, and procedures ACTION: Notice of proposed rulemaking
(c) Applicability
the Administrator finds necessary for (NPRM).
safety in air commerce. This regulation This AD applies to all Arriel 1D and 1D1
is within the scope of that authority turboshaft engines with a pre-modification
(mod) TU357 gas generator module (M03), SUMMARY: We propose to adopt a new
because it addresses an unsafe condition installed. airworthiness directive (AD) for certain
that is likely to exist or develop on Airbus Model A330–200 Freighter series
products identified in this rulemaking (d) Reason airplanes; Model A330–200 and A330–
action. This AD was prompted by reports of 300 series airplanes; Model A340–200
divergent rubbing between the piston shaft and A340–300 series airplanes; Model
Regulatory Findings small diameter labyrinth and the rear bearing A340–500 series airplanes; and Model
We determined that this proposed AD support. We are issuing this AD to prevent A340–600 series airplanes. This
would not have federalism implications failure of the labyrinth seal and engine, in-
flight shutdown, and loss of control of the
proposed AD was prompted by a report
under Executive Order 13132. This indicating that, during an operational
helicopter.
proposed AD would not have a test of a ram air turbine (RAT), the RAT
substantial direct effect on the States, on (e) Actions and Compliance did not deploy in automatic mode. This
asabaliauskas on DSK5VPTVN1PROD with PROPOSALS
the relationship between the national Comply with this AD within the proposed AD would require
Government and the States, or on the compliance times specified, unless already identification of the manufacturer, part
distribution of power and done. number, and serial number of the RAT,
responsibilities among the various (1) Within 4 months or 240 engine and re-identifying and modifying the
levels of government. operating hours after the effective date of this
AD, whichever occurs later, remove the pre-
RAT if necessary. We are proposing this
For the reasons discussed above, I modification (mod) TU357 gas generator AD to prevent non-deployment of the
certify this proposed regulation: module (M03) from service and replace with RAT, which, if preceded by a total
(1) Is not a ‘‘significant regulatory a part eligible for installation. engine flame-out, or during a total loss
action’’ under Executive Order 12866, (2) Reserved. of normal electrical power generation,
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could result in reduced control of the Transport Airplane Directorate, FAA, affected RAT actuators and, depending on its
airplane. 1601 Lind Avenue SW., Renton, WA configuration (modified or not), the
98057–3356; telephone 425–227–1138; accomplishment of applicable corrective
DATES: We must receive comments on actions [modifying the RAT actuator.
this proposed AD by April 15, 2016. fax 425–227–1149.
Additional actions include re-identifying the
ADDRESSES: You may send comments, SUPPLEMENTARY INFORMATION: RAT actuator part number and RAT part
using the procedures found in 14 CFR Comments Invited number, as applicable.]
11.43 and 11.45, by any of the following We invite you to send any written You may examine the MCAI in the
methods: relevant data, views, or arguments about AD docket on the Internet at http://
• Federal eRulemaking Portal: Go to www.regulations.gov by searching for
this proposed AD. Send your comments
http://www.regulations.gov. Follow the and locating Docket No. FAA–2016–
to an address listed under the
instructions for submitting comments. 3983.
ADDRESSES section. Include ‘‘Docket No.
• Fax: 202–493–2251.
• Mail: U.S. Department of FAA–2016–3983; Directorate Identifier Related ADs
Transportation, Docket Operations, 2015–NM–009–AD’’ at the beginning of
your comments. We specifically invite EASA and the FAA have issued
M–30, West Building Ground Floor, additional ADs related to the RAT. FAA
Room W12–140, 1200 New Jersey comments on the overall regulatory,
economic, environmental, and energy AD 2012–21–19, Amendment 39–17235
Avenue SE., Washington, DC 20590. (77 FR 65812, October 31, 2012, which
• Hand Delivery: U.S. Department of aspects of this proposed AD. We will
consider all comments received by the corresponds to EASA AD 2011–0197,
Transportation, Docket Operations, dated October 10, 2011), requires an
M–30, West Building Ground Floor, closing date and may amend this
proposed AD based on those comments. inspection of the RAT anti-stall valve in
Room W12–140, 1200 New Jersey the pump housing for correct setting, re-
Avenue SE., Washington, DC, between 9 We will post all comments we
receive, without change, to http:// identification of the RAT pump,
a.m. and 5 p.m., Monday through performing a functional ground test of
Friday, except Federal holidays. www.regulations.gov, including any
personal information you provide. We the RAT, and replacement of the RAT
For Airbus service information pump or the RAT assembly with a
identified in this NPRM, contact Airbus will also post a report summarizing each
substantive verbal contact we receive serviceable part if necessary. FAA AD
SAS, Airworthiness Office—EAL, 1 2012–21–19 is applicable to all Airbus
Rond Point Maurice Bellonte, 31707 about this proposed AD.
Model A330–200 Freighter series
Blagnac Cedex, France; telephone +33 5 Discussion airplanes; Model A330–200 and –300
61 93 36 96; fax +33 5 61 93 45 80; email The European Aviation Safety Agency series airplanes; and Model A340–200
airworthiness.A330-A340@airbus.com; (EASA), which is the Technical Agent and –300 series airplanes.
Internet http://www.airbus.com. For for the Member States of the European The FAA also issued AD 2012–21–20,
Hamilton Sundstrand service Union, has issued EASA Airworthiness Amendment 39–17236 (77 FR 65799,
information identified in this AD, Directive 2015–0008, dated January 15, October 31, 2012), which corresponds to
contact Hamilton Sundstrand, Technical 2015 (referred to after this as the EASA AD 2011–0204, dated October 14,
Publications, Mail Stop 302–9, 4747 Mandatory Continuing Airworthiness 2011. FAA AD 2012–21–20 requires
Harrison Avenue, P.O. Box 7002, Information, or ‘‘the MCAI’’), to correct identification of the supplier, part
Rockford, IL 61125–7002; telephone an unsafe condition for certain Airbus number, and serial number of the RAT
860–654–3575; fax 860–998–4564; email Model A330–200 Freighter series actuator; and re-identification of the
tech.solutions@hs.utc.com; Internet airplanes; Model A330–200, and A330– RAT actuator and RAT, or replacement
http://www.hamiltonsundstrand.com. 300 series airplanes; Model A340–200, of the RAT actuator with a serviceable
You may view this referenced service and A340–300 series airplanes; Model unit and re-identification of the RAT, if
information at the FAA, Transport A340–500 series airplanes; and Model necessary. FAA AD 2012–21–20 is
Airplane Directorate, 1601 Lind Avenue A340–600 series airplanes. The MCAI applicable to certain Airbus Model
SW., Renton, WA. For information on states: A330–200 Freighter series airplanes,
the availability of this material at the Model A330–200 and –300 series
FAA, call 425–227–1221. During a scheduled Ram Air Turbine
(RAT) operational test on an A330 aeroplane, airplanes, and Model A340–200, –300,
Examining the AD Docket the RAT did not deploy in automatic mode. –500, and –600 series airplanes.
The subsequent investigation conducted by In addition, the FAA issued AD 2015–
You may examine the AD docket on the RAT manufacturer Hamilton Sundstrand 26–02, Amendment 39–18350 (80 FR
the Internet at http:// (HS) and Arkwin Industries, revealed that 81174, December 29, 2015), which
www.regulations.gov by searching for this failure to deploy was due to an corresponds to EASA AD 2013–0274,
and locating Docket No. FAA–2016– inadequate stroke margin in the dated November 15, 2013. FAA AD
3983; or in person at the Docket manufacturing shimming procedure of the 2015–26–02 requires, for certain
Management Facility between 9 a.m. actuator deployment solenoids.
This condition, if not corrected, could airplanes, identification of the part
and 5 p.m., Monday through Friday, number, serial number, and standard of
possibly result in reduced control of the
except Federal holidays. The AD docket the RAT pump, RAT module, RAT
aeroplane, particularly if occurring following
contains this proposed AD, the a total engine flame out, or during a total loss actuator, and RAT lower gearbox
regulatory evaluation, any comments of normal electrical power generation. assembly; and corrective actions if
asabaliauskas on DSK5VPTVN1PROD with PROPOSALS
received, and other information. The Prompted by this unsafe condition, Airbus necessary. For certain other airplanes,
street address for the Docket Operations issued Service Bulletin (SB) A330–29–3126, AD 2015–26–02 requires re-
office (telephone 800–647–5527) is in SB A340–29–4097 and SB A340–29–5025, identification or replacement of the RAT
the ADDRESSES section. Comments will providing instructions to identify the
manufacturer, part number (P/N) and serial module.
be available in the AD docket shortly
number (s/n) of the RAT actuator, and to Related Service Information Under
after receipt.
modify the shimming procedure for the 1 CFR Part 51
FOR FURTHER INFORMATION CONTACT: affected RAT actuator.
Vladimir Ulyanov, Aerospace Engineer, For the reasons described above, this Airbus has issued the following
International Branch, ANM–116, [EASA] AD requires identification of the service information, which describes
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![Federal Register / Vol. 81, No. 40 / Tuesday, March 1, 2016 / Proposed Rules 10547
procedures for identifying the supplier, Aviation Programs,’’ describes in more (a) Comments Due Date
part number, and serial number of the detail the scope of the Agency’s We must receive comments by April 15,
installed RAT actuator; modifying the authority. 2016.
RAT; and re-identifying the RAT We are issuing this rulemaking under
(b) Affected ADs
actuator and RAT. the authority described in ‘‘Subtitle VII,
• Service Bulletin A330–29–3126, Part A, Subpart III, Section 44701: This AD affects AD 2012–21–19,
Amendment 39–17235 (77 FR 65812, October
dated June 12, 2014. General requirements.’’ Under that
31, 2012); AD 2012–21–20, Amendment 39–
• Service Bulletin A340–29–4097, section, Congress charges the FAA with 17236 (77 FR 65799, October 31, 2012); and
dated June 12, 2014. promoting safe flight of civil aircraft in AD 2015–26–02, Amendment 39–18350 (80
• Service Bulletin A340–29–5025, air commerce by prescribing regulations FR 81174, December 29, 2015).
dated June 16, 2014. for practices, methods, and procedures
Hamilton Sundstrand has issued the Administrator finds necessary for (c) Applicability
Service Bulletins ERPS06M–29–21, safety in air commerce. This regulation This AD applies to the airplanes identified
dated May 27, 2014; and ERPS33T–29– is within the scope of that authority in paragraphs (c)(1) through (c)(7) of this AD,
7, dated June 6, 2014. This service because it addresses an unsafe condition certificated in any category.
information describes procedures for (1) Airbus Model A330–223F and –243F
that is likely to exist or develop on airplanes, all manufacturer serial numbers;
identifying the affected RAT actuator products identified in this rulemaking except those on which Airbus Modification
and RAT part numbers and serial action. 204067 has been embodied in production.
numbers, modifying affected actuators, (2) Airbus Model A330–201, –202, –203,
and re-identifying affected RAT Regulatory Findings
–223, and –243 airplanes, all manufacturer
actuators and RATs. We determined that this proposed AD serial numbers; except those on which
This service information is reasonably would not have federalism implications Airbus Modification 204067 has been
available because the interested parties under Executive Order 13132. This embodied in production.
have access to it through their normal proposed AD would not have a (3) Airbus Model A330–301, –302, –303,
course of business or by the means substantial direct effect on the States, on –321, –322, –323,- 341, –342, and –343
identified in the ADDRESSES section. airplanes, all manufacturer serial numbers;
the relationship between the national
except those on which Airbus Modification
FAA’s Determination and Requirements Government and the States, or on the 204067 has been embodied in production.
of This Proposed AD distribution of power and (4) Airbus Model A340–211, –212, and
responsibilities among the various –213, airplanes, all manufacturer serial
This product has been approved by levels of government. numbers.
the aviation authority of another For the reasons discussed above, I (5) Airbus Model A340–311, –312, and
country, and is approved for operation certify this proposed regulation: –313 airplanes, all manufacturer serial
in the United States. Pursuant to our 1. Is not a ‘‘significant regulatory numbers.
bilateral agreement with the State of action’’ under Executive Order 12866; (6) Airbus Model A340–541 airplanes, all
Design Authority, we have been notified 2. Is not a ‘‘significant rule’’ under the manufacturer serial numbers.
of the unsafe condition described in the (7) Airbus Model A340–642 airplanes, all
DOT Regulatory Policies and Procedures
manufacturer serial numbers.
MCAI and service information (44 FR 11034, February 26, 1979);
referenced above. We are proposing this 3. Will not affect intrastate aviation in (d) Subject
AD because we evaluated all pertinent Alaska; and Air Transport Association (ATA) of
information and determined an unsafe 4. Will not have a significant America Code 29, Hydraulic Power.
condition exists and is likely to exist or economic impact, positive or negative,
(e) Reason
develop on other products of these same on a substantial number of small entities
type designs. under the criteria of the Regulatory This AD was prompted by a report
indicating that, during an operational test of
Flexibility Act.
Costs of Compliance a ram air turbine (RAT), the RAT did not
List of Subjects in 14 CFR Part 39 deploy in automatic mode. We are issuing
We estimate that this proposed AD this AD to prevent non-deployment of the
affects 84 airplanes of U.S. registry. Air transportation, Aircraft, Aviation RAT, which, if preceded by a total engine
We also estimate that it would take safety, Incorporation by reference, flame-out, or during a total loss of normal
about 1 work-hour per product to Safety. electrical power generation, could result in
comply with the basic requirements of reduced control of the airplane.
this proposed AD. The average labor The Proposed Amendment
(f) Compliance
rate is $85 per work-hour. Based on Accordingly, under the authority
these figures, we estimate the cost of delegated to me by the Administrator, Comply with this AD within the
the FAA proposes to amend 14 CFR part compliance times specified, unless already
this proposed AD on U.S. operators to
done.
be $7,140, or $85 per product. 39 as follows:
In addition, we estimate that any (g) Identification and Replacement for
necessary follow-on actions would take PART 39—AIRWORTHINESS Certain Airbus Model A330, and A340–200
about 14 work-hours and require parts DIRECTIVES and –300 Airplanes
costing $427,301, for a cost of $428,491 For Airbus Model A330–200 Freighter
per product. We have no way of ■ 1. The authority citation for part 39 series airplanes, Model A330–200 and –300
asabaliauskas on DSK5VPTVN1PROD with PROPOSALS
determining the number of aircraft that continues to read as follows: series airplanes, and Model A340–200 and
might need actions. Authority: 49 U.S.C. 106(g), 40113, 44701. –300 series airplanes: Within 30 months after
the effective date of this AD, identify the
Authority for This Rulemaking § 39.13 [Amended] supplier, part number, and serial number of
■ 2. The FAA amends § 39.13 by adding the installed RAT actuator, in accordance
Title 49 of the United States Code with the Accomplishment Instructions of
specifies the FAA’s authority to issue the following new airworthiness
Airbus Service Bulletin A330–29–3126,
rules on aviation safety. Subtitle I, directive (AD): dated June 12, 2014; or Airbus Service
section 106, describes the authority of Airbus: Docket No. FAA–2016–3983; Bulletin A340–29–4097, dated June 12, 2014;
the FAA Administrator. ‘‘Subtitle VII: Directorate Identifier 2015–NM–009–AD. as applicable.
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![Federal Register / Vol. 81, No. 40 / Tuesday, March 1, 2016 / Proposed Rules 10549
(2) Contacting the Manufacturer: For any DEPARTMENT OF TRANSPORTATION airworthiness.A330-A340@airbus.com;
requirement in this AD to obtain corrective Internet http://www.airbus.com. You
actions from a manufacturer, the action must Federal Aviation Administration may view this referenced service
be accomplished using a method approved information at the FAA, Transport
by the Manager, International Branch, ANM– 14 CFR Part 39 Airplane Directorate, 1601 Lind Avenue
116, Transport Airplane Directorate, FAA; or SW., Renton, WA. For information on
[Docket No. FAA–2016–3988; Directorate
the European Aviation Safety Agency the availability of this material at the
Identifier 2015–NM–130–AD]
(EASA); or Airbus’s EASA Design FAA, call 425–227–1221.
Organization Approval (DOA). If approved by RIN 2120–AA64
the DOA, the approval must include the Examining the AD Docket
DOA-authorized signature. Airworthiness Directives; Airbus You may examine the AD docket on
(3) Required for Compliance (RC): If any Airplanes the Internet at http://
Airbus service information contains AGENCY: Federal Aviation www.regulations.gov by searching for
procedures or tests that are identified as RC,
Administration (FAA), DOT. and locating Docket No. FAA–2016–
those procedures and tests must be done to 3988; or in person at the Docket
comply with this AD; any procedures or tests ACTION: Notice of proposed rulemaking
Management Facility between 9 a.m.
that are not identified as RC are (NPRM). and 5 p.m., Monday through Friday,
recommended. Those procedures and tests SUMMARY: We propose to adopt a new except Federal holidays. The AD docket
that are not identified as RC may be deviated airworthiness directive (AD) for certain contains this proposed AD, the
from using accepted methods in accordance regulatory evaluation, any comments
Airbus Model A330–200, –200
with the operator’s maintenance or received, and other information. The
Freighter, and –300 series airplanes; and
inspection program without obtaining street address for the Docket Operations
all Airbus Model A340–200, –300, –500,
approval of an AMOC, provided the office (telephone 800–647–5527) is in
and –600 series airplanes. This
procedures and tests identified as RC can be the ADDRESSES section. Comments will
proposed AD was prompted by reports
done and the airplane can be put back in an be available in the AD docket shortly
of chafing of the feeder cable at the
airworthy condition. Any substitutions or after receipt.
changes to procedures or tests identified as
pylon-wing junction due to vibration;
one report revealed that the cable loom FOR FURTHER INFORMATION CONTACT:
RC require approval of an AMOC. Vladimir Ulyanov, Aerospace Engineer,
plastic support bracket of the G-route
(l) Related Information was broken due to vibration; and International Branch, ANM–116,
another report revealed wire chafing Transport Airplane Directorate, FAA,
(1) Refer to Mandatory Continuing
Airworthiness Information (MCAI) EASA due to clamp damage. This proposed 1601 Lind Avenue SW., Renton, WA
Airworthiness Directive 2015–0008, dated AD would require modifying the cable 98057–3356; telephone 425–227–1138;
January 15, 2015, for related information. loom support bracket of the G-route of fax 425–227–1149.
This MCAI may be found in the AD docket the inboard pylons at the pylon-wing SUPPLEMENTARY INFORMATION:
on the Internet at http://www.regulations.gov junction. We are proposing this AD to Comments Invited
by searching for and locating Docket No. prevent chafing of the wiring in the
FAA–2016–3983. pylon-wing area, which could result in We invite you to send any written
(2) For Airbus service information an electrical short circuit near a relevant data, views, or arguments about
identified in this proposed AD, contact flammable fluid vapor zone, and this proposed AD. Send your comments
Airbus SAS, Airworthiness Office—EAL, 1 consequent fire or fuel tank explosion. to an address listed under the
ADDRESSES section. Include ‘‘Docket No.
Rond Point Maurice Bellonte, 31707 Blagnac DATES: We must receive comments on
Cedex, France; telephone +33 5 61 93 36 96; FAA–2016–3988; Directorate Identifier
this proposed AD by April 15, 2016. 2015–NM–130–AD’’ at the beginning of
fax +33 5 61 93 45 80; email
ADDRESSES: You may send comments, your comments. We specifically invite
airworthiness.A330-A340@airbus.com;
using the procedures found in 14 CFR comments on the overall regulatory,
Internet http://www.airbus.com. For
11.43 and 11.45, by any of the following economic, environmental, and energy
Hamilton Sundstrand service information
methods: aspects of this proposed AD. We will
identified in this AD, contact Hamilton
• Federal eRulemaking Portal: Go to consider all comments received by the
Sundstrand, Technical Publications, Mail
http://www.regulations.gov. Follow the closing date and may amend this
Stop 302–9, 4747 Harrison Avenue, P.O. Box
7002, Rockford, IL 61125–7002; telephone
instructions for submitting comments. proposed AD based on those comments.
860–654–3575; fax 860–998–4564; email
• Fax: 202–493–2251. We will post all comments we
tech.solutions@hs.utc.com; Internet http://
• Mail: U.S. Department of receive, without change, to http://
www.hamiltonsundstrand.com. You may
Transportation, Docket Operations, M– www.regulations.gov, including any
view this referenced service information at
30, West Building Ground Floor, Room personal information you provide. We
the FAA, Transport Airplane Directorate, W12–140, 1200 New Jersey Avenue SE., will also post a report summarizing each
1601 Lind Avenue SW., Renton, WA. For Washington, DC 20590. substantive verbal contact we receive
information on the availability of this • Hand Delivery: U.S. Department of about this proposed AD.
material at the FAA, call 425–227–1221. Transportation, Docket Operations, M–
30, West Building Ground Floor, Room Discussion
Issued in Renton, Washington, on February W12–140, 1200 New Jersey Avenue SE., The European Aviation Safety Agency
asabaliauskas on DSK5VPTVN1PROD with PROPOSALS
19, 2016. Washington, DC, between 9 a.m. and 5 (EASA), which is the Technical Agent
Dorr M. Anderson, p.m., Monday through Friday, except for the Member States of the European
Acting Manager, Transport Airplane Federal holidays. Union, has issued EASA Airworthiness
Directorate, Aircraft Certification Service. For service information identified in Directive 2015–0142, dated July 17,
[FR Doc. 2016–04288 Filed 2–29–16; 8:45 am] this NPRM, contact Airbus SAS, 2015 (referred to after this as the
BILLING CODE 4910–13–P
Airworthiness Office—EAL, 1 Rond Mandatory Continuing Airworthiness
Point Maurice Bellonte, 31707 Blagnac Information, or ‘‘the MCAI’’), to correct
Cedex, France; telephone +33 5 61 93 36 an unsafe condition for certain Airbus
96; fax +33 5 61 93 45 80; email Model A330–200, –200 Freighter, and
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Document Created: 2018-02-02 15:00:07
Document Modified: 2018-02-02 15:00:07
| 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 | Proposed Rules | |
| Action | Notice of proposed rulemaking (NPRM). | |
| Dates | We must receive comments on this proposed AD by April 15, 2016. | |
| Contact | Vladimir Ulyanov, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356; telephone 425-227-1138; fax 425-227-1149. | |
| FR Citation | 81 FR 10545 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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