2019-16-08: Flight controls

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 removing Airworthiness Directive (AD) 2018-22-13, Amendment 39-19486 (83 FR 55617, November 7, 2018), and adding the following new AD: 2019-16-08 Airbus SAS: Amendment 39-19711; Docket No. FAA-2019-0193; Product Identifier 2018-NM-159-AD. (a) Effective Date This AD is effective November 5, 2019. (b) Affected ADs This AD replaces AD 2018-22-13, Amendment 39-19486 (83 FR 55617, November 7, 2018) (``AD 2018-22-13''). (c) Applicability This AD applies to Airbus SAS Model A350-941 and -1041 airplanes, certificated in any category, except those on which Airbus modifications 113758 and113759 have been embodied in production. (d) Subject Air Transport Association (ATA) of America Code 27, Flight controls. (e) Reason This AD was prompted by a technical issue detected on the inboard aileron electrohydrostatic actuators that caused potential erroneous monitoring of those actuators. The FAA is issuing this AD to address possible in-flight loss of inboard aileron control, consequent increased fuel consumption due to the resulting drag, and reduced control or performance of the airplane if one engine is also inoperative. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Retained Revision of Existing Airplane Flight Manual (AFM), With Revised Compliance Language and Corrected Temporary Revision (TR) Date This paragraph restates the requirements of paragraph (g) of AD 2018-22-13, with revised compliance language and a corrected TR date. At the applicable time specified in paragraph(g)(1) or (2) of this AD, revise the Abnormal Procedures section of the existing AFM to include the information in Airbus A350 TR 113, Issue 1, dated August 17, 2018, which introduces updated procedures related to inboard aileron fault operations. This may be done by inserting a copy of Airbus A350 TR 113, Issue 1, dated August 17, 2018, into the existing AFM. When Airbus A350 TR 113, Issue 1, dated August 17, 2018, has been included in general revisions of the existing AFM, the general revisions may be inserted into the existing AFM, provided the relevant information in the general revisions is identical to that in Airbus A350 TR 113, Issue 1, dated August 17, 2018, and the TR may be removed. Operate the airplane according to the procedures in Airbus A350 TR 113, Issue 1, dated August 17, 2018. In case any discrepancy is identified between procedures displayed on the electronic centralized aircraft monitoring (ECAM) and procedures stated in the applicable existing AFM, the existing AFM procedures prevail. (1) For airplanes modified by Airbus modifications 113758 and 113760: Within 30 days after the effective date of this AD. (2) For airplanes not identified in paragraph (g)(1) of this AD: Within 30 days after November 23, 2018 (the effective date of AD 2018-22-13). [[Page 51960]] (h) New Requirement of This AD: Modification Within 6 months after the effective date of this AD, do the actions specified in paragraphs (h)(1) and (2) of this AD. (1) Install the Airbus temporary quick change (ATQC) as specified in paragraph (h)(1)(i) or (ii) of this AD, as applicable. (i) For airplanes with flight warning system (FWS) standard S4/ 2.0: Install ATQC standard V4 for FWS standard S4/2.0, in accordance with the Accomplishment Instructions of Airbus Service Bulletin A350-31-P028, dated September 17, 2018. (ii) For airplanes with FWS standard S5/2.2: Install ATQC standard V4 for FWS standard S5/2.2, in accordance with the Accomplishment Instructions of Airbus Service Bulletin A350-31-P029, dated September 17, 2018. After installation of ATQC standard V4, ATQC standard V5 for FWS standard S5/2.2 may be installed, in accordance with the Accomplishment Instructions of Airbus Service Bulletin A350-31-P032, dated February 28, 2019. (2) Activate ECAM temporary change code No. 27AF, in accordance with the Accomplishment Instructions of Airbus Service Bulletin A350-31-P030, dated September 17, 2018. (i) Other FAA AD Provisions (1) Alternative Methods of Compliance (AMOCs): The Manager, International Section, Transport Standards Branch, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the International Section, send it to the attention of the person identified in paragraph (j)(2) of this AD. Information may be emailed to [email protected]. (i) 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. (ii) AMOCs approved previously for AD 2018-22-13 are approved as AMOCs for the corresponding provisions of this AD. (2) Contacting the Manufacturer: As of the effective date of this AD, for any requirement in this AD to obtain corrective actions from a manufacturer, the action must be accomplished using a method approved by the Manager, International Section, Transport Standards Branch, FAA; or the European Union Aviation Safety Agency (EASA); or Airbus SAS'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 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. (j) Related Information (1) Refer to Mandatory Continuing Airworthiness Information (MCAI) EASA AD 2018-0213R1, dated November 9, 2018, for related information. This MCAI may be found in the AD docket on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2019-0193. (2) For more information about this AD, contact Kathleen Arrigotti, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax 206-231-3218. (k) 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. (3) 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 A350-31-P028, dated September 17, 2018. (ii) Airbus Service Bulletin A350-31-P029, dated September 17, 2018. (iii) Airbus Service Bulletin A350-31-P030, dated September 17, 2018. (iv) Airbus Service Bulletin A350-31-P032, dated February 28, 2019. (v) Airbus A350 Temporary Revision (TR) 113, Issue 1, dated August 17, 2018. (4) For service information identified in this AD, contact Airbus SAS, Airworthiness Office--EAL, Rond-Point Emile Dewoitine No: 2, 31700 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. (5) You may view this service information at the FAA, Transport Standards Branch, 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 206-231-3195. (6) 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, email [email protected], or go to http://www.archives.gov/federal-register/cfr/ibr-locations.html.