2018-18-19: Time limits/maintenance checks

Adoption of the Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: PART 39--AIRWORTHINESS DIRECTIVES 0 1. The authority citation for part 39 continues to read as follows: Authority: 49 U.S.C. 106(g), 40113, 44701. Sec. 39.13 [Amended] 0 2. The FAA amends Sec. 39.13 by adding the following new airworthiness directive (AD): 2018-18-19 Airbus SAS: Amendment 39-19398; Docket No. FAA-2018-0364; Product Identifier 2017-NM-154-AD. (a) Effective Date This AD is effective October 23, 2018. (b) Affected ADs This AD affects AD 2015-22-05, Amendment 39-18310 (80 FR 69846, November 12, 2015) (``AD 2015-22-05''). (c) Applicability This AD applies to Airbus SAS Model A300 B2-1A, B2-1C, B2K-3C, B2-203, B4-2C, B4-103, and B4-203 airplanes; Model A300 B4-601, B4- 603, B4-620, and B4-622 airplanes; Model A300 B4-605R and B4-622R airplanes; Model A300 F4-605R and F4-622R airplanes; Model A300 C4- 605R Variant F airplanes; and Model A310-203, -204, -221, -222, - 304, -322, -324, and -325 airplanes; certificated in any category, all manufacturer serial numbers. (d) Subject Air Transport Association (ATA) of America Code 05, Time limits/ maintenance checks. (e) Reason This AD was prompted by a determination that new or more restrictive maintenance requirements and airworthiness limitations are necessary. We are issuing this AD to prevent fatigue damage in principal structural elements, which could result in reduced structural integrity of the airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Maintenance or Inspection Program Revision Within 90 days after the effective date of this AD: Revise the maintenance or inspection program, as applicable, to incorporate the applicable information specified in paragraph (g)(1), (g)(2), or (g)(3) of this AD, as applicable. The initial compliance times for accomplishing the tasks is at the applicable times specified in the applicable information specified in paragraph (g)(1), (g)(2), or (g)(3) of this AD, or within 90 days after the effective date of this AD, whichever occurs later. (1) For Model A300 series airplanes: Section 4, ``Life Limits (LL)/Demonstrated Fatigue Lives (DF),'' of Part 1, ``Safe Life Airworthiness Limitation Items (SL--ALI),'' Revision 02, dated August 28, 2017, of the Airbus A300 Airworthiness Limitations Section (ALS). (2) For Model A300 B4-600, B4-600R, and F4-600R series airplanes, and Model A300 C4-605R Variant F airplanes (collectively called Model A300-600 series airplanes): Section 4, ``Life Limits (LL)/Demonstrated Fatigue Lives (DF),'' of Part 1, ``Safe Life Airworthiness Limitation Items (SL--ALI),'' Revision 02, dated August 28, 2017, of the Airbus A300-600 Airworthiness Limitations Section (ALS). (3) For Model A310 series airplanes: Section 4,``Life Limits (LL)/Demonstrated Fatigue Lives (DF),'' of Part 1, ``Safe Life Airworthiness Limitation Items (SL--ALI),'' Revision 02, dated August 28, 2017, of the Airbus A310 Airworthiness Limitations Section (ALS). (h) No Alternative Actions or Intervals After accomplishment of the revision required by paragraph (g) of this AD, no alternative actions (e.g., inspections) or intervals may be used unless the actions or intervals are approved as an alternative method of compliance (AMOC) in accordance with the procedures specified in paragraph (j)(1) of this AD. (i) Terminating Action Accomplishing the actions required by paragraph (g) of this AD terminates all requirements of AD 2015-22-05. [[Page 47059]] (j) Other FAA AD Provisions The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, International Section, Transport Standards Branch, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the International Section, send it to the attention of the person identified in paragraph (k)(2) of this AD. Information may be emailed to: 9-ANM-116-AMOC-REQUESTS@faa.gov. Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/certificate holding district office. (2) Contacting the Manufacturer: For any requirement in this AD to obtain corrective actions from a manufacturer, the action must be accomplished using a method approved by the Manager, International Section, Transport Standards Branch, FAA; or the European Aviation Safety Agency (EASA); or Airbus SAS's EASA Design Organization Approval (DOA). If approved by the DOA, the approval must include the DOA-authorized signature. (k) Related Information (1) Refer to Mandatory Continuing Airworthiness Information (MCAI) EASA AD 2017-0204, dated October 12, 2017, for related information. This MCAI may be found in the AD docket on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2018-0364. (2) For more information about this AD, contact Dan Rodina, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax 206-231-3225. (l) 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) Part 1, ``Safe Life Airworthiness Limitation Items (SL-- ALI),'' Revision 02, dated August 28, 2017, of the Airbus Model A300 Airworthiness Limitations Section (ALS). (ii) Part 1, ``Safe Life Airworthiness Limitation Items (SL-- ALI),'' Revision 02, dated August 28, 2017, of the Airbus Model A300-600 Airworthiness Limitations Section (ALS). (iii) Part 1, ``Safe Life Airworthiness Limitation Items (SL-- ALI),'' Revision 02, dated August 28, 2017, of the Airbus Model A310 Airworthiness Limitations Section (ALS). (3) For service information identified in this AD, contact Airbus SAS, Airworthiness Office--EAW, Rond-Point Emile Dewoitine No: 2, 31700 Blagnac Cedex, France; telephone +33 5 61 93 36 96; fax +33 5 61 93 44 51; email account.airworth-eas@airbus.com; internet http://www.airbus.com. (4) You may view this service information at the FAA, Transport Standards Branch, 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 206-231-3195. (5) You may view this service information that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202-741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.