Airworthiness Directives; Airbus Airplanes, 22219-22221 [2018-09980]

Download as PDF Federal Register / Vol. 83, No. 93 / Monday, May 14, 2018 / Proposed Rules amozie on DSK3GDR082PROD with PROPOSALS (i) The minimum en route speed scheduled in non-icing conditions does not provide the maneuvering capability specified in § 25.143(h) for the en route configuration, or 7. In lieu of § 25.125(b)(2)(ii)(B) and § 25.125(b)(2)(ii)(C), the following applies: § 25.125 Landing. (b) In determining the distance in (a): * * * * * 2. A stabilized approach, with a calibrated airspeed of not less than VREF, must be maintained down to the 50-foot height. * * * * * (ii) In icing conditions, VREF may not be less than: (A) The speed determined in subparagraph (b)(2)(i) of this section; (B) A speed that provides the maneuvering capability specified in § 25.143(h) with the ‘‘Landing Ice’’ accretion defined in appendix C to part 25. 8. In lieu of § 25.143(j), the following applies: § 25.143 General. (j) For flight in icing conditions— before the ice protection system has been activated and is performing its intended function—the following requirements apply: (1) If activating the ice protection system depends on the pilot seeing a specified ice accretion on a reference surface (not just the first indication of icing), the requirements of § 25.143 apply with the ice accretion defined in part II(e) of appendix C to part 25. (2) For other means of activating the ice protection system, it must be demonstrated in flight with the ice accretion defined in part II(e) of appendix C to part 25 that: (i) The airplane is controllable in a pull-up maneuver up to 1.5 g load factor or lower if limited by AOA protection; and (ii) There is no reversal of pitch control force during a pushover maneuver down to 0.5 g load factor. 9. In lieu of § 25.207, ‘‘Stall warning,’’ to read as the requirements defined in Part I of these special conditions. Issued in Renton, Washington, on May 8, 2018. Victor Wicklund, Manager, Transport Standards Branch, Policy and Innovation Division, Aircraft Certification Service. [FR Doc. 2018–10168 Filed 5–11–18; 8:45 am] BILLING CODE 4910–13–P VerDate Sep<11>2014 16:11 May 11, 2018 Jkt 244001 DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2018–0364; Product Identifier 2017–NM–154–AD] RIN 2120–AA64 Airworthiness Directives; Airbus Airplanes Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). AGENCY: We propose to adopt a new airworthiness directive (AD) for all Airbus Model A300 and A310 series airplanes; Model A300 B4–600, B4– 600R, and F4–600R series airplanes, and Model A300 C4–605R Variant F airplanes (collectively called Model A300–600 series airplanes). This proposed AD was prompted by a determination that new or more restrictive maintenance requirements and airworthiness limitations are necessary. This proposed AD would require revising the maintenance or inspection program, as applicable, to incorporate new or more restrictive maintenance requirements and airworthiness limitations. We are proposing this AD to address the unsafe condition on these products. DATES: We must receive comments on this proposed AD by June 28, 2018. 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 https://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: Deliver to Mail address above between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. For service information identified in this NPRM, contact Airbus SAS, Airworthiness Office—EAW, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France; telephone +33 5 61 93 36 96; fax +33 5 61 93 44 51; email account.airworth-eas@airbus.com; internet https://www.airbus.com. You may view this service information at the FAA, Transport Standards Branch, 2200 South 216th Street, Des Moines, WA. For information on the availability of SUMMARY: PO 00000 Frm 00007 Fmt 4702 Sfmt 4702 22219 this material at the FAA, call 206–231– 3195. Examining the AD Docket You may examine the AD docket on the internet at https:// www.regulations.gov by searching for and locating Docket No. FAA–2018– 0364; 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 NPRM, 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: Dan Rodina, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax 206–231–3225. SUPPLEMENTARY INFORMATION: Comments Invited We invite you to send any written relevant data, views, or arguments about this proposal. Send your comments to an address listed under the ADDRESSES section. Include ‘‘Docket No. FAA– 2018–0364; Product Identifier 2017– NM–154–AD’’ at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of this NPRM. We will consider all comments received by the closing date and may amend this NPRM based on those comments. We will post all comments we receive, without change, to https:// www.regulations.gov, including any personal information you provide. We will also post a report summarizing each substantive verbal contact we receive about this NPRM. 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 2017–0204, dated October 12, 2017 (referred to after this as the Mandatory Continuing Airworthiness Information, or ‘‘the MCAI’’), to correct an unsafe condition for all Airbus Model A300 and A310 series airplanes, and Model A300 B4–600, B4–600R, and F4–600R series airplanes, and Model A300 C4–605R Variant F airplanes (collectively called Model A300–600 series airplanes). The MCAI states: The airworthiness limitations for the Airbus A300, A310, A300–600 and A300– E:\FR\FM\14MYP1.SGM 14MYP1 22220 Federal Register / Vol. 83, No. 93 / Monday, May 14, 2018 / Proposed Rules 600ST family aeroplanes, which are approved by EASA, are currently defined and published in the Airbus A300, A310 and A300–600 Airworthiness Limitations Section (ALS) documents. The Safe Life Airworthiness Limitation Items are specified in the A300, A310 and A300–600 (including the A300–600ST) ALS Part 1 documents. These instructions have been identified as mandatory for continuing airworthiness. Failure to accomplish these instructions could result in an unsafe condition. EASA previously issued AD 2013–0248 [which corresponds to FAA AD 2015–22–05, Amendment 39–18310 (80 FR 69846, November 12, 2015) (‘‘AD 2015–22–05’’)] to require the implementation of the instructions and airworthiness limitations as specified in Airbus A300, A310 and A300– 600 ALS Part 1 documents at Revision 01. Since that [EASA] AD was issued, improvement of safe life component selection and life extension campaigns resulted in life limitations changes, among others new or more restrictive life limitations, approved by EASA. Consequently, Airbus published Revision 02 of the A300, A310 and A300–600 ALS Part 1, compiling all ALS Part 1, compiling all ALS Part 1 changes approved since previous Revision 01. For the reason described above, this [EASA] AD retains the requirements of EASA AD 2013–0248, which is superseded, and requires accomplishment of the actions specified in A300 ALS Part 1 Revision 02, A310 ALS Part 1 Revision 02 and A300–600 ALS Part 1 Revision 02. amozie on DSK3GDR082PROD with PROPOSALS This NPRM would require revising the maintenance or inspection program to incorporate certain maintenance requirements and airworthiness limitations. The unsafe condition is fatigue damage in principal structural elements, which could result in reduced structural integrity of the airplane. You may examine the MCAI in the AD docket on the internet at https:// www.regulations.gov by searching for and locating Docket No. FAA–2018– 0364. Relationship Between Proposed AD and AD 2015–22–05 This NPRM would not supersede AD 2015–22–05. Rather, we have determined that a stand-alone AD would be more appropriate to address the changes in the MCAI. This NPRM would require revising the maintenance or inspection program, as applicable, to incorporate maintenance requirements and/or airworthiness limitations that are newer or more restrictive than those required by AD 2015–22–05. Accomplishment of the proposed actions would then terminate all requirements of AD 2015–22–05. Related Service Information Under 1 CFR Part 51 Airbus has issued the following service information, which describes VerDate Sep<11>2014 16:11 May 11, 2018 Jkt 244001 procedures for revising the maintenance or inspection program to incorporate new or more restrictive maintenance requirements and airworthiness limitations. These documents are distinct since they apply to different airplane models. • 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 Model A300 Airworthiness Limitations Section (ALS). • 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 Model A300–600 Airworthiness Limitations Section (ALS). • 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 Model A310 Airworthiness Limitations Section (ALS). 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. This proposed AD requires revisions to certain operator maintenance documents to include new actions (e.g., inspections). Compliance with these actions is required by 14 CFR 91.403(c). For airplanes that have been previously modified, altered, or repaired in the areas addressed by this proposed AD, the operator may not be able to accomplish the actions described in the revisions. In this situation, to comply with 14 CFR 91.403(c), the operator PO 00000 Frm 00008 Fmt 4702 Sfmt 4702 must request approval for an alternative method of compliance according to paragraph (j)(1) of this proposed AD. The request should include a description of changes to the required actions that will ensure the continued damage tolerance of the affected structure. Costs of Compliance We estimate that this proposed AD affects 132 airplanes of U.S. registry. We estimate the following costs to comply with this proposed AD: We have determined that revising the maintenance or inspection program takes an average of 90 work-hours per operator, although we recognize that this number may vary from operator to operator. In the past, we have estimated that this action takes 1 work-hour per airplane. Since operators incorporate maintenance or inspection program changes for their affected fleet(s), we have determined that a per-operator estimate is more accurate than a perairplane estimate. Therefore, we estimate the total cost per operator to be $7,650 (90 work-hours × $85 per workhour). 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. This proposed AD is issued in accordance with authority delegated by the Executive Director, Aircraft Certification Service, as authorized by FAA Order 8000.51C. In accordance with that order, issuance of ADs is normally a function of the Compliance and Airworthiness Division, but during this transition period, the Executive Director has delegated the authority to issue ADs applicable to transport category airplanes to the Director of the System Oversight Division. E:\FR\FM\14MYP1.SGM 14MYP1 Federal Register / Vol. 83, No. 93 / Monday, May 14, 2018 / Proposed Rules 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. –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. We must receive comments by June 28, 2018. (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). (b) Affected ADs (h) No Alternative Actions or Intervals This AD affects AD 2015–22–05, Amendment 39–18310 (80 FR 69846, November 12, 2015) (‘‘AD 2015–22–05’’). 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. 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 1. The authority citation for part 39 continues to read as follows: ■ Authority: 49 U.S.C. 106(g), 40113, 44701. § 39.13 [Amended] 2. The FAA amends § 39.13 by adding the following new airworthiness directive (AD): ■ Airbus: Docket No. FAA–2018–0364; Product Identifier 2017–NM–154–AD. amozie on DSK3GDR082PROD with PROPOSALS (a) Comments Due Date (c) Applicability This AD applies to Airbus 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, VerDate Sep<11>2014 16:11 May 11, 2018 Jkt 244001 (i) Terminating Action Accomplishing the actions required by paragraph (g) of this AD terminates all requirements of AD 2015–22–05. PO 00000 Frm 00009 Fmt 4702 Sfmt 4702 22221 (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-AMOCREQUESTS@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’s EASA Design Organization Approval (DOA). If approved by the DOA, the approval must include the DOAauthorized signature. (k) Related Information (1) Refer to Mandatory Continuing Airworthiness Information (MCAI) EASA Airworthiness Directive 2017–0204, dated October 12, 2017, for related information. This MCAI may be found in the AD docket on the internet at https://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. (3) For service information identified in this AD, contact Airbus SAS, Airworthiness Office—EAW, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France; telephone +33 5 61 93 36 96; fax +33 5 61 93 44 51; email account.airworth-eas@ airbus.com; internet https://www.airbus.com. 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. Issued in Des Moines, Washington, on April 27, 2018. Michael Kaszycki, Acting Director, System Oversight Division, Aircraft Certification Service. [FR Doc. 2018–09980 Filed 5–11–18; 8:45 am] BILLING CODE 4910–13–P E:\FR\FM\14MYP1.SGM 14MYP1

Agencies

[Federal Register Volume 83, Number 93 (Monday, May 14, 2018)]
[Proposed Rules]
[Pages 22219-22221]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2018-09980]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2018-0364; Product Identifier 2017-NM-154-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 all 
Airbus Model A300 and A310 series airplanes; Model A300 B4-600, B4-
600R, and F4-600R series airplanes, and Model A300 C4-605R Variant F 
airplanes (collectively called Model A300-600 series airplanes). This 
proposed AD was prompted by a determination that new or more 
restrictive maintenance requirements and airworthiness limitations are 
necessary. This proposed AD would require revising the maintenance or 
inspection program, as applicable, to incorporate new or more 
restrictive maintenance requirements and airworthiness limitations. We 
are proposing this AD to address the unsafe condition on these 
products.

DATES: We must receive comments on this proposed AD by June 28, 2018.

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 https://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: Deliver to Mail address above between 9 
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
    For service information identified in this NPRM, contact Airbus 
SAS, Airworthiness Office--EAW, 1 Rond Point Maurice Bellonte, 31707 
Blagnac Cedex, France; telephone +33 5 61 93 36 96; fax +33 5 61 93 44 
51; email [email protected]; internet https://www.airbus.com. You may view this service information at the FAA, 
Transport Standards Branch, 2200 South 216th Street, Des Moines, WA. 
For information on the availability of this material at the FAA, call 
206-231-3195.

Examining the AD Docket

    You may examine the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2018-
0364; 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 NPRM, 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: Dan Rodina, Aerospace Engineer, 
International Section, Transport Standards Branch, FAA, 2200 South 
216th St., Des Moines, WA 98198; telephone and fax 206-231-3225.

SUPPLEMENTARY INFORMATION:

Comments Invited

    We invite you to send any written relevant data, views, or 
arguments about this proposal. Send your comments to an address listed 
under the ADDRESSES section. Include ``Docket No. FAA-2018-0364; 
Product Identifier 2017-NM-154-AD'' at the beginning of your comments. 
We specifically invite comments on the overall regulatory, economic, 
environmental, and energy aspects of this NPRM. We will consider all 
comments received by the closing date and may amend this NPRM based on 
those comments.
    We will post all comments we receive, without change, to https://www.regulations.gov, including any personal information you provide. We 
will also post a report summarizing each substantive verbal contact we 
receive about this NPRM.

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 2017-0204, dated October 12, 2017 (referred to 
after this as the Mandatory Continuing Airworthiness Information, or 
``the MCAI''), to correct an unsafe condition for all Airbus Model A300 
and A310 series airplanes, and Model A300 B4-600, B4-600R, and F4-600R 
series airplanes, and Model A300 C4-605R Variant F airplanes 
(collectively called Model A300-600 series airplanes). The MCAI states:

    The airworthiness limitations for the Airbus A300, A310, A300-
600 and A300-

[[Page 22220]]

600ST family aeroplanes, which are approved by EASA, are currently 
defined and published in the Airbus A300, A310 and A300-600 
Airworthiness Limitations Section (ALS) documents. The Safe Life 
Airworthiness Limitation Items are specified in the A300, A310 and 
A300-600 (including the A300-600ST) ALS Part 1 documents. These 
instructions have been identified as mandatory for continuing 
airworthiness.
    Failure to accomplish these instructions could result in an 
unsafe condition.
    EASA previously issued AD 2013-0248 [which corresponds to FAA AD 
2015-22-05, Amendment 39-18310 (80 FR 69846, November 12, 2015) 
(``AD 2015-22-05'')] to require the implementation of the 
instructions and airworthiness limitations as specified in Airbus 
A300, A310 and A300-600 ALS Part 1 documents at Revision 01.
    Since that [EASA] AD was issued, improvement of safe life 
component selection and life extension campaigns resulted in life 
limitations changes, among others new or more restrictive life 
limitations, approved by EASA. Consequently, Airbus published 
Revision 02 of the A300, A310 and A300-600 ALS Part 1, compiling all 
ALS Part 1, compiling all ALS Part 1 changes approved since previous 
Revision 01.
    For the reason described above, this [EASA] AD retains the 
requirements of EASA AD 2013-0248, which is superseded, and requires 
accomplishment of the actions specified in A300 ALS Part 1 Revision 
02, A310 ALS Part 1 Revision 02 and A300-600 ALS Part 1 Revision 02.

    This NPRM would require revising the maintenance or inspection 
program to incorporate certain maintenance requirements and 
airworthiness limitations. The unsafe condition is fatigue damage in 
principal structural elements, which could result in reduced structural 
integrity of the airplane. You may examine the MCAI in the AD docket on 
the internet at https://www.regulations.gov by searching for and 
locating Docket No. FAA-2018-0364.

Relationship Between Proposed AD and AD 2015-22-05

    This NPRM would not supersede AD 2015-22-05. Rather, we have 
determined that a stand-alone AD would be more appropriate to address 
the changes in the MCAI. This NPRM would require revising the 
maintenance or inspection program, as applicable, to incorporate 
maintenance requirements and/or airworthiness limitations that are 
newer or more restrictive than those required by AD 2015-22-05. 
Accomplishment of the proposed actions would then terminate all 
requirements of AD 2015-22-05.

Related Service Information Under 1 CFR Part 51

    Airbus has issued the following service information, which 
describes procedures for revising the maintenance or inspection program 
to incorporate new or more restrictive maintenance requirements and 
airworthiness limitations. These documents are distinct since they 
apply to different airplane models.
     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 Model A300 Airworthiness Limitations Section 
(ALS).
     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 Model A300-600 Airworthiness Limitations Section (ALS).
     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 Model A310 Airworthiness Limitations Section 
(ALS).
    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.
    This proposed AD requires revisions to certain operator maintenance 
documents to include new actions (e.g., inspections). Compliance with 
these actions is required by 14 CFR 91.403(c). For airplanes that have 
been previously modified, altered, or repaired in the areas addressed 
by this proposed AD, the operator may not be able to accomplish the 
actions described in the revisions. In this situation, to comply with 
14 CFR 91.403(c), the operator must request approval for an alternative 
method of compliance according to paragraph (j)(1) of this proposed AD. 
The request should include a description of changes to the required 
actions that will ensure the continued damage tolerance of the affected 
structure.

Costs of Compliance

    We estimate that this proposed AD affects 132 airplanes of U.S. 
registry.
    We estimate the following costs to comply with this proposed AD:
    We have determined that revising the maintenance or inspection 
program takes an average of 90 work-hours per operator, although we 
recognize that this number may vary from operator to operator. In the 
past, we have estimated that this action takes 1 work-hour per 
airplane. Since operators incorporate maintenance or inspection program 
changes for their affected fleet(s), we have determined that a per-
operator estimate is more accurate than a per-airplane estimate. 
Therefore, we estimate the total cost per operator to be $7,650 (90 
work-hours x $85 per work-hour).

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.
    This proposed AD is issued in accordance with authority delegated 
by the Executive Director, Aircraft Certification Service, as 
authorized by FAA Order 8000.51C. In accordance with that order, 
issuance of ADs is normally a function of the Compliance and 
Airworthiness Division, but during this transition period, the 
Executive Director has delegated the authority to issue ADs applicable 
to transport category airplanes to the Director of the System Oversight 
Division.

[[Page 22221]]

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-2018-0364; Product Identifier 2017-NM-154-AD.

(a) Comments Due Date

    We must receive comments by June 28, 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 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.

(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: [email protected]. Before using any 
approved AMOC, notify your appropriate principal inspector, or 
lacking a principal inspector, the manager of the local flight 
standards district office/certificate holding district office.
    (2) Contacting the Manufacturer: For any requirement in this AD 
to obtain corrective actions from a manufacturer, the action must be 
accomplished using a method approved by the Manager, International 
Section, Transport Standards Branch, 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.

(k) Related Information

    (1) Refer to Mandatory Continuing Airworthiness Information 
(MCAI) EASA Airworthiness Directive 2017-0204, dated October 12, 
2017, for related information. This MCAI may be found in the AD 
docket on the internet at https://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.
    (3) For service information identified in this AD, contact 
Airbus SAS, Airworthiness Office--EAW, 1 Rond Point Maurice 
Bellonte, 31707 Blagnac Cedex, France; telephone +33 5 61 93 36 96; 
fax +33 5 61 93 44 51; email [email protected]; 
internet https://www.airbus.com. 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.

    Issued in Des Moines, Washington, on April 27, 2018.
Michael Kaszycki,
Acting Director, System Oversight Division, Aircraft Certification 
Service.
[FR Doc. 2018-09980 Filed 5-11-18; 8:45 am]
 BILLING CODE 4910-13-P

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