- Effective
- April 26, 2021
- Published
- March 22, 2021 · 86 FR 15092–15094
- Issued
- February 23, 2021
- Superseded by
- AD2022-18-01
- Models
- A330-223F, A330-243
- Data sheet
- TCDSA46NM
- Registered aircraft
- 40 matched by model
- Product
- Aircraft · Large airplane
- ATA chapter
- 05 · Time limits and maintenance checks
- Amendment
- 39-21455
- Docket
- FAA-2020-1115
- Issued as
- Final rule
Unofficial copy from the Federal Register XML, document 2021-05550. Only the govinfo PDF is the legal edition. DRS record last changed November 21, 2025.
Copies of the files this page was built from, with their SHA-256. Retrieved October 18, 2026.
| File | Size | SHA-256 | Original |
|---|---|---|---|
| Official PDF | 247 KB | b16c7124…3f39e8f | 2021-05550.pdf on govinfo.gov |
| Federal Register XML | 21 KB | c2bc804b…b4f84c7 | 2021-05550.xml on federalregister.gov |
| FAA DRS HTML attachment | 64 KB | 713955d5…80a2da7 | FAA DRS (API key needed) |
| FAA DRS PDF | 245 KB | 3e94445f…a103469 | FAA DRS (API key needed) |
On this page
Summary
The FAA is adopting a new airworthiness directive (AD) for certain Airbus SAS Model A330-200 Freighter series airplanes. This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary. This AD requires revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations, as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products.
The airworthiness directive
2021-05-12 Airbus SAS: Amendment 39-21455; Docket No. FAA-2020-1115; Product Identifier MCAI-2020-01230-T.
(a) Effective Date
PDF page 2This airworthiness directive (AD) is effective April 26, 2021.
(b) Affected ADs
PDF page 2The AD affects AD 2018-23-14, Amendment 39-19501 (83 FR 60754, November 27, 2018) (AD 2018-23-14).
(c) Applicability
PDF page 2This AD applies to Airbus SAS Model A330-223F and -243F airplanes, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before June 29, 2020.
(d) Subject
PDF page 2Air Transport Association (ATA) of America Code 05, Time Limits/Maintenance Checks.
(e) Reason
PDF page 2This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary. The FAA is issuing this AD to address fatigue cracking, accidental damage, or corrosion in principal structural elements, and possible failure of certain life limited parts, which could result in reduced structural integrity of the airplane.
(f) Compliance
PDF page 2Comply with this AD within the compliance times specified, unless already done.
(g) Requirements
PDF page 2Except as specified in paragraph (h) of this AD: Comply with all required actions and compliance times specified in, and in accordance with, European Union Aviation Safety Agency (EASA) AD 2020-0190, dated August 27, 2020 (EASA AD 2020-0190).
(h) Exceptions to EASA AD 2020-0190
PDF page 2(1) The requirements specified in paragraph (1) of EASA AD 2020-0190 do not apply to this AD.
(2) Paragraph (2) of EASA AD 2020-0190 specifies revising “the approved AMP” within 12 months after its effective date, but this AD requires revising the existing maintenance or inspection program, as applicable, to incorporate the “limitations” specified in paragraph (2) of EASA AD 2020-0190 within 90 days after the effective date of this AD.
(3) The initial compliance time for doing the tasks specified in paragraph (2) of EASA AD 2020-0190 is on or before the applicable “limitations” specified in paragraph (2) of EASA AD 2020-0190, or within 90 days after the effective date of this AD, whichever occurs later.
(4) The provision specified in paragraph (3) of EASA AD 2020-0190 does not apply to this AD.
(5) The “Remarks” section of EASA AD 2020-0190 does not apply to this AD.
(i) Provisions for Alternative Actions or Intervals
PDF page 2After the existing maintenance or inspection program has been revised as required by paragraph (g) of this AD, no alternative actions ( e.g., inspections) or intervals are allowed unless they are approved as specified in the provisions of the “Ref. Publications” section of EASA AD 2020-0190.
(j) Terminating Action for Certain Requirements of AD 2018-23-14
PDF page 2Accomplishing the revision required by this AD terminates the limitation for the nose landing gear lower torque link having part number D64001, as required by paragraph (g) of AD 2018-23-14, for Model A330-223F and -243F airplanes only.
(k) Other FAA AD Provisions
PDF page 2The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager, Large Aircraft Section, International Validation 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 Large Aircraft Section, International Validation Branch, send it to the attention of the person identified in paragraph (l) of this AD. Information may be emailed to: 9-AVS-AIR-730-AMOC@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 instructions from a manufacturer, the instructions must be accomplished using a method approved by the Manager, Large Aircraft Section, International Validation Branch, FAA; or 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): Except as required by paragraph (k)(2) of this AD, 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.
(l) Related Information
PDF page 3For more information about this AD, contact Vladimir Ulyanov, Aerospace Engineer, Large Aircraft Section, International Validation Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax 206-231-3229; email vladimir.ulyanov@faa.gov.
(m) Material Incorporated by Reference
PDF page 3(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) European Union Aviation Safety Agency (EASA) AD 2020-0190, dated August 27, 2020.
(ii) [Reserved]
(3) For EASA AD 2020-0190, contact the EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; email ADs@easa.europa.eu; internet www.easa.europa.eu. You may find this EASA AD on the EASA website at https://ad.easa.europa.eu.
(4) You may view this material at the FAA, Airworthiness Products Section, Operational Safety Branch, 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 206-231-3195. This material may be found in the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2020-1115.
(5) You may view this material that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, email fedreg.legal@nara.gov, or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Rule preamble
The FAA’s background, reasoning and cost estimate, published with the AD.
DatesPage 1
This AD is effective April 26, 2021.
The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of April 26, 2021.
AddressesPage 1
For material incorporated by reference (IBR) in this AD, contact the EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; email ADs@easa.europa.eu; internet www.easa.europa.eu. You may find this IBR material on the EASA website at https://ad.easa.europa.eu. You may view this IBR material at the FAA, Airworthiness Products Section, Operational Safety Branch, 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 206-231-3195. It is also available in the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2020-1115.
For further information contactPage 1
Vladimir Ulyanov, Aerospace Engineer, Large Aircraft Section, International Validation Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax 206-231-3229; email vladimir.ulyanov@faa.gov.
DiscussionPage 1
The EASA, which is the Technical Agent for the Member States of the European Union, has issued EASA AD 2020-0190, dated August 27, 2020 (also referred to as the Mandatory Continuing Airworthiness Information, or the MCAI) (EASA AD 2020-0190), to correct an unsafe condition for all Airbus SAS Model A330-200 Freighter series airplanes, and Model A340-213 and -313 airplanes. EASA AD 2020-0190 refers to Airbus A330 Airworthiness Limitations Section (ALS) Part 1, Variation 10.2, dated June 29, 2020. Airplanes with an original airworthiness certificate or original export certificate of airworthiness issued after June 29, 2020 must comply with the airworthiness limitations specified as part of the approved type design and referenced on the type certificate data sheet; this AD therefore does not include those airplanes in the applicability.
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply to certain Airbus SAS Model A330-200 Freighter series airplanes. The NPRM published in the Federal Register on December 10, 2020 (85 FR 79440). The NPRM was prompted by a determination that new or more restrictive airworthiness limitations are necessary. The NPRM proposed to require revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations, as specified in EASA AD 2020-0190.
The FAA is issuing this AD to address fatigue cracking, accidental damage, or corrosion in principal structural elements, and possible failure of certain life limited parts, which could result in reduced structural integrity of the airplane. See the MCAI for additional background information.
CommentsPage 1
The FAA gave the public the opportunity to participate in developing this final rule. The FAA received no comments on the NPRM or on the determination of the cost to the public.
ConclusionPage 1
The FAA reviewed the relevant data and determined that air safety and the public interest require adopting this final rule as proposed, except for minor editorial changes. The FAA has determined that these minor changes:
• Are consistent with the intent that was proposed in the NPRM for addressing the unsafe condition; and
• Do not add any additional burden upon the public than was already proposed in the NPRM.
Related Service Information Under 1 CFR Part 51Page 1
EASA AD 2020-0190 describes new or more restrictive airworthiness limitations for airplane structures and safe life limits.
This material is reasonably available because the interested parties have access to it through their normal course of business or by the means identified in the ADDRESSES section.
Costs of CompliancePage 1
The FAA estimates that this AD affects 6 airplanes of U.S. registry. The FAA estimates the following costs to comply with this AD:
The FAA has determined that revising the existing maintenance or inspection program takes an average of 90 work-hours per operator, although the agency recognizes that this number may vary from operator to operator. Since operators incorporate maintenance or inspection program changes for their affected fleet(s), the FAA has determined that a per-operator estimate is more accurate than a per-airplane estimate. Therefore, the agency estimates the average total cost per operator to be $7,650 (90 work-hours x $85 per work-hour).
Authority for This RulemakingPage 2
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.
The FAA is 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 findingsPage 2
This AD will not have federalism implications under Executive Order 13132. This AD will not have a substantial direct effect on the States, on the relationship between the national government and the States, or on the distribution of power and responsibilities among the various levels of government.
For the reasons discussed above, I certify that this AD:
(1) Is not a “significant regulatory action” under Executive Order 12866,
(2) Will not affect intrastate aviation in Alaska, and
(3) 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.
Adoption of the AmendmentPage 2
Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows:
Adoption of the amendmentPage 2
1. The authority citation for part 39 continues to read as follows:
2. The FAA amends § 39.13 by adding the following new airworthiness directive:
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 40
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 2009 | 3 |
|---|---|
| 2010 | 3 |
| 2011 | 3 |
| 2012 | 5 |
| 2013 | 9 |
| 2014 | 8 |
| 2015 | 3 |
| 2016 | 1 |
| 2017 | 1 |
4 with no year recorded