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FAA orders · airworthiness directive · current

2018-18-21: Time Limits/Maintenance Checks

FAA order 2018-18-21 is an airworthiness directive in force since October 23, 2018. The FAA's subject line: Time Limits/Maintenance Checks. It names Airbus A300: about 120 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: other and general.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Airbus SAS
Models
A300 B4-601, A300 B4-603, A300 B4-605R, A300 B4-620, A300 B4-622, A300 B4-622R, A300 C4-605R Variant F, A300 F4-605R, A300 F4-622R, A310-203, A310-204, A310-221, A310-222, A310-304, A310-322, A310-324, A310-325
On this site
Airbus A300 120 registered

Dates and paperwork

In force since
October 23, 2018
Published
September 18, 2018 (signed August 24, 2018)
Docket
FAA-2018-0396
Replaced by
2024-14-07, 2025-18-07, 2023-12-07, 2022-25-12
Status
Current
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

We are adopting a new airworthiness directive (AD) for all Airbus SAS 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), and Model A310 series airplanes. This AD was prompted by a determination that new or more restrictive maintenance requirements and airworthiness limitations are necessary. This AD requires revising the maintenance or inspection program, as applicable, to incorporate new or more restrictive maintenance requirements and airworthiness limitations. We are issuing this AD to address the unsafe condition on these products.

The order itself the regulatory text, as published

Show the full text (6,637 characters)
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): 2018-18-21 Airbus SAS: Amendment 39-19400; Docket No. FAA-2018-0396; Product Identifier 2017-NM-156-AD. (a) Effective Date This AD is effective October 23, 2018. (b) Affected ADs This AD affects AD 2015-02-16, Amendment 39-18083 (80 FR 5028, January 30, 2015) (``AD 2015-02-16''). (c) Applicability This AD applies to the Airbus SAS airplanes identified in paragraphs (c)(1) through (c)(5) of this AD, certificated in any category, all manufacturer serial numbers. (1) Model A300 B4-601, B4-603, B4-620, and B4-622 airplanes.(2) Model A300 B4-605R and B4-622R airplanes. (3) Model A300 F4-605R and F4-622R airplanes. (4) Model A300 C4-605R Variant F airplanes. (5) Model A310-203, -204, -221, -222, -304, -322, -324, and -325 airplanes. (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 mitigate the risks associated with the effects of aging on airplane systems. Such effects could change system characteristics, leading to an increased potential for failure of certain life-limited parts, and reduced structural integrity or controllability of the airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. [[Page 47056]] (g) Revision of Maintenance or Inspection Program Within 90 days after the effective date of this AD, revise the maintenance or inspection program, as applicable, to incorporate Airbus A310 Airworthiness Limitations Section (ALS) Part 4, ``System Equipment Maintenance Requirements (SEMR),'' Revision 03, dated August 28, 2017; or A300-600 Airworthiness Limitations Section (ALS) Part 4, ``System Equipment Maintenance Requirements (SEMR),'' Revision 03, dated August 28, 2017; as applicable. The initial compliance time for doing the revised actions is at the applicable time specified in Airbus A310 Airworthiness Limitations Section (ALS) Part 4, ``System Equipment Maintenance Requirements (SEMR),'' Revision 03, dated August 28, 2017, or A300-600 Airworthiness Limitations Section (ALS) Part 4, ``System Equipment Maintenance Requirements (SEMR),'' Revision 03, dated August 28, 2017; as applicable; or within 90 days after the effective date of this AD; whichever occurs later. (h) No Alternative Actions or Intervals After the maintenance or inspection program has been revised as required by paragraph (g) of this AD, no alternative actions (e.g., inspections) or intervals may be used unless the actions and 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 for AD 2015-02-16 Accomplishing the actions required by this AD terminates all requirements of AD 2015-02-16. (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 2017-0202, 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-2018-0396. (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) Airbus A300-600 Airworthiness Limitations Section (ALS) Part 4, ``System Equipment Maintenance Requirements (SEMR),'' Revision 03, dated August 28, 2017. (ii) Airbus A310 Airworthiness Limitations Section (ALS) Part 4, ``System Equipment Maintenance Requirements (SEMR),'' Revision 03, dated August 28, 2017. (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.

Related safety bulletins advice on the same designs, not orders

2019-02-19NE-19-03 · Escape Slide Maintenance Tasks and Intervals - JASC 2565
2008-12-11NM-09-03 · Engine Fuel and Control - Implementing Fuel Tank System Airworthiness Limitations
2008-07-02NM-08-31 · Equipment/Furnishings: Non-Textile Floors
2006-12-11SW-07-13 · Oxygen Reserve Cylinder
2006-07-27NM-06-57 · Reports of damage to airplanes and to property on the ground caused by blue or clear ice falling from airplanes.

Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of October 7, 2026. Connections as data: /graph/directive/2018-18-21.json · aircraft systems.