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Airworthiness directives › 2018-18-19

AD 2018-18-19 Airworthiness Directives; Airbus SAS Airplanes

Superseded. This directive was replaced by AD 2024-06-11. Work to the current one.
2018-10-23
2018-09-18
39-19398
FAA-2018-0364
Airframe
2024-06-11

Models named: A300 B2-1A, B2-1C, B2K-3C, B2-203, B4-2C, B4-103, B4-203, A300 B4-601, B4-603, B4-620. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

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.

Compliance

Comply with this AD within the compliance times specified, unless already done.

Required actions

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).

Unsafe condition

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.

Affected ADs

This AD affects AD 2015-22-05, Amendment 39-18310 (80 FR 69846, November 12, 2015) (“AD 2015-22-05”).

Read the original on the Federal Register →

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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1