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Airworthiness Directive

AD 2010-06-05: Airbus Model A300 B4-2C, B4-103, and B4-203 Airplanes; and Model A300 B4-601, B4-603…

Airworthiness Directives; Airbus Model A300 B4-2C, B4-103, and B4-203 Airplanes; and Model A300 B4-601, B4-603, B4-620, B4-622, B4-605R, and B4-622R Airplanes

Effective
Apr 15, 2010
Published
Mar 11, 2010
Registered aircraft
26

Models this AD may apply to

AI-extracted — verify against original

Matched from the AD's applicability section. Applicability must be confirmed by a mechanic against the aircraft's records.

Aircraft

  • Airbus A300 B4-103
  • Airbus A300 B4-103
  • Airbus A300 B4-203
  • Airbus A300 B4-2C
  • Airbus A300 B4-601
  • Airbus A300 B4-605R
  • Airbus A300 B4-620
  • Airbus A300 B4-622
  • Airbus A300 B4-622
  • Airbus A300 B4-622R
  • Airbus A300 B4-622R
  • Only with: Airplanes modified preventively in service (without preliminary crack findings) per Airbus Service Bulletin A300-53-0297 or A300-57-6053 (Airbus Modification 10453); not applicable where incorporated as corrective action following crack finding.
  • Only with: Airplanes modified preventively in service (without preliminary crack findings) per Airbus Service Bulletin A300-53-0297 or A300-57-6053 (Airbus Modification 10453); not applicable where incorporated as corrective action following crack finding.

Applicability

From the AD text
This AD applies to Airbus airplanes, certificated in any category, as identified in paragraphs (c)(1) and (c)(2) of this AD. (1) Model A300 B4-2C, B4-103, and B4-203 airplanes, all serial numbers, modified preventively in service (without preliminary crack findings) in accordance with Airbus Service Bulletin A300-53-0297 (Airbus Modification 10453). (2) Model A300 B4-601, B4-603, B4-605R, B4-620, B4-622, and B4-622R airplanes, all serial numbers, modified preventively in service (without preliminary crack findings) in accordance with Airbus Service Bulletin A300-57-6053 (Airbus Modification 10453). Note 1: For airplanes on which Airbus Service Bulletin A300-53-0297 or A300-57-6053 (Airbus Modification 10453), as applicable, has been incorporated as a corrective action (repair following crack finding), no action is required by this AD.

Related ADs

Superseded or revised by AD 2012-25-06.

Read the AD in the Federal RegisterReport an error on this page