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2020-0145 : Landing Gear – Main Landing Gear Hinge Arm / Barrel – Pin Replacement / Inspection / Spacer Modification

Number 2020-0145
Issued by Europe  Europe
Issue date 2020-07-01
Effective date 2020-07-15
EASA approval number
ATA Chapter 32
Approval Holder
/ Type Designation
  • AIRBUS S.A.S.
    • A300
      • A300B4-102
      • A300B4-103
      • A300B4-120
      • A300B4-203
      • A300B4-220
      • A300B4-2C
      • A300C4-203
      • A300F4-203
    • A300-600
      • A300B4-601
      • A300B4-603
      • A300B4-605R
      • A300B4-620
      • A300B4-622
      • A300B4-622R
      • A300C4-605R variant F
      • A300C4-620
      • A300F4-605R
      • A300F4-622R
    • A300-600ST (Beluga)
      • A300F4-608ST
Revision Not applicable
Correction Not applicable
Supersedure This AD supersedes EASA AD 2018-0170 dated 06 August 2018.
Publication(s) and related information Airbus AOT A32W008-16 original issue dated 25 February 2016, or Revision 01 dated 30 July 2018. Airbus SB A300-32-0468 original issue dated 24 September 2019. Airbus SB A300-32-0469 original issue dated 24 September 2019. Airbus SB A300-32-0470 original issue dated 19 March 2020. Airbus SB A300-32-6119 original issue dated 24 September 2019. Airbus SB A300-32-6120 original issue dated 24 September 2019. Airbus SB A300-32-6121 original issue dated 19 March 2020. Airbus SB A300-32-9024 original issue dated 24 September 2019. Airbus SB A300-32-9025 original issue dated 24 September 2019. Airbus SB A300-32-9026 original issue dated 19 March 2020. SAFRAN Landing Systems SB 470-32-840 original issue dated 03 December 2019. The use of later approved revisions of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
PAD number 20-074
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 05 May 2020 as PAD 20-074 for consultation until 02 June 2020. The Comment Response Document can be found in the EASA Safety Publications Tool, in the compressed (zipped) file attached to the record for this AD. 3. Enquiries regarding this AD should be referred to the EASA Programming and Continued Airworthiness Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu. 4. Information about any failures, malfunctions, defects or other occurrences, which may be similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on a product, part or appliance not affected by this AD, can be reported to the EU aviation safety reporting system.