You are not logged in
  Safety Publications Tool

2019-0188 : Hydraulic Power – Hydraulic Reservoir Air Pressurization System Lines – Functional Tests

Number 2019-0188
Issued by Europe  Europe
Issue date 2019-07-31
Effective date 2019-08-31
EASA approval number
ATA Chapter 29
Approval Holder
/ Type Designation
  • AIRBUS S.A.S.
    • 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
    • A310
      • A310-203
      • A310-203C
      • A310-204
      • A310-221
      • A310-222
      • A310-304
      • A310-308
      • A310-322
      • A310-324
      • A310-325
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information Airbus A300-600 (including A300-600ST) ALS Part 3 Revision 1, Variation 1.1 dated 21 February 2019. Airbus A310 ALS Part 3 Revision 1, Variation 1.1 dated 21 February 2019. The use of later approved revisions or variations of the above-mentioned documents is acceptable for compliance with the requirements of this AD.
PAD number 19-084R1
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 21 May 2019 as PAD 19-084 for consultation until 18 June 2019 and republished on 03 July 2019 as PAD 19-084R1 for additional consultation until 17 July 2019. The Comment Response Documents 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.