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2016-0080 : Fuel – Fuel Pumps / Power Supply Circuit Breaker – Functional Test / Replacement / Fuel Pumps Replacement

Number 2016-0080
Issued by Europe  Europe
Issue date 2016-04-21
Effective date 2016-05-05
EASA approval number
ATA Chapter 28
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
    • 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 This AD supersedes EASA AD 2013-0163 dated 24 July 2013.
Publication(s) and related information Airbus AOT A28W002-13 original issue dated 23 July 2013. Airbus SB A300-28-0093 original issue dated 15 December 2015. Airbus SB A300-28-6111 original issue dated 15 December 2015. Airbus SB A300-28-9025 original issue dated 15 December 2015. Airbus SB A310-28-2176 original issue dated 15 December 2015. The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
PAD number 16-041
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 16 March 2016 as PAD 16-041 for consultation until 13 April 2016. No comments were received during the consultation period. 3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs[at]easa.europa.eu.