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  Safety Publications Tool

2012-0091 : Fuel / Main Transfer System – Inner, Centre and Trim Tank Fuel Pump Control Circuit – Modification

Number 2012-0091
Issued by Europe  Europe
Issue date 2012-05-25
Effective date 2012-06-08
EASA approval number
ATA Chapter 28
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 SB A310-28-2170 original issue, dated 28 February 2012. Airbus SB A300-28-6104 original issue, dated 28 February 2012. Airbus SB A300-28-9018 original issue, dated 28 February 2012. The use of later approved revisions of these documents is acceptable for compliance with requirements of this AD
PAD number 12-025
Remarks 1. If requested and appropriately substantiated, EASA can approve Alternative Methods of Compliance for this AD. 2. This AD was posted on 29 March 2012 as PAD 12-025 for consultation until 26 April 2012. The Comment Response Document can be found at https://ad.easa.europa.eu. 3. Enquiries regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA. E-mail ADs[at]easa.europa.eu.