Airworthiness Directives (ADs)
CAA-2006-05-003D(已被CAA-2023-05-008取代)
The aircraft owner or operator shall comply with Airworthiness Directives issued by the CAA or the aeronautics authority of the State of Design (SoD) of the aviation products, appliances and parts, and take all necessary actions thereto.
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Issue Date
- 2014/10/14
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Applicability
- Airbus A318-111, A318-112, A318-121, A318-122, A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A320-211, A320-212, A320-214, A320-215, A320-216, A320-231, A320-232, A320-233, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231 and A321-232 aeroplanes, all manufacturer serial numbers, if equipped with Eaton Aerospace Limited (formerly FR-HITEMP Limited) fuel pumps identified by Part Number (P/N) 568-1-27202-001, P/N 568-1-27202-002, or P/N 568-1-27202-005.
Note: Aeroplanes on which fuel pumps have not been modified or replaced since embodiment of Airbus modification (mod) 37508 in production are not affected by the requirements of this AD.
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Model Number
- A318, A319, A320 and A321 aeroplanes
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CAA AD Number
- CAA-2006-05-003D(已被CAA-2023-05-008取代)
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2007-0218R2
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Effective Date
- 2014/10/10
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Subject
- Fuel – Main Fuel Pump System / Fuel Pumps – Airworthiness
Limitations / Inspection / Replacement
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Reference Publications (Revision/ATA/SB)
- ATA 28. This AD revises EASA AD 2007-0218R1(CAA-2006-05-003C) dated 28 February 2011. The original issue of this AD superseded EASA AD 2006-0222 dated 20 July 2006.
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Remarks
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