Airworthiness Directives (ADs)
CAA-2006-05-003C(已有後續修訂版)
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
- 2011/03/02
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Applicability
- A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A320-111,
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 fuel pumps manufactured by Eaton Aerospace Limited (formerly FR-HITEMP Limited) with 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 37508 in production are not affected
by the requirements of this AD.
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Model Number
- AIRBUS A318, A319, A320 and A321 aeroplanes
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CAA AD Number
- CAA-2006-05-003C(已有後續修訂版)
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2007-0218R1
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Effective Date
- 2011/03/14
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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 This AD revises EASA AD 2007-0218(CAA-2006-05-003B)dated 10 August 2007, which superseded EASA AD 2006-0222 dated 20 July 2006. Ref. AIRBUS SB A320-28-1159 original issue.
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Remarks
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