Airworthiness Directives (ADs)
CAA-2010-06-007
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
- 2010/06/29
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Applicability
- Airbus Model A318-111, A318-112, A318-121, and A318-122 aeroplanes;
Model A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319- 132, and A319-133 aeroplanes; Model A320-211, A320-212, A320-214, A320-215, A320-216, A320-231, A320-232, and A320-233 aeroplanes, and Model A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231 and A321-232 aeroplanes, that are equipped with a Hamilton Sundstrand Ram Air Turbine (RAT) model ERPS08M as identified by Part-Number (P/N) in
Hamilton Sundstrand Service Bulletin (SB) ERPS08M-29-8 original issue dated 17 June 2009
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Model Number
- AIRBUS A318, A319, A320, and A321 aeroplanes
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CAA AD Number
- CAA-2010-06-007
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2010-0120
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Effective Date
- 2010/07/05
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Subject
- Hydraulic Power – Hamilton Sundstrand Ram Air Turbine Balance
Weight Screws – Inspection / Replacement
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Reference Publications (Revision/ATA/SB)
- ATA 29. This AD supersedes EASA AD 2009-0259 (CAA-2009-12-005) dated 10 December 2009. Ref. Airbus AOT (All Operators Telex) No.A320-29A1150 original issue and Hamilton Sundstrand Service Bulletin No. ERPS08M-29-8 original issue.
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Remarks
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