Airworthiness Directives (ADs)
CAA-2014-08-011A(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
- 2014/11/13
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Applicability
- SA 365 N, SA 365 N1, AS 365 N2, AS 365 N3, EC 155 B, EC 155 B1,
AS 332 C, AS332 C1, AS332 L, AS 332 L1, AS 332 L2 and EC 225 LP
helicopters, all serial numbers (s/n), MBB-BK 117 A-1, MBB-BK 117 A-3, MBB-BK 117 A-4, MBB-BK 117 B-1, MBB-BK 117 B-2, MBB-BK 117 C-1 and MBB-BK 117 C-2 helicopters, all s/n, and AB 212, AB 412 and AB 412EP helicopters, all s/n,
if equipped with Emergency Flotation System, all part numbers, as approved
optional kit for ditching provision from the helicopter Manufacturer or by a
Supplemental Type Certificate (STC).
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Model Number
- SA 365, AS 365, EC 155, AS 332 and
EC 225 helicopters
MBB-BK117 helicopters
AB 212 and AB 412 helicopters
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CAA AD Number
- CAA-2014-08-011A(已有後續修訂版)
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2014-0188R1
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Effective Date
- 2014/11/07
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Subject
- Equipment & Furnishings – Emergency Flotation System –
Rotorcraft Flight Manual (Supplement)
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Reference Publications (Revision/ATA/SB)
- ATA 25. This AD revises EASA AD 2014-0188(CAA-2014-08-011) dated 28 August 2014. Ref. None
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Remarks
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