Airworthiness Directives (ADs)
CAA-2014-07-009
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
- 2014/07/21
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Applicability
- HR Smith (Technical Developments) Crash Position Indicator (CPI) system 15-503-134-1 series, if equipped with
- Beacon Release Unit (BRU) Part Number (P/N) 503-21-1, and
- System Interface Unit (SIU) P/N 503-24 or P/N 503-24-2 or P/N 503-24-6.
This CPI system is known to be installed on, but not limited to the following aircraft:
- Airbus Helicopters (formerly Eurocopter) Model EC 225 LP
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Model Number
- HR SMITH Crash Position Indicator System 15 503 134-1 series
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CAA AD Number
- CAA-2014-07-009
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Aeronautics Authority of Original AD
- EASA
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Original AD Number
- 2014-0125
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Effective Date
- 2014/05/22
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Subject
- Equipment / Furnishings – Crash Position Indicator System – Replacement; Aircraft Flight Manual – Amendment
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Reference Publications (Revision/ATA/SB)
- ATA 25. Ref. HR Smith SB HRS-SB-03-17-141 issue 05 dated 10 April 2014.
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Remarks
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