Airworthiness Directives (ADs)

Aviation Industry

CAA-2014-04-006A

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.

Issue Date: 2014/05/19

Applicability: HR Smith (Technical Developments) Crash Position Indicator (CPI) System 15-503-134 and 15-503-134-1 series, when equipped with Control Panel part number (P/N) 503-22-() and Beacon release unit P/N 503-21 and System Interface Unit P/N 503-24-() (including 503-24) or P/N 503-42-() (including 503- 42), except System Interface Units having P/N 503-24-A, P/N 503-24-()-A, P/N 503-24-G, P/N 503-24-()-G, P/N 503-42-A, P/N 503-42-()-A, P/N 503-42-G or P/N 503-42-()-G. This CPI System is known to be installed on, but not limited to the following aircraft: - Airbus Helicopters (formerly Eurocopter) Models EC 155B, EC 155 B1, SA 365 N, AS 365 N3, AS 332 L1, AS 332 L2 and EC 225 LP, - Airbus Helicopters Deutschland (formerly Eurocopter Deutschland) EC 135 series and MBB-BK117-C2, - Agusta Westland A109 series, AB139 and AW139, - Sikorsky S-61N, S-76 series and S-92A, and - MD Helicopters Inc. MD900.

Model Number: HR Smith Crash Position Indicator System 15-503-134 and 15-503-134-1 series

CAA AD Number: CAA-2014-04-006A

Aeronautics Authority of Original AD: EASA

Original AD Number: 2014-0095R1

Effective Date: 2014/05/12

Subject: Equipment / Furnishings – Crash Position Indicator – Modification Aircraft Flight Manual – Amendment

Reference Publications (Revision/ATA/SB): ATA 25, This AD revises EASA AD 2014-0095(CAA-2014-04-006) dated 23 April 2014, which superseded EASA AD 2014-0019(CAA-2014-01-009) dated 17 January 2014.

Remarks

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