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Airworthiness Directives (ADs)

CAA-2010-03-018

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
2010/04/01
Applicability
This AD applies to various aircraft, certificated in any category, equipped with any Honeywell Primus II RNZ-850( )/-851( ) integrated navigation units (INUs) identified in a service bulletin identified in Table 1 of this AD. The aircraft include, but are not limited to, BAE Systems (Operations) Limited (Jetstream) Model 4101 airplanes; Bombardier Model BD-700-1A10 airplanes; Bombardier Model CL-215-6B11 (CL-415 variant) airplanes; Cessna Model 560, 560XL, and 650 airplanes; Dassault-Aviation Model Mystere-Falcon 50 airplanes; 328 Support Services GmbH (Dornier) Model 328-100 and -300 airplanes; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135 airplanes and Model EMB-145, -145ER, -145MR, -145LR, -145XR, -145MP, and - 145EP airplanes; Learjet Model 45 airplanes; Hawker Beechcraft Corporation Model Hawker 800XP and Hawker 1000 airplanes; and Sikorsky Model S-76A, S-76B, and S-76C aircraft.
Model Number
Various Aircraft Equipped With Honeywell Primus II RNZ-850( )/- 851( ) Integrated Navigation Units
CAA AD Number
CAA-2010-03-018
Aeronautics Authority of Original AD
FAA
Original AD Number
2010-07-02
Effective Date
2010/05/03
Subject
We are issuing this AD to ensure that the flightcrew has accurate localizer and glideslope deviation indications. An erroneous localizer or glideslope deviation indication could lead to the aircraft making an approach off the localizer, which could result in impact with an obstacle or terrain.
Reference Publications (Revision/ATA/SB)
This AD supersedes AD 2006-22-05(CAA-2003-02-017A). Ref. Alert Service Bulletin 7510134-34-A0016R1, 7510134-34-A0017, 7510100-34-A0034 and 7510100-34-A0035; Service Bulletin 7510100-34-0037 and 7510134-34-0018.
Remarks
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