VAL Avionics INS 422 Instrukcja Operatora Pobierz pdf (Strona 7)

VAL AVIONICS LTD

INS 429 INTEGRATED NAVIGATION SYSTEM

INSTALLATION AND OPERATOR’S MANUAL

Original Issue Page 7 of 21

2 SECTION II - INSTALLATION

2.1 GENERAL INFORMATION

2.1.1 Scope

This section of the manual will provide the needed information to successfully complete the installation of

your new INS 429 Integrated Navigation System. Please read this section completely before proceeding

with the installation process. Although the INS 429 installation procedures are designed with the do-it-

yourselfer in mind, we at Val Avionics Ltd. strongly suggest that you seek the advice of a qualified

avionics installation facility before beginning this or any other installation project. Qualified avionics

installation technicians can offer good advice as to time-tested installation practices and techniques that can

save you many hours of time and frustration.

2.2 UNPACKING AND INSPECTION

Use care when unpacking the equipment. Inspect the unit and supplied parts for visual signs of damage

during shipment. Examine the unit for loose screws, dents, broken buttons and other signs of damage that

may have occurred during shipment. Verify the contents of the container with the list in section 1.5. If any

damaged or missing parts are discovered during the inspection save the shipping material and contact the

freight carrier to file a claim. If it is suspected that parts were omitted from the container please feel free to

contact Val Avionics Ltd., to acquire the missing items.

2.3 EQUIPMENT INSTALLATION PROCEDURES

2.3.1 Cooling Requirements

Forced air-cooling is not required for the INS 429 Integrated Navigation System. However, when planning

the location for mounting, ensure adequate spacing from heat producing sources such as heating or

defrosting ducts.

2.3.2 Mounting Requirements

The INS 429 Integrated Navigation System should be rigidly mounted in the instrument panel using the

hardware provided in the installation kit. Ensure that the mounting location will provide easy access and a

clear view of the equipment’s front panel from the pilot’s position. Ensure that the mounting position will

provide adequate clearance between the unit and the associated wire harness and the aircraft controls.

Bracing at the rear of the unit should be installed to ensure rigidity in the panel. Consult FAA Advisory

Circular AC 43.13-2A for acceptable practices and techniques.

August 2008

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VAL Avionics INS 422 Instrukcja Operatora Strona 7