NVS 6
MANUAL
The design of the LVC is illustrated in Fig. 5.3. Structurally, the LVC consists of casing (1), which accommodates voltage converter (2) attached to it by means of screws (3). Cover (4) is fastened to the casing with screws (5). Connector plug (6) serves to connect the LVC to the helicopter electrical system of 27 V with the aid of the cable arranged on board the aircraft.
Connector receptacle (7) is intended to connect cable (11), shown in Fig. 5.1, to the LVC.
Connector plug (6) and connector receptacle (7) are secured to the casing by means of screws (8) as shown in Fig. 5.3.
Gaskets (9) installed between the casing, the connector plug and the receptacle serve to protect the LVC interior against direct entry of moisture, whereas LVC cover (4) is filled with sealing compound for the same purpose. Cable (11) attached to the voltage converter is connected to cable (15) to make an electric power supply circuit of the
The use of cables with
5.5Apart from spare dehydrator cartridge, the single set of spare parts includes the following: test pattern, mount, casing, clamp, counterweight, screwdriver, cloth, spare batteries or rechargeable batteries. Spare parts availability is optional, to be specified in each individual supply contract.
5.5.1Test pattern (5), shown in Fig. 3.1, is designed for checking the quality of the image of the NVS 6 (resolving power). The check procedure is presented in 6.2.21 of this Manual.
5.5.2The mount, shown in Fig. 5.4, is intended to secure the NVS 6 on the helmet of the pilot or a helmet of a similar type.
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