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<strong>Talon</strong> <strong>Helicopters</strong> <strong>Ltd</strong>.<br />

- <strong>Edition</strong> 2 -<br />

Company Operations Manual<br />

Chapter 6 § Aircraft Requirements<br />

6.6.2 Instrument Requirements - Night VFR (702)<br />

No person shall conduct a take-off for the purpose of a night VFR flight unless it is equipped with the following<br />

instruments:<br />

§ instruments required for day VFR;<br />

§ sensitive altimeter adjustable for barometric pressure;<br />

§ vertical speed indicator;<br />

§ a means of preventing malfunction caused by icing for each airspeed indicating system;<br />

§ outside air temperature gauge;<br />

§ a gyroscopic direction indicator or a stabilized magnetic direction indicator, when the aerodrome is not<br />

visible from the aircraft;<br />

§ an attitude indicator;<br />

§ a turn and slip indicator or turn coordinator;<br />

§ where the aircraft is to be operated within the Northern Domestic Airspace, a means of establishing<br />

direction that is not dependent on a magnetic source;<br />

§ radio communication equipment adequate to permit 2-way communication on the appropriate<br />

frequency;<br />

§ radio navigation equipment adequate to permit the aircraft to be navigated safely; and,<br />

§ means for lighting for all instruments used to operate the helicopter.<br />

6.7 Fuelling Procedures<br />

6.7.1 Supervision<br />

The PIC will supervise the fuelling of their aircraft to ensure that the following fuelling procedures are followed.<br />

6.7.2 Fuel Contamination Precautions<br />

<strong>Helicopters</strong> should be fuelled from a dispensing system that has an approved filter, water separator, or monitor to<br />

prevent water or sediment entering the helicopter’s fuel tanks. If it is necessary to use drums or cans of fuel then<br />

the fuel is to be filtered through a proper filter and water separator. A clean chamois or felt lined filter funnel may<br />

only be used under dire emergency conditions, recognizing that filter fibres may clog fuel system filters and<br />

nozzles. After the emergency flight, the aircraft should be checked following approved maintenance instructions<br />

for contaminated fuel.<br />

Note: Ordinary plastic funnels or other non-conducting materials can increase static generation. The use<br />

of chamois as a filter is extremely hazardous.<br />

During the pre-flight check, a reasonable quantity of fuel should be drawn from the lowest point in the fuel system<br />

into a plastic jar. A “clear and bright” visual test should be made to establish that the fuel is completely free of<br />

visible solid contamination and water (including any resting on the bottom or sides of the container) and that the<br />

fuel possesses an inherent brilliance and sparkle in the presence of light.<br />

6.7.3 Bonding Requirements<br />

Fuel passing through pipes, filters and hoses generates static electricity. If proper precautions are not taken, this<br />

static can discharge as a spark, and ignite the fuel.<br />

Sparks can be avoided by proper electrical bonding of all parts of the fuelling system and the aircraft. Bonding<br />

cables must be conductive, durable and flexible. Bonding connections must be electrically and mechanically firm.<br />

Loose bonds can be an arc point generating a spark and must be repaired. Jacks, plugs, clamps, and connecting<br />

points must be clean, unpainted metal to provide a positive electrical connection. The bond must be maintained<br />

December 31, 2015 <strong>Amend</strong>ment 0 6-3

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