INDIGO INSTRUMENTS (1117-1427)

#95. The heading information originating from the gyromagnetic compass flux valve is sent to the:

• Aheading indicator
• Berror detector
• Camplifier.
• Derector system.

#96. The gyromagnetic compass torque motor :

• Ais fed by the flux valve
• Bcauses the directional gyro unit to precess
• Cfeeds the error detector system
• Dcauses the heading indicator to precess

The term 'useful load' as applied to an aeroplane includes

• Atraffic load plus useable fuel.
• B traffic load only.
• C the revenue-earning portion of traffic load only.
• Dthe revenue-earning portion of traffic load plus useable fuel.