Q1. The function of a vibrator in some gas turbine ignition systems is to provide:
Q2. Concerning the starting procedure of a gas turbine engine: (potential error: see explanation)
Q3. An aircraft flying in conditions of continuous heavy rain and high ambient temperatures may require the precautionary use of:
Q4. In an ignition system during a normal start of a gas turbine engine, igniter activation:
Q5. The use of igniters in a gas turbine engine is required: 1. Throughout the operating range of the engine2. during engine acceleration3. For in-flight relightsThe combination that regroups all of the correct statements is:
Q6. The use of igniters is necessary on a turbo-jet:1 – throughout the operating range of the engine2 – for accelerations3 – for ground starts4 – for in-flight relights5 – during turbulence in flight6 – under heavy precipitation or in icing conditionsThe grouping of correct statements ai e:
Q7. For a turbine engine, the self-sustaining speed relates to the minimum RPM at which the engine: