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What is the procedure for a manual engine start?
How do you know that the ITT and torque limiter is working?
The TPE 331 has a high starting electrical current due to:
A series vs a parallel battery start will be:
Thermal runaway in a NiCad battery is caused by:
An auto start uses which components to control FF and IGN:
Which of the following annunciator lights are red:
What is procedure when faced with a double generator failure?
During a generator assisted start of the non-running engine, the running generator assists:
If you have to use the alternative static source, which systems must be switched off?
What are the system voltages of the AC and DC power systems?
What is the starter limitation when performing multiple starts?
If the start selector is in “AIR” position, which system is automatically activated?
Which BUS does the engine fire detection system draw its power from?
During the engine starting cycle, at the moment of depressing the start switch, the current flowing through the starter generator is:
After starting the engine, if the yellow “IGN” light remains on this means:
If the yellow IGN light remains on after start you should:
After a complete electrical failure, will the lack of ignition cause the engines to shut down?
To tie BATT BUS 1, the “BUS TIE” switch should be in the following position:
How do you re-set a generator that won’t come online?
If a BATT TEMP light illuminates after first engine start at base:
If a BATT TEMP light illuminates after second engine start at base:
If a BATT TEMP light illuminates after the second engine start at a remote airfield:
A BATT TEMP light signifies:
Engine starting on the Dornier 228 is:
If both boost pumps fail during flight, the following statement is true:
Failing fuel quantity probes can:
If both boost pumps on one side have failed during flight, what will happen to the engine?
How many ELT units are installed, and the number required for dispatch according to MEL “Remarks and exceptions”?
How many fuel pumps can be INOP, and what is the repair category?
What is the number required to allow dispatch for the “Stall Warning System”?
What is the repair category when 1 fuel quantity indicator is U/S?
What is the time limit for the operation of manual ignition above 10 deg C OAT?
Will fuel pump 1 being inoperative affect the unusable fuel during climb?
Which system powers the lift transducer heater?
Describe the immediate actions required if the GPU power drops offline during engine starting before self-sustaining speed is achieved?
If you depress the INV RESET switch to “RESET”, what happens to the inverter system?
If you switch off the “NON ESS” bus during flight, what will happen to the electrical system in the cockpit?
During takeoff, the BETA lights are off, what mode is the engine/propeller in?
During an engine auto-start procedure, when is the fuel flow and ignition activated by the speed switch?
If the engine torque indication suddenly reads 20% lower, but the FF, ITT and RPM indications remain the same:
The best way to check the condition of the aircraft batteries is to: