Engines

The ENGINE CONTROL warning light is inhibited while airborne.
1. True
2. False
The REVERSER warning light illuminated during a normal reverse sequence indicates ?
1. One or more faults in the system if the light illuminates at the start of the reverse sequence.
2. A normal indication if the light extinguishes after 10 seconds.
3. A normal indication until the reverser sleeves are stowed at the completion of the reverse sequence.
If both the ON and ALTN lights in the EEC switch are illuminated simultaneously, what condition is indicated ?
1. The EEC has automatically switched to soft alternate mode.
2. The EEC is inoperative for that engine.
3. The EEC has been manually switched to the soft alternate mode.
4. The soft alternate mode is armed.
The EEC will provide N1 and N2 overspeed protection in both normal and alternate modes.
1. True
2. False
EGT redline protection is ?
1. not provided by the EEC in any mode.
2. provided by the EEC in both normal and alternate modes.
3. provided by the EEC in normal mode only.
At what point does the EEC receive electrical power ?
1. When the engine start switch is positioned to GRD.
2. When the battery switch is placed ON.
3. When engine rotation reaches 15 % N2.
If the ON light is extinguished and the ALTN light is illuminated in the EEC switch, what has occurred ?
1. The EEC has been manually selected to alternate mode.
2. The EEC has automatically switched to alternate mode.
3. The EEC alternate mode is armed.
The Master Caution and ENG annunciator will illuminate if the EEC enters soft alternate mode.
1. True
2. False
"Approach Idle" is commanded by the EEC under what normal condition(s) ?
1. Flaps in the landing configuration or engine anti-ice ON.
2. Below 2000 feet RA.
3. Below 15,000 feet.
4. Landing gear extended.
By what method is engine oil cooled ?
1. A main engine oil cooler using fuel from the fuel tanks.
2. A main engine oil cooler using air flow from the engine.
3. An oil cooler located in the oil tank.
Where in the engine oil system is the oil cooler located ?
1. In the engine oil supply line after leaving the oil tank.
2. In the engine oil return line before reaching the oil tank.
3. In the oil tank.
4. The engine accessory section.
Where is the oil filter located in the engine oil system ?
1. In the engine oil return line.
2. In the engine oil supply line.
3. In the oil tank.
4. In the engine oil cooler.
What is the indication of an imminent oil filter bypass due to contamination ?
1. An amber OIL FILTER BYPASS warning on the associated Display Unit (DU).
2. Illumination of the Master Caution and ENG annunciator.
3. An amber OIL FILTER BYPASS warning on the associated Display Unit (DU) and illumination of the Master Caution and ENG annunciator.
4. Illumination of the FILTER BYPASS warning light on the Fuel Panel.
The Master Caution warning and ENG annunciator will illuminate in conjunction with which of the following warnings or conditions ?
1. OIL FILTER BYPASS, LOW OIL PRESSURE, Oil temperature indicator red band.
2. REVERSER, ENGINE CONTROL, EEC alternate mode.
3. REVERSER, ENGINE CONTROL, OIL FILTER BYPASS, LOW OIL PRESSURE.
4. FILTER BYPASS, LOW OIL PRESSURE, Oil temperature indicator amber band.
How is fuel heated prior to reaching the engine ?
1. The main engine oil coolers and IDG oil coolers.
2. An electrical fuel heater.
3. The IDG oil cooler.
4. The main engine oil cooler.
Imminent contamination of the engine fuel filter is indicated by ?
1. the FILTER BYPASS warning light, Master Caution warning and FUEL annunciator.
2. the FILTER BYPASS warning light only.
3. the FILTER BYPASS warning light, Master Caution warning and ENG annunciator.
Raising the engine start lever opens which fuel valve(s) ?
1. Spar Fuel Shutoff Valve and Engine Fuel Shutoff Valve.
2. Spar Fuel Shutoff Valve.
3. Engine Fuel Shutoff Valve.
4. Engine Fuel Shutoff Valve and Engine Bypass Valve.
Which indication is NOT dependent on the EEC ?
1. Oil Quantity.
2. Fuel Flow.
3. Oil Temperature.
4. Oil Pressure.
How is the EEC affected by a single DEU (Display Electronic Unit) failure ?
1. The EEC for the affected side reverts to alternate mode and the ALTN light illuminates.
2. Both EECs revert to alternate mode and the ALTN lights illuminate..
3. Failure of a single DEU has no effect on the EECs.
4. Both EECs are rendered inoperative and the EEC ON lights are extinguished.
If a throttle is retarded to idle while the EEC is in soft alternate mode, what is the result ?
1. The EEC shifts to hard alternate mode.
2. Approach idle is commanded by the EEC.
3. Ground minimum idle is commanded by the EEC.
4. Flight minimum idle is commanded by the EEC.
Hard alternate mode thrust is always equal to or greater than normal mode thrust as commanded by the EEC.
1. True
2. False
During a battery start with no AC power available, when will the EEC become powered to provide all normal engine parameters and indications ?
1. At 15% N2 rotation.
2. At 56 % N2 rotation.
3. When the start switch is placed to the GRD position.
4. When the start lever is raised to idle.
Which of these warning lights receive their input directly from the EEC ?
1. OIL FILTER BYPASS, FILTER BYPASS
2. ENGINE CONTROL, REVERSER
3. LOW OIL PRESSURE, OIL FILTER BYPASS
4. REVERSER, START VALVE OPEN
Which hydraulic system(s) normally power the thrust reversers ?
1. System A
2. System B
3. System A for Engine 1 and System B for Engine 2.
4. System A or B.
Is thrust reverse available in the event of a loss of System A or B ?
1. Yes, the Standby System is available for the affected thrust reverser.
2. No, the affected thrust reverser is inoperative.
3. No, both trust reversers are inoperative.
4. Yes, the remaining system will power both thrust reversers.
Can thrust reverse be deployed if the aircraft has not touched down ?
1. No, the Air / Ground safety sensor must be in ground mode.
2. Yes, if the thrust levers are in idle and either radio altimeter senses less than 10 feet RA.
3. Yes, if the thrust levers are in idle and both radio altimeters sense less than 10 feet RA.
4. No, the Air / Ground safety sensor must be in ground mode and either radio altimeter senses O feet RA.
What is the crew's indication that the reverser sleeve has fully deployed from the stowed position ?
1. A green REV indication above the respective N1 indicator.
2. An amber REV indication above the respective N1 indicator.
3. The REVERSER warning light on the Engine Panel illuminates.
4. The reverse thrust lever may be moved beyond the interlock position.
The REVERSE light on the Aft Overhead Engine Panel indicates ?
1. that reverse has been commanded with the reverse thrust lever.
2. that the thrust reverser has been commanded to stow.
3. reverse thrust is inoperative for that engine.
When is the selected igniter armed for ignition when starting an engine on the ground ?
1. When the start switch is placed to the GRD position.
2. When the start lever is raised to idle.
3. When the igniter is selected by placing the selector switch to L, BOTH or R.
Placing the start switch to GRD for an inflight start arms which igniter(s) ?
1. Both igniters.
2. The left igniter.
3. The right igniter.
4. The igniter that has been selected with the igniter selector switch.
Which igniters are energized when the start switch is placed in the CONT position if N2 is below idle and the start lever is in idle ?
1. Both igniters regardless of the selector switch position.
2. The selected igniter(s).
Which start switch position will energize both igniters regardless of igniter selector switch position if the start lever is in idle ?
1. FLT
2. CONT
3. GRD
What is the electrical source for the left igniter ?
1. AC Transfer Bus 1.
2. AC Transfer Bus 2.
3. The AC Standby Bus.
4. DC Bus 1.
What is the electrical source for the right igniter ?
1. The AC Standby Bus.
2. AC Transfer Bus 1.
3. AC Transfer Bus 2.
4. DC Bus 2.
Which system arms the igniter plugs ?
1. The EEC.
2. The start levers.
3. The start switches.
Which power source opens the engine start valve and closes the engine bleed valve when the start switch is placed to ground ?
1. The Battery.
2. Transfer Bus 1.
3. The Battery Bus.
4. DC Bus 1.
The start valve closes and the START VALVE OPEN light extinguishes at approximately ?
1. 56 % N2
2. 56% N1
3. 15% N2
4. 15% N1
Which is the recommended value before raising the start lever to idle during the engine start sequence ?
1. 25% N2 or maximum motoring speed.
2. 56% N2 or maximum motoring speed.
3. At the first indication of N1 rotation.
4. 25% N1 or maximum motoring speed.
The EEC provides protection against a wet start.
1. True
2. False
The EEC provides protection when a hot start has occurred.
1. True
2. False
The EEC provides protection against EGT start limit exceedance.
1. True
2. False
The EEC does not provide abnormal start protections for inflight starts.
1. True
2. False

Engines