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PASGT LEC MIDTERM QUIZ 2 - 2631

Total questions: 20

Worksheet time: 15mins

Name
Class
Date
1.

What is the primary purpose of marine gas turbine maintenance?

a)

Increase fuel viscosity to improve combustion efficiency under load conditions

b)

Reduce crew workload during voyages by automating propulsion control systems

c)

Ensure safe, reliable, and efficient turbine operation throughout its service life

d)

Modify turbine performance parameters for emergency auxiliary electricity generation

2.

Which type of maintenance is performed regularly to prevent breakdowns?

a)

Corrective Maintenance, carried out only after equipment failure has occurred

b)

Routine/Preventive Maintenance, done periodically to avoid unexpected faults

c)

Scheduled Major Overhaul, performed after a specific operational hour threshold

d)

Emergency Maintenance, triggered when a critical system shuts down suddenly

3.

What does LOTO stand for in maintenance safety?

a)

Lubrication Operation Test Order, used to verify oil circulation before startup

b)

Level Operation Timing Outline, a procedure to control load application rates

c)

Lock-Out/Tag-Out, a safety method to isolate and secure hazardous energy sources

d)

Low Overheat Temperature Override, a system that prevents excessive temperature rise

4.

Which component is typically inspected for cracks or thermal fatigue during maintenance?

a)

Cooling water pumps only, due to their high exposure to temperature fluctuations

b)

Turbine blades and vanes, as they face extreme stress, heat, and rotational forces

c)

Lubrication filters exclusively, since they accumulate impurities during operation

d)

Fuel injectors, because they regulate flow and atomization under combustion pressure

5.

During pre-maintenance preparation, which procedure ensures safe system isolation?

a)

Locking and tagging energy sources to prevent accidental re-energization

b)

Measuring ambient temperature only to verify safe working conditions

c)

Checking fuel viscosity exclusively before starting disassembly operations

d)

Igniting residual fuel to confirm combustion chamber clearance

6.

Which PPE is essential during turbine maintenance?

a)

Reflective vests exclusively, to ensure visibility inside confined compartments

b)

Life jackets and hearing aids only, especially in shipboard environments

c)

Heat-resistant gloves, goggles, and safety boots to protect against burns and impact

d)

Fireproof suits without gloves, to protect only the body from radiant heat

7.

What is checked during visual inspection before maintenance?

a)

Oil/fuel leaks, corrosion, and foreign object debris around critical components

b)

Exhaust gas temperature only, to assess combustion chamber condition

c)

Starter motor rotation exclusively, to confirm mechanical integrity

d)

Ambient air humidity only, to measure atmospheric working conditions

8.

What is performed before restarting the turbine after maintenance?

a)

Fuel viscosity adjustment only, to improve spray characteristics

b)

Leak tests, sensor checks, dry rotation, and trial start to ensure readiness

c)

Fire extinguisher replacement exclusively, to comply with safety requirements

d)

Cooling water flow measurement only, to confirm circulation rate

9.

Which maintenance task is performed on the combustion chamber?

a)

Inspecting fuel nozzles and cleaning carbon deposits to maintain proper combustion

b)

Aligning starter motor exclusively, to ensure smooth engine acceleration

c)

Purging ventilation lines only, to prevent pressure build-up in ducts

d)

Checking oil pump pressure only, to verify lubrication circuit performance

10.

Which system is calibrated and tested during maintenance?

a)

Air intake system only, to ensure adequate oxygen delivery

b)

Control and monitoring system, to verify accurate sensor feedback and system response

c)

Lubrication system exclusively, to guarantee smooth mechanical operation

d)

Fuel injection system only, to check spray pattern and flow rates

11.

A turbine shows abnormal vibration during trial rotation after maintenance. What is the likely cause?

a)

Ambient temperature below the required operating range, affecting thermal balance

b)

Fire extinguisher system positioned too close to the exhaust section, altering airflow

c)

Misalignment or foreign object debris in the rotating assembly causing imbalance

d)

Fuel viscosity too high, resulting in incomplete combustion and load fluctuations

12.

If a bearing oil leak occurs after reassembly, what could be the primary reason?

a)

Incorrect seal installation or worn seal components failing to maintain pressure containment

b)

Sensor calibration drift caused by previous electrical interference during inspection

c)

Fuel pressure too low to achieve sufficient atomization during startup operations

d)

Ventilation system over-pressurized, forcing air into the lubrication circuits

13.

During inspection, carbon deposits are found in the combustion chamber. Which factor contributed most?

a)

Cooling water overcapacity causing incomplete combustion cycles and unburnt residues

b)

Incomplete fuel combustion or irregular maintenance leading to soot accumulation

c)

Excess lubrication oil flow entering the combustion chamber and mixing with fuel

d)

Misaligned starter motor affecting ignition timing during repeated starts

14.

A fuel pump fails to operate during testing after maintenance. What is a likely analysis?

a)

Turbine blade alignment incorrect, leading to imbalance during startup sequence

b)

Oil filter clogged and restricting lubrication flow through key components

c)

Electrical isolation not properly restored or mechanical fault present in the pump

d)

Ambient air too cold for the fuel delivery system to function effectively

15.

Sensor calibration drifts are discovered during post-maintenance checks. What is the probable cause?

a)

Fuel line purging incomplete, causing erratic combustion pressure readings

b)

Wear, damage, or improper handling during maintenance affecting sensor precision

c)

Excess torque on fasteners altering sensor mount alignment and signal quality

d)

Low oxygen concentration in the compartment affecting sensor feedback signals

16.

A technician experiences difficulty disassembling a component. Which factor is most likely responsible?

a)

Excessive lubrication oil flow, creating suction and sealing between moving parts

b)

Incorrect sensor calibration causing misleading pressure readings during disassembly

c)

Thermal expansion or corrosion of parts increasing friction and mechanical binding

d)

Low ambient temperature reducing material flexibility during removal

17.

An alarm triggers unexpectedly during trial start. What is the likely explanation?

a)

Interlock or sensor miscalibration causing false safety or operational signals

b)

Fuel valve partially open, creating inconsistent pressure within the combustion system

c)

Overfilled lubrication system leading to unexpected pressure build-up

d)

Foreign object debris in ventilation ducts restricting airflow detection

18.

Blade damage is found during inspection. What is the primary cause?

a)

Ambient air contamination alone, causing slight erosion but not mechanical failure

b)

Improper ventilation only, leading to localized temperature fluctuations

c)

Incorrect oil type exclusively, resulting in reduced lubrication at contact points

d)

Foreign object impact or overheating during operation causing structural damage

19.

If a heat exchanger shows insufficient cooling during tests, what is the likely cause?

a)

Misaligned turbine casing causing uneven thermal transfer across surfaces

b)

Blockage, pump failure, or fouling in the system reducing heat transfer efficiency

c)

Excess lubrication oil circulation interfering with cooling flow patterns

d)

Carbon deposits in the combustion chamber reducing heat absorption capacity

20.

During troubleshooting, sensors report normal readings but abnormal vibration persists. What is the best analysis?

a)

Fuel pump pressure too high, leading to fluctuating combustion cycles

b)

Mechanical misalignment or FOD undetected by sensors causing imbalance

c)

Cooling system overcapacity resulting in excessive thermal contraction

d)

Ventilation system underperforming and reducing turbine aerodynamic stability