WorksheetsPASGT LEC MIDTERM QUIZ 2 - 2631
Total questions: 20
Worksheet time: 15mins
What is the primary purpose of marine gas turbine maintenance?
Increase fuel viscosity to improve combustion efficiency under load conditions
Reduce crew workload during voyages by automating propulsion control systems
Ensure safe, reliable, and efficient turbine operation throughout its service life
Modify turbine performance parameters for emergency auxiliary electricity generation
Which type of maintenance is performed regularly to prevent breakdowns?
Corrective Maintenance, carried out only after equipment failure has occurred
Routine/Preventive Maintenance, done periodically to avoid unexpected faults
Scheduled Major Overhaul, performed after a specific operational hour threshold
Emergency Maintenance, triggered when a critical system shuts down suddenly
What does LOTO stand for in maintenance safety?
Lubrication Operation Test Order, used to verify oil circulation before startup
Level Operation Timing Outline, a procedure to control load application rates
Lock-Out/Tag-Out, a safety method to isolate and secure hazardous energy sources
Low Overheat Temperature Override, a system that prevents excessive temperature rise
Which component is typically inspected for cracks or thermal fatigue during maintenance?
Cooling water pumps only, due to their high exposure to temperature fluctuations
Turbine blades and vanes, as they face extreme stress, heat, and rotational forces
Lubrication filters exclusively, since they accumulate impurities during operation
Fuel injectors, because they regulate flow and atomization under combustion pressure
During pre-maintenance preparation, which procedure ensures safe system isolation?
Locking and tagging energy sources to prevent accidental re-energization
Measuring ambient temperature only to verify safe working conditions
Checking fuel viscosity exclusively before starting disassembly operations
Igniting residual fuel to confirm combustion chamber clearance
Which PPE is essential during turbine maintenance?
Reflective vests exclusively, to ensure visibility inside confined compartments
Life jackets and hearing aids only, especially in shipboard environments
Heat-resistant gloves, goggles, and safety boots to protect against burns and impact
Fireproof suits without gloves, to protect only the body from radiant heat
What is checked during visual inspection before maintenance?
Oil/fuel leaks, corrosion, and foreign object debris around critical components
Exhaust gas temperature only, to assess combustion chamber condition
Starter motor rotation exclusively, to confirm mechanical integrity
Ambient air humidity only, to measure atmospheric working conditions
What is performed before restarting the turbine after maintenance?
Fuel viscosity adjustment only, to improve spray characteristics
Leak tests, sensor checks, dry rotation, and trial start to ensure readiness
Fire extinguisher replacement exclusively, to comply with safety requirements
Cooling water flow measurement only, to confirm circulation rate
Which maintenance task is performed on the combustion chamber?
Inspecting fuel nozzles and cleaning carbon deposits to maintain proper combustion
Aligning starter motor exclusively, to ensure smooth engine acceleration
Purging ventilation lines only, to prevent pressure build-up in ducts
Checking oil pump pressure only, to verify lubrication circuit performance
Which system is calibrated and tested during maintenance?
Air intake system only, to ensure adequate oxygen delivery
Control and monitoring system, to verify accurate sensor feedback and system response
Lubrication system exclusively, to guarantee smooth mechanical operation
Fuel injection system only, to check spray pattern and flow rates
A turbine shows abnormal vibration during trial rotation after maintenance. What is the likely cause?
Ambient temperature below the required operating range, affecting thermal balance
Fire extinguisher system positioned too close to the exhaust section, altering airflow
Misalignment or foreign object debris in the rotating assembly causing imbalance
Fuel viscosity too high, resulting in incomplete combustion and load fluctuations
If a bearing oil leak occurs after reassembly, what could be the primary reason?
Incorrect seal installation or worn seal components failing to maintain pressure containment
Sensor calibration drift caused by previous electrical interference during inspection
Fuel pressure too low to achieve sufficient atomization during startup operations
Ventilation system over-pressurized, forcing air into the lubrication circuits
During inspection, carbon deposits are found in the combustion chamber. Which factor contributed most?
Cooling water overcapacity causing incomplete combustion cycles and unburnt residues
Incomplete fuel combustion or irregular maintenance leading to soot accumulation
Excess lubrication oil flow entering the combustion chamber and mixing with fuel
Misaligned starter motor affecting ignition timing during repeated starts
A fuel pump fails to operate during testing after maintenance. What is a likely analysis?
Turbine blade alignment incorrect, leading to imbalance during startup sequence
Oil filter clogged and restricting lubrication flow through key components
Electrical isolation not properly restored or mechanical fault present in the pump
Ambient air too cold for the fuel delivery system to function effectively
Sensor calibration drifts are discovered during post-maintenance checks. What is the probable cause?
Fuel line purging incomplete, causing erratic combustion pressure readings
Wear, damage, or improper handling during maintenance affecting sensor precision
Excess torque on fasteners altering sensor mount alignment and signal quality
Low oxygen concentration in the compartment affecting sensor feedback signals
A technician experiences difficulty disassembling a component. Which factor is most likely responsible?
Excessive lubrication oil flow, creating suction and sealing between moving parts
Incorrect sensor calibration causing misleading pressure readings during disassembly
Thermal expansion or corrosion of parts increasing friction and mechanical binding
Low ambient temperature reducing material flexibility during removal
An alarm triggers unexpectedly during trial start. What is the likely explanation?
Interlock or sensor miscalibration causing false safety or operational signals
Fuel valve partially open, creating inconsistent pressure within the combustion system
Overfilled lubrication system leading to unexpected pressure build-up
Foreign object debris in ventilation ducts restricting airflow detection
Blade damage is found during inspection. What is the primary cause?
Ambient air contamination alone, causing slight erosion but not mechanical failure
Improper ventilation only, leading to localized temperature fluctuations
Incorrect oil type exclusively, resulting in reduced lubrication at contact points
Foreign object impact or overheating during operation causing structural damage
If a heat exchanger shows insufficient cooling during tests, what is the likely cause?
Misaligned turbine casing causing uneven thermal transfer across surfaces
Blockage, pump failure, or fouling in the system reducing heat transfer efficiency
Excess lubrication oil circulation interfering with cooling flow patterns
Carbon deposits in the combustion chamber reducing heat absorption capacity
During troubleshooting, sensors report normal readings but abnormal vibration persists. What is the best analysis?
Fuel pump pressure too high, leading to fluctuating combustion cycles
Mechanical misalignment or FOD undetected by sensors causing imbalance
Cooling system overcapacity resulting in excessive thermal contraction
Ventilation system underperforming and reducing turbine aerodynamic stability
