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Free Practice Questions for GASM Uzakyol Başmühendisi

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Key Facts: GASM Uzakyol Başmühendisi Exam

STCW III/2

Regulation Level

IMO STCW Convention

70 / 100

Module Pass Score

GASM Sınav Yönergesi

5 Modules

Tablo-8 Assessment

UAB Denizcilik Genel Müd.

Computer-Based

Testing Mode

GASM Exam Centers

5 Years

CoC Validity

STCW Revalidation

3,000+ kW

Vessel Power Scope

Chief Engineer Unlimited

GASM Uzakyol Başmühendisi theory is the statutory management-level exam for Chief Engineers on vessels over 3,000 kW in Turkey. It evaluates five modules under Tablo-8 with a 70% passing threshold per paper. This OpenExamPrep resource offers 100 independent practice questions in English covering core propulsion, auxiliary, legal, naval architecture, and technical communication topics.

Sample GASM Uzakyol Başmühendisi Practice Questions

Try these sample questions to review concepts for the GASM Uzakyol Başmühendisi exam. Each question includes a detailed explanation. Start the interactive quiz above for the full 100+ question experience with AI tutoring.

1What is the primary operational purpose of fitting spring-loaded relief valves to the scavenge air receiver of a large two-stroke marine crosshead diesel engine?
A.To release excess overpressure safely into the engine room space in the event of a scavenge fire or explosive ignition of unburnt cylinder oil and carbon residues, reseating immediately to prevent ingress of atmospheric oxygen.
B.To vent excess turbocharger boost air directly overboard when the vessel operates at reduced cruising speed or during slow steaming.
C.To provide an emergency source of high-pressure breathing air to the engine room during a total electrical blackout.
D.To prevent cylinder exhaust gases from backflowing into the turbocharger compressor wheel during engine starting.
Explanation: Scavenge air relief valves are critical statutory safety devices installed on the scavenge manifolds of large two-stroke crosshead engines. In the event of a scavenge fire or violent pressure surge caused by the ignition of unburnt cylinder lubricating oil and carbon deposits, they lift rapidly to relieve overpressure and prevent trunking rupture. They reseat immediately under spring force to stop atmospheric oxygen from entering and sustaining the fire.
2A six-cylinder, two-stroke single-acting marine diesel engine has a cylinder bore of 0.60 m and a stroke of 2.40 m. When running at 100 rpm, indicator cards reveal an average mean indicated pressure (MIP) of 1.80 MPa (18.0 bar) across all cylinders. What is the total indicated power developed by the engine?
A.12,215 kW
B.6,108 kW
C.24,430 kW
D.15,380 kW
Explanation: For a two-stroke engine, power per cylinder is given by P = P_mi * L * A * n. Cylinder cross-sectional area A = (pi / 4) * (0.60)^2 = 0.282743 m^2. Stroke length L = 2.40 m, and rotational frequency n = 100 / 60 = 1.6667 rev/s. Power per cylinder = 1,800,000 Pa * 2.40 m * 0.282743 m^2 * (100 / 60) s^-1 = 2,035,752 W = 2,035.75 kW. For 6 cylinders, total indicated power = 6 * 2,035.75 kW = 12,214.5 kW, which rounds to 12,215 kW.
3A main propulsion engine delivers 10,000 kW brake power at normal sea load while consuming 1,750 kg/h of heavy fuel oil with a lower heating value (LHV) of 42,700 kJ/kg. What are the specific fuel oil consumption (SFOC) and the overall brake thermal efficiency of the engine?
A.SFOC = 175.0 g/kWh; brake thermal efficiency = 48.2%
B.SFOC = 195.0 g/kWh; brake thermal efficiency = 43.2%
C.SFOC = 160.0 g/kWh; brake thermal efficiency = 52.8%
D.SFOC = 175.0 g/kWh; brake thermal efficiency = 39.5%
Explanation: SFOC is calculated as fuel mass flow per unit power: SFOC = (1,750 kg/h * 1,000 g/kg) / 10,000 kW = 175.0 g/kWh. Brake thermal efficiency eta_b = Work output / Heat input = P_b / (m_f * LHV). Work output per hour = 10,000 kW * 3,600 s = 36,000,000 kJ. Heat input per hour = 1,750 kg * 42,700 kJ/kg = 74,725,000 kJ. Thus, eta_b = 36,000,000 / 74,725,000 = 0.48177 = 48.2%.
4In an electronically controlled two-stroke marine diesel engine (MAN B&W ME-C series), which hydraulic component directly controls fuel injection timing and quantity by regulating servo oil flow to the fuel pressure booster?
A.The Fuel Injection Valve Actuation (FIVA) valve or Electronic Fuel Injection (ELFI) valve.
B.The cylinder lubricating oil dosage injector (Alpha lubricator).
C.The starting air distributor pilot valve.
D.The scavenge air auxiliary blower variable speed drive.
Explanation: In MAN B&W ME-C electronically controlled engines, the camshaft is replaced by hydraulic cylinder units (HCUs). The FIVA (Fuel Injection Valve Actuation) valve or ELFI (Electronic Fuel Injection) proportional valve is driven by the engine control system (ECS). It modulates high-pressure hydraulic servo oil (200-300 bar) to actuate the fuel oil pressure booster piston, precisely governing injection timing, pressure profile, and fuel quantity per stroke.
5In a common rail two-stroke marine diesel engine (WinGD / Wärtsilä RT-flex), what is the function of the Injection Control Unit (ICU)?
A.It meters the exact quantity of fuel delivered from the 1,000-bar fuel rail to the cylinder injectors using an electronically controlled rail valve and volumetric sensor.
B.It pressurizes the fuel oil from booster pump pressure up to common rail operating pressure.
C.It preheats the heavy fuel oil to achieve the required injection viscosity before admission to the rail.
D.It recirculates unburnt cylinder exhaust gas into the scavenge trunking for Tier III compliance.
Explanation: In WinGD RT-flex common rail engines, the ICU (Injection Control Unit) is mounted adjacent to each cylinder. It contains electro-hydraulic rail valves controlled by the WECS (Wärtsilä Engine Control System) that meter fuel from the high-pressure fuel rail (approx. 1,000 bar) to the injectors. The ICU features an internal free-floating piston and position transmitter that provides precise volumetric feedback of fuel injected per cycle.
6A Chief Engineer observes that a propulsion engine turbocharger suddenly begins to surge violently with rhythmic loud banging noises, heavy air receiver pressure fluctuations, and vibration. What is the fundamental physical cause of turbocharger surging?
A.The compressor discharge air pressure exceeds the pressure capability of the impeller due to reduced mass flow or high downstream backpressure, causing momentary flow reversal through the compressor blades.
B.The turbine wheel overspeed governor has tripped and locked the exhaust gas wastegate valve wide open.
C.Heavy fuel oil has leaked into the turbine casing and ignited, generating a localized acoustic shock wave.
D.The charge air cooler seawater circulating pump has lost suction, leading to an immediate vacuum in the scavenge receiver.
Explanation: Turbocharger surge occurs when the operating point on the compressor performance map crosses the surge line. When the mass airflow through the compressor falls too low relative to the downstream receiver pressure (often due to fouled scavenge ports, fouled air coolers, sudden engine load reduction, or exhaust pulse mismatches), the compressor blades stall aerodynamically. Air then surges backward through the impeller until downstream pressure drops, whereupon normal flow restarts, setting up a destructive cyclic pulsation.
7When analyzing engine combustion using an out-of-phase (90 degrees displaced) indicator diagram (draw card), what specific diagnostic information is most accurately determined compared to a standard power card?
A.The point of fuel injection ignition delay, the rate of initial pressure rise, and the exact value and crank angle of maximum combustion pressure (Pmax).
B.The total indicated power and mean indicated pressure (MIP) developed across the full expansion stroke.
C.The exact flow resistance and backpressure across the exhaust gas economizer tubes.
D.The mechanical friction losses between the piston compression rings and the cylinder liner.
Explanation: On a standard power indicator card, the piston is moving very slowly near top dead center (TDC), so the pressure changes during combustion are compressed into a narrow vertical spike. By shifting the indicator drive 90 degrees out of phase, the indicator drum moves at its maximum linear velocity when the engine piston is at TDC. This spreads out the pressure trace around TDC, allowing precise visual and quantitative evaluation of compression pressure (Pcomp), ignition delay, rate of pressure rise (bar/degree), and peak firing pressure (Pmax).
8What is the primary diagnostic purpose of taking a light-spring indicator diagram on a marine diesel engine?
A.To magnify the low-pressure events of the cycle, enabling detailed inspection of the scavenge air intake, cylinder exhaust blowdown, and pumping losses.
B.To record peak combustion pressures up to 200 bar without damaging the indicator stylus mechanism.
C.To measure fuel injector opening pressure and needle bounce under full load conditions.
D.To calculate the indicated thermal efficiency of the high-pressure expansion line.
Explanation: A light-spring indicator diagram uses a highly flexible spring (with a low spring scale such as 1 mm = 0.1 bar) fitted with a protective stop to prevent damage during high-pressure combustion. Its sole purpose is to magnify the low-pressure gas exchange process near the bottom dead center (exhaust blowdown, scavenging period, and air inlet pressure). It immediately detects fouled exhaust ports, high exhaust backpressure, late exhaust valve opening, or inadequate scavenge pressure.
9When taking crankshaft web deflection measurements on a large propulsion engine, what condition is indicated if the bottom (B) reading is significantly more positive than the top (T) reading (i.e., the web gauge opens wider at the bottom)?
A.The adjacent main bearing journals are lying lower than the outer journals, indicating excessive wear or foundation sagging beneath that crankthrow.
B.The adjacent main bearings are positioned excessively high, indicating an arched or hogging bedplate beneath that crankthrow.
C.The connecting rod small end bearing clearance has completely closed up.
D.The flywheel thrust face is exerting excessive forward axial preload against the bedplate.
Explanation: Crankshaft web deflection gauges measure the distance between adjacent crank webs as the shaft is turned through one revolution. When the webs open out at the bottom (B reading greater than T reading), the crank pin is bowed downward, meaning the main bearings supporting that throw are lower than the adjacent bearings. This indicates excessive wear of the main bearing shells, loose holding-down bolts, or local sagging of the ship's double bottom structure.
10Modern ultra-long-stroke two-stroke marine engines operating with low jacket cooling temperatures are highly susceptible to severe 'cold corrosion' of cylinder liners. What is the fundamental chemical mechanism causing this wear, and what is the primary operational mitigation?
A.Sulfur trioxide (SO3) in combustion gases combines with condensed water vapor below the acid dew point to form sulfuric acid (H2SO4); it is mitigated by matching cylinder oil Base Number (BN) and feed rate, alongside jacket water temperature elevation.
B.Nitric acid (HNO3) condenses on the upper liner surface; it is mitigated by injecting sodium hydroxide into the scavenge air manifold.
C.Unburnt hydrocarbon fuel dilutes cylinder oil on cold liner walls; it is mitigated by dropping scavenge air temperature below 15 degrees Celsius.
D.Vanadium pentoxide fluxes the cylinder liner iron matrix; it is mitigated by installing ceramic thermal barrier sleeves in all cylinder bores.
Explanation: In high-efficiency ultra-long-stroke engines, peak cylinder pressures exceed 180-200 bar, which raises the sulfuric acid dew point to 140-160 degrees Celsius. When liner wall temperatures fall below this dew point, condensed water reacts with sulfur trioxide (SO3) from fuel combustion to form corrosive sulfuric acid (H2SO4). Mitigation requires selecting a cylinder lubricating oil with a matching Base Number (BN) and feed rate to neutralize the acid, combined with load-dependent jacket water preheating (e.g. jacket temperature control at 85-90 degrees Celsius) and scavenge air temperature optimization.

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