T-54A Systems Practice Exam

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• What is the maximum generator load allowed on the ground for the T-54A?
• What is the wingspan of the T-54?
• What is the maximum operating altitude for the T-54?
• Which of the following is true regarding the manual extension of the landing gear?
• What is required for the auxiliary tank Jet Pump to operate normally?
• Which components are affected by the CAS system in the aircraft?
• Which statement about the Firewall Shutoff Valve is true?
• Can a pilot over-torque the engine above 2230 ft-lb with the autothrottles engaged and pneumatic torque-limiters operative?
• Which of the following statements regarding Reverse operation is incorrect?
• Where is the go-around button located?
• What is the maximum flaps extension speed (VFE) for the T-54A?
• What should be done if the start ITT exceeds 830 degrees Celsius?
• Which of the following selections cannot be made individually by each pilot?
• When will the rudder boost system disengage in the T-54A?
• What is the purpose of the separate hydraulic lines in the T-54A?
• How is the electrical system of the T-54A commonly referred to?
• What is the length of the T-54?
• What is a potential cause of engine flameout in the T-54?
• If the left starter is accidentally turned on during flight, what will happen?
• Pneumatic bleed air is NOT used to operate which of the following?
• At what altitude can explosive decompression become most dangerous?
• What type of components does the hot battery bus provide power to with the battery switch off?
• Which NAVAID cannot be used as a NAV source on the T-54?
• What is the acceleration limitation for flaps up in the T-54A?
• What is an incorrect statement about the reversionary panel?
• What is the maximum generator load above FL310?
• Which surface does not have manually operated trim tabs installed?
• At what altitude does the red Cabin Alt High CAS message illuminate?
• What happens if all engine oil dumps out of the reduction gear box on the T-54A?
• Which of the following is NOT a flight director lateral mode?
• At what altitude does the red Cabin Alt High CAS message illuminate?
• What is the minimum N1 at low idle?
• What is the maximum torque in ft-lb that the engine can handle with the autothrottles and pneumatic torque-limiters operative?
• What does it indicate if the crew is alerted during flight?
• Will the T54 automatically alert pilots to a cabin altitude above 10,000 ft?
• What is true about the T-54A's configuration concerning flotation gear?
• What will happen if the autothrottles are engaged during a manual drop in thrust?
• What is the purpose of the oil-to-fuel heat exchanger?
• What does VSSE stand for?
• Which statement accurately describes the purpose of the ground fine range in aircraft operation?
• What does a voltage reading of 24V indicate after starting the left engine?
• How is the aircraft exterior lighting controlled?
• At a cabin pressure altitude of 12,500 feet, what happens?
• On the ground with the air conditioning running, what is the minimum N1 limit on the right engine with generator load under 80%?
• What type of indicator is unnecessary for the Engine Air Inlet Ice Protection system?
• What is the Prop RPM Red display maximum range with the associated "Left or right engine" aural cue?
• Which capability does the CDI have on NDB approaches in the T-54?
• Which statement regarding VMCA assumptions is incorrect?
• Will Rudder Boost function with bleed air valves in ENVIR OFF?
• At what oil temperature range is normal oil pressure achieved at altitudes below 21,000 feet?
• What is the role of the VOR/LOC/TAC CDI Course in navigation?
• What is the maximum allowed ITT for cruise climb in the T-54A?
• What controls the deployment of passenger oxygen masks?
• What does a dual current limiter failure indicate in flight if multiple systems fail?
• How many fire extinguishers are accessible by the crew in the aircraft cabin?
• What is the consequence of selecting "Both A and E" regarding the T-54 systems?
• When a new CAS message appears on a display, where will it be positioned?
• According to T-54A operating procedures, how many different DMEs can a pilot display on their PFD?
• What happens to the fuel pressure when the standby fuel pump is off?
• What aspect of flight may require the use of hydraulic pressure systems?
• What is the total usable fuel capacity of the T-54?
• When can you safely perform crossfeeding of fuel in flight?
• When should the Autothrottle AIRSPEED mode be used?
• Which operating mode does not have separate hydraulic lines for the T-54A?
• At what altitude does TAKEOFF mode switch to CLIMB mode when climbing with autothrottles engaged?
• What is the Vmca for the T-54 when the flaps are in approach position?
• In terms of pressure management, what component is essential for maintaining cabin pressure in the T-54A?
• Which of the following systems includes the option for SVS On or Off?
• When can landing gear be successfully extended normally?
• During takeoff, if the airspeed is below VMCG, which statement is correct?
• What does an amber light illuminated on the SDU switch panel indicate?
• What does an L-R DC Generator CAS message indicate?
• What is pneumatic bleed air used to operate?
• What outcome may occur from setting the propeller levers incorrectly?
• What does the battery ammeter reading help the crew monitor?
• Under which condition should stall heat be used?
• How are the pilot's controls for exterior lighting described?
• Is it permissible to take off with the Auto-Throttles inoperative according to NATOPS?
• If the overspeed governor fails while the primary governor is operating, what will happen?
• When the Pilot's Static Port is clogged, which of the following will happen to the airspeed?
• If the pilot's static port is blocked, which selection is needed to resolve ADS indication without indicated errors?
• If the maximum takeoff weight has been achieved, how much fuel must be burned to avoid exceeding max landing weight?
• Is UHF guard frequency normally monitored via the Canyon radio?
• Which function is NOT handled by the Flight Director?
• True or False: The propeller levers are directly connected to the Primary Prop Governor and set Prop RPM between 1600-2000.
• Where is the landing gear alternate extension handle located?
• Under which condition is Autothrottle ICE mode active?
• Which is the correct list of flight director vertical modes?
• Does the SDU battery provide backup power to NAV 1?
• Which of the following is a function of the navigation source during nav to nav transfer?
• Is the rudder boost system operational with the bleed air switch set to ENVIR OFF?
• When will CAS messages remain displayed?
• For crossfeed operations, what must be done with the standby fuel pump switch?
• Which aircraft system does NOT receive hydraulic pressure in the T-54?
• What will illuminate if the right starter is accidentally turned on in flight?
• What is an indication that the landing gear warning horn should activate?
• In the event of a clogged static port in a constant speed climb, how will the VSI behave?
• What is indicated by the NO TRANSFER light in the fuel system?
• Which of the following statements is true regarding engine oil pressure during acceleration?
• When will the autothrottle system automatically disengage?
• What does Autothrottle Guard mode prevent?
• What is needed for a safe approach when there is a crosswind component of 22 KIAS?
• What can be restored when the Master Power CB is pulled?
• With a Primary Governor Failure, what may happen to the prop RPM?
• Is the aircraft capable of maintaining its systems while in ENVIR OFF?
• What is the maximum demonstrated tailwind component during approach and landing?
• Which compressor type is more efficient at lower N1?
• What occurs if the propeller linkage fails?
• For maximum cooling on the ground in the T-54A, what should be set?
• What does the term "Baro Mins" refer to in the context of aviation?
• What should you do if you observe fluctuating oil pressure readings?
• What is the true statement about the pneumatics in the T-54?
• What does a fuel press message indicate?
• What is the maximum N1 setting during reverse operation?
• What is the battery rating for the T-54A?
• Will the left generator turn on if the gen voltage reads 24V after engine start?
• Which statement about the static system on the T-54 is accurate?
• How is high idle N1 determined for the T-54A?
• What type of power operates the standby boost pumps in the T-54A?
• What action should be taken if the oil pressure drops below 60 psi?
• What is the minimum N1 limit for the right engine when on the ground with air conditioning off and generator load less than 80%?
• Which trim tab is known as the anti-servo?
• What is the purpose of the T54 oil system?
• Which statement is true regarding ground power connected to the aircraft?
• What are the starter limitations for engine starting?
• Which indicator will show 'Zero' when the static port is clogged and during a constant speed climb?
• What condition prohibits takeoff regarding fuel quantity gauges?
• In case of a mismatch between flap positions, what happens?
• What should be the status of the Bleed Air Valves for maximum cooling on the T-54A?
• What is the correct rating for the Battery in amp/hrs?
• What do the Generator Control Units provide?
• What condition is required for the activation of the autofeather system?
• Which system utilizes the transponder information?
• When can the autofeather switch be armed?
• What system does the anti-servo tab help control?
• What is the value of maximum torque on takeoff?
• What is the result if the Yaw Damp is inoperative?
• To operate incorrectly in a go-around situation, which button would be essential to locate?
• What is indicated if the Hot Battery bus is still functional with the battery switch off?
• In the T-54A, what action is prohibited in case of a fuel imbalance during flight greater than 1,000 pounds?
• What happens when the autothrottle is disengaged regarding Guard protection?
• What is the normal voltage range regulated by the Generator Control Units?
• Which altitude triggers the illumination of the red Cabin Alt High CAS message?
• What is the minimum N1 at high idle for the T-54A?
• In the event of a complete loss of hydraulic fluid, what happens to the landing gear?
• What is the maximum crosswind component on landing for the T-54A?
• What is indicated when the prop RPM gauge enters the Yellow Display Caution Range?
• What does the ALT knob on the Flight Guidance Panel (FGP) set?
• What is the Bleed Air Valve switch position that allows the aircraft to pressurize?
• During which condition is the pilot required to monitor the engine RPM closely?
• Where can the generator and battery load gauges be found?
• Where does the hydraulic power for the landing gear come from in the T-54A?
• During high altitude operations, what can cabin altitude reach without alerting flight crew?
• Which component is responsible for indicating wind direction in the T-54?
• At what cabin pressure altitude will passenger oxygen masks deploy?
• What is the purpose of the rudder boost system in flight?
• Which airspeed should be used when climbing with two engines over an obstacle?
• What happens to prop RPM and torque if the primary governor fails?
• Is it true that an engine can run up to 10 hours with a fuel pump failure if electric power is available?
• Which of the following is true regarding the standby fuel pump?
• Which trim on the T-54A is designated as antiservo?
• Which cockpit switch enables AC power to cabin outlets?
• Which of the following maneuvers are approved for the T-54A?
• How are the landing gear on the T-54A controlled and actuated?
• What is the function of the negative pressure relief valve?
• How is the nose gear locked in the down position?
• Which circuit breakers should not be attempted to reset?
• How should the auxiliary tanks be filled when refueling the T-54A?
• What is the appropriate airspeed to use when climbing with one engine inoperative, without obstacles?
• When should the rudder boost system be turned off?
• What is the maximum demonstrated crosswind limitation?
• What happens when the left engine flames out at FL270 with AP/AT engaged in speed mode?
• What is the function of the T-54A oil system?
• What does a L-DC generator CAS message indicate?
• What happens if Baro Mins is reached during an approach?
• Where is the landing gear warning horn silence button located for the right seat pilot?
• When refueling the T-54A, which tanks should be filled first?
• Which system must remain operational for generator checks?
• What must be activated to use the toilet on the aircraft?
• What is true about the battery ammeter on the overhead panel?
• Under what condition should the autothrottle be disengaged?
• What happens when the Go-Around button is pressed on the left power lever?
• If the Primary Prop Governor fails, what could happen to the prop RPM?
• Which switch controls the flush mechanism for the aircraft toilet?
• What is the maximum ITT permissible on takeoff?
• What is the outcome of operating propellers in reverse range?
• How can a pilot check the voltage on the battery of the T-54A?
• How many VHF capable radios are found on the T-54?
• If the prop advance happens, what is true regarding the power levers during a governor failure?
• What is the minimum aircraft battery voltage when using a GPU for start?
• What is the function of the vertical stabilizer de-ice in the T-54 aircraft?
• What occurs to the cabin altitude without alerts during high elevation mode?
• Operating propellers in the reverse range resets what aspect of the fuel system?
• Which tanks should be filled first when refueling the T-54?
• Under which conditions should the parking brake not be set?
• What is Vyse for the T-54?
• What is the maximum cabin-atmosphere differential that the aircraft pressurization system will maintain?
• What does the FURN switch control in the cockpit?
• Can the extension handle be used for retraction after practice emergency gear extension?
• Which of the following describes a scenario preventing engine oil pressure drop in the T-54A?
• What mode does the autothrottle ENGINE-OUT Mode operate in to maintain maximum torque on the remaining engine?
• What should pilots monitor closely to prevent engine flameout?
• Which statement is true regarding the illumination of the Cabin Alt High CAS message?
• What is displayed in the Flight Mode Annunciation (FMA) field on the PFDs?
• Where are the cabin fire extinguishers located?
• What could indicate an exceeding of NATOPS limits during engine start?
• What action should be taken when the Door Unlocked CAS message illuminates?
• Where is the SDU located on the aircraft?
• What color is a CAS warning message?
• Under what conditions can the landing gear warning horn silence button be operated?
• What does the presence of a blown current limiter indicate in the aircraft?
• Which system does T-54A hydraulics not support?
• Which component is responsible for overpressure relief in the T-54A?
• What happens to the prop RPM after 5 minutes of flying?
• What do the condition levers do when the power levers are at flight idle?
• Which flight director lateral mode arms vertical guidance?
• What should be avoided during turbulent air penetration?
• Where are the aircraft's exterior lighting controls located?
• What is the oil capacity of the T-54A engine oil system?
• What method is used for de-icing the leading edge wing and horizontal stabilizer surfaces?
• Which mode is responsible for providing lateral navigation guidance?
• What N1 percentage indicates normal oil pressure under specified temperature conditions?
• What is the height of the T-54?
• When will the crew be alerted concerning cabin masks?
• What does the anti-icing system for the leading edge engine inlet utilize?
• Is it possible to monitor COM1, COM2, and the Canyon radio simultaneously?
• What is the purpose of propeller deicing boots?
• What is the function of mechanical pins in landing gear systems?
• Which component could be tested using loadmeters on the T-54A?
• What is the maximum allowable g-force when flaps are down in the T-54A?
• What may occur if the fuel dump exceeds 1,000 pounds in flight?
• What can happen if there is insufficient weight on the right main landing gear squat switch during ground roll?
• Which flight mode is associated with vertical speed adjustments?
• How does the pilot know if the prop amps are operational?
• If the maximum extended airspeed limit is 181 KIAS, what must be ensured before extending the gear?
• What is the maximum landing gear extension speed for the T-54A?
• What is the maximum landing gear retraction speed (VLO)?
• What type of conditions does Autothrottle ICE mode specifically respond to?
• A flashing master warning light will remain illuminated until which condition is met?
• What must passengers do when explosive decompression occurs?
• What should be done prior to introducing fuel during Battery Start?
• What is the status of cockpit USB-C chargers when the furnishing switch is off?
• When does the landing gear warning horn sound normally?
• What condition deactivates autofeather for the left engine when armed?
• What range of oil pressure in flight is considered undesirable?
• What is the total fuel capacity of the T-54?
• True or False: The go-around mode disengages the Auto-Pilot but maintains yaw damp and auto-throttles.
• Which statement about the gear motor circuit breaker (CB) is incorrect?
• True or False: Longer than 2-3 second actuations of the Man Temp INCR/DECR switch at shorter than 60 second intervals may lead to a bleed air failure.
• Can the aircraft still pressurize with bleed air valves in ENVIR OFF?
• At what speed should the landing gear be fully extended according to T-54A standards?
• Which equipment affects the accuracy of the standby magnetic compass?
• What is the T-54A's length?
• True or False: Explosive decompression does not affect all passengers onboard.
• What is the correct rating for the Generators in amps?
• What is the role of the propeller governor in the T-54 aircraft?
• What does a loadmeter indicate?
• How are active and armed flight director modes displayed?
• Which engine should be started first when using a GPU for start?
• What must be done if the left engine is out and AP/AT is engaged?
• What is the maximum g-force allowed for level banked turns at greater than 2.0g?
• Which feature is specifically designed to limit overspeed in the autothrottle system?
• What color is a CAS caution message?
• Which items are included in the hot battery bus?
• If the Yaw Damp is inoperative, what is the maximum operating altitude for the T-54?
• Which three autothrottle modes provide engine-out protection?
• What should be checked during the climb checklist regarding the rudder boost system?
• How are the main landing gear locked in the down position?
• What happens to the rudder boost system when the ENVIR switch is turned off?
• Which of the following actions can be performed by the Generator Control Units?
• What occurs if the red Cabin Alt High CAS message is illuminated?
• To guarantee 30 minutes of battery power in case of dual generator failure, the battery amps on takeoff must be:
• What is the function of the Heading Bug in aviation systems?
• Which of the following is NOT included in the pedestal controls for Fusion systems?
• Is it true that the ice light switch only illuminates the leading edge of the left wing?
• What should be done if engine out mode is activated?
• Is the T-54 capable of conducting an NDB approach?
• What is the primary purpose of the condition levers during operation?
• What is indicated by a normal oil pressure range in the T-54A?
• What is the normal range for pneumatic pressure?
• What is the role of an oil heat exchanger in the T-54A?
• What is the capability of each Starter/Generator on the T-54A?
• What is the minimum required voltage for the aircraft battery when ground power is connected?
• From where does hydraulic power for the landing gear come?
• What is considered unsafe in flight regarding oil pressure?
• What is the main concern when the standby magnetic compass is used with powered equipment?
• Which system indicates the operational status of the left generator?
• Which scenario leads to an automatic switch from TAKEOFF to CLIMB mode?
• What component is used for preheating fuel in the T-54A?
• What is the prop de-ice functionality in the T-54 aircraft?
• What is indicated by the aircraft loadmeter during routine operations?
• Which aircraft system might impact the performance of the T-54 during high-speed flight?
• What happens to fuel before entering the combustion chamber in a T54 system?
• What is the consequence of oil pressure falling below the safety threshold during flight?
• Which of the following is NOT a component of the aircraft's pneumatic system?
• If the yaw damper is inoperative, what is the implication?
• What is the maximum weight allowed in the baggage compartment of the T-54A?
• In the T-54, when operating with high-speed maneuvers, which system is critical for stability?
• What might a DC Volt/Loadmeter indicating 0 or 24 volts after starting the left engine signify?
• What is the consequence of having bleed air valves in ENVIR OFF during flight?
• What does a manual control of the prop feather indicate?
• During flight operations, the hydraulic pressure system is utilized for which of the following?
• What does the Autothrottle system ensure during a go-around?
• What airspeed should be used for turbulent air penetration?
• What does the power lever setting indicate for autofeather system activation?
• What is the maximum maneuvering airspeed (Va) in KIAS and the turbulent air penetration speed for the T-54A?
• Which of the following maneuvers is prohibited for the T-54A?
• What system provides terrain avoidance for the T-54A?
• What is the VMCA for the T-54?
• What happens if a prop on the T-54 goes overspeed beyond 2120 RPM and is feathered?
• What is the maximum landing weight of the T-54A?
• If a DC Volt/Loadmeter indicates 28 volts after starting the left engine, what might this indicate?
• What action must be taken to extinguish the ACK GUARD DISCONNECT message?
• What occurs if the prop linkage fails in the T-54?
• How is negative pressure relief accomplished in the T-54A?
• How are the flaps on the T-54A controlled?
• How long after disengaging auto-throttle is Guard Mode available?
• If a NO TRANSFER light illuminates while fuel is still available in the AUX tank, what is the first step in the emergency procedures?
• What components does the Hot Battery bus provide power to with the battery switch off?
• In what condition will the cabin become pressurized according to the air pressure management system?
• Which bug is an individual selection option for pilots in the T-54 system?
• What is the primary function of the ground heat bus in the aircraft?
• Can the T-54 accelerate on centerline with just aileron and rudder during an engine failure before 84 KIAS?
• What is the maximum continuous power for torque in the T-54A?
• What is the ITT limit for Autothrottle CLIMB Mode?