Tradewind Aviation Pilatus PC-12 NG Initial Check Practice Test

These questions are part of the practice quiz. Start practicing

• What does the stall warning system utilize to detect stall conditions?
• What is the max operating speed (Vmo/Mmo) of the aircraft?
• Which buses are lost in the event of a GEN 1 or GEN 2 failure?
• How many fuel tanks does the Pilatus PC-12 NG have in total?
• What is the maximum weight for cargo loading in the Pilatus PC-12 NG?
• What could indicate a malfunction in the cabin pressure system based on the altitude readouts?
• What is the key aspect of crew resource management (CRM) for Pilatus PC-12 NG operation?
• What type of electrical system does the Pilatus PC-12 NG utilize?
• What is the amp hour rating of the lead-acid batteries used in the electrical system?
• At what RPM does the CSU maintain the propeller during normal operations?
• What types of weather instruments are present in the Pilatus PC-12 NG?
• What altitude does the CPCS prevent the cabin from exceeding in automatic mode?
• What is the stall warning system in the Pilatus PC-12 NG designed to do?
• Which component is critical to ensure passenger safety in pressurized flight environments?
• At what Ng percentage do secondary fuel nozzles start to occur?
• What is the maximum cabin altitude that can be achieved before the Outflow Valve closes?
• What happens if the High-Pressure Engine-Driven Pump fails?
• What is the typical cruise speed of the Pilatus PC-12 NG?
• Which oxygen flow condition is indicated by the PX Oxygen AUTO setting?
• Which of the following is important for fuel management in the Pilatus PC-12 NG?
• What is the typical cruise altitude for the Pilatus PC-12 NG?
• What is the maximum range of the Pilatus PC-12 NG?
• What does the 3D cam in the aircraft control?
• If the aircraft experiences a GEN failure, how does it maintain control?
• What external feature does the electrical system include for ground operations?
• What is the service ceiling of the Pilatus PC-12 NG?
• What is the primary function of the Negative Pressure Relief Valves?
• What is the purpose of the Air Cycle System in the aircraft?
• Which feature enhances landing performance in the Pilatus PC-12 NG?
• What type of messages can be displayed on the Primary Flight Display (PFD) from the Flight Alert System (FAS)?
• Which generator operates the start motor?
• What is the maximum torque limit for the aircraft?
• Which of the following pumps is NOT found in the Pilatus PC-12 NG fuel system?
• What happens to cabin pressure control if the blow out disk ruptures?
• What safety measure is triggered at a cabin altitude above 13,500 feet?
• Does a FAS message require immediate action?
• What is the location of the Power Junction Box (PJB) in the aircraft?
• What happens to oil when the engine is shut down?
• What procedures should be followed in the event of cabin depressurization in the Pilatus PC-12 NG?
• What is the maximum operating altitude for the Pilatus PC-12 NG?
• What is the width of the aircraft?
• What is the governor limit for prop RPM in the Pilatus PC-12 NG?
• What is the primary function of the High-Pressure Engine-Driven Pump?
• With PX Oxygen in the AUTO position, when will the flow of oxygen begin?
• What indications are shown on the engine display in the Pilatus PC-12 NG?
• What does the acronym ACS stand for?
• What is the operating temperature range for the Pilatus PC-12 NG engine?
• What does the Engine Fire Detection system consist of?
• What is the max wind component for takeoff and landing in the Pilatus PC-12 NG?
• What is the total oil capacity of the system?
• What is lost during a Dual GEN failure?
• What type of landing gear does the Pilatus PC-12 NG have?
• What is the maximum allowable baggage capacity for the Pilatus PC-12 NG?
• What is the limit for fuel imbalance in the Pilatus PC-12 NG indicated by LCD segments?
• What is the maximum landing weight (MLW) of the aircraft?
• When is the Auto-Balance System deactivated in the Pilatus PC-12 NG?
• What type of propeller is used on the Pilatus PC-12 NG?
• If GEN 1 or GEN 2 fails, will all four screens remain functional?
• What is the maximum flap operating speed at Flaps 30-40?
• Does fresh air enter the cabin of the Pilatus PC-12 NG?
• How is cabin temperature controlled in the Pilatus PC-12 NG?
• What is the purpose of the check valves installed in the motive flow line?
• Which statement describes the power section of the PT6A-67P engine?
• What is the Ground Idle Ng percentage?
• Which items are powered under the First Level of Integrity?
• What can be done if the Ng falls below 50% for MOR usage?
• What is the procedure for an engine failure at takeoff in the Pilatus PC-12 NG?
• What is the shaft horsepower of the power plant when detuned?
• What is the maximum continuous power output of the engine in the Pilatus PC-12 NG?
• What is the role of the elevator trim in the Pilatus PC-12 NG?
• What level of integrity results from a dual GEN failure?
• What is the maintenance interval for the Pilatus PC-12 NG?
• Why is it crucial to manage engine temperature during flight in the Pilatus PC-12 NG?
• How can pilots reduce drag during flight in the Pilatus PC-12 NG?
• What is the function of the 2.0 PSI outflow valve in the fuel vent system?
• What is the fuel limit difference in LCD segments for the Auto-Balance System to activate?
• Which bus is NOT affected by a GEN 1 or GEN 2 failure?
• What is the purpose of the Propeller De-Icing System?
• What is the general range of the Pilatus PC-12 NG?
• How does Battery 1 assist with starting the engine?
• Under what condition can the Maximum Operating Range (MOR) be used?
• What are the three positions for the Condition Lever?
• What type of fuel is recommended for the Pilatus PC-12 NG?
• How often should the oil level be checked in relation to shutdown?
• What does the Oil-Fuel Heat Exchanger prevent?
• At what weight is the Vo (Design Maneuvering Speed) 166?
• What is the function of the circuit breakers in the Pilatus PC-12 NG?
• What type of fuel is primarily used in the Pilatus PC-12 NG?
• Where are the Negative Pressure Relief Valves located in the aircraft?
• Which flight control surfaces provide stability in pitch and roll for the Pilatus PC-12 NG?
• When should you use a Ground Power Unit (GPU)?
• What is the capacity of each generator in the 28 Volt DC system?
• What level of integrity is associated with a GEN failure?
• What does CPCS stand for in aviation terminology?
• What is the typical approach configuration for landing in the Pilatus PC-12 NG?
• What is the maximum takeoff weight (MTOW) of the aircraft?
• What are the primary navigation aids in the Pilatus PC-12 NG?
• When are oil levels considered most reliable?
• What type of lighting system is used for the cockpit of the Pilatus PC-12 NG?
• What kind of gear doors does the Pilatus PC-12 NG utilize?
• Which battery is associated with the "HOT BUS"?
• What is the primary purpose of the Pilatus PC-12 NG?
• What is the maximum ramp weight (MRW) of the aircraft?
• What is the maximum allowable dilution ratio for fuel without Prist in the Pilatus PC-12 NG?
• What does the Fuel Control Unit (FCU) respond to during normal operations?
• What is the primary air port for the ACS while in flight?
• How is the aircraft's center of gravity important to the Pilatus PC-12 NG?
• At what altitude does the Outflow Valve close if cabin altitude exceeds a certain limit?
• What condition must the ITT meet prior to engine start?
• During which phase of flight is the ACS primarily utilized?
• By how much does the torque drop for every 10,000 feet in altitude?
• Is it possible to lose the First Level of integrity in the aircraft?
• Does the ACS in the Pilatus PC-12 NG ever draw from both air ports simultaneously?
• Does the Pilatus PC-12 NG have an auto-balance feature for the fuel system?
• What is the role of the Emergency Power System in the Pilatus PC-12 NG?
• At what PSI does the blow out disk rupture in the system?
• Which of the following is a requirement for starting the engine?
• What is the role of the Scavenger Pump in the oil system?
• What Ng percentage is required to rise above for the condition lever to switch to ground idle?
• What landing gear type is featured in the Pilatus PC-12 NG?
• How is cabin pressurization controlled in the Pilatus PC-12 NG?
• What are the functions of the digital engine control (DEC) in the Pilatus PC-12 NG?
• What type of engine powers the Pilatus PC-12 NG?
• What is the maximum zero-fuel weight (MZFW) of the aircraft?
• What happens to the AVIONICS during a Dual GEN failure?
• What is the maximum cargo weight allowed in the aircraft?
• What happens when the oil levels are low within the system?
• What is the purpose of the fuel boost pump in the Pilatus PC-12 NG?
• How many passengers can the Pilatus PC-12 NG typically accommodate in a commuter configuration?
• How does the Pilatus PC-12 NG indicate engine performance?
• Which part is responsible for the reverse flow in the PT6A-67P engine?
• If an item is INOP and not listed in the Minimum Equipment List (MEL), what is the first step?
• How many fuel pumps are installed in the Pilatus PC-12 NG?
• What is the special function of the electrical system in case of failures?
• What role do the flaps play during takeoff in the Pilatus PC-12 NG?
• At what fuel weight difference does the Auto-Balance System activate in the Pilatus PC-12 NG?
• What is the tail height of the aircraft?
• How does the overspeed governor feather the propeller?
• What specific emergency procedures should be followed during a hard landing in the Pilatus PC-12 NG?
• Can a discrepancy log be created while in the air?
• If the engine is at idle and insufficient air is drawn from P2.5, which source is used instead?
• Which pump is responsible for returning oil to the cooler from the reduction gearbox?
• How is the fuel system configured in the Pilatus PC-12 NG?
• What is the primary function of the Pressure Pump in the oil system?
• How long is the aircraft?
• How does the Pilatus PC-12 NG perform in short field takeoff scenarios?
• What might occur if the RPM falls within the prohibited range?
• What is the maximum weight for the aircraft's cargo configuration?
• What checks should be performed before each flight in the Pilatus PC-12 NG?
• What is the recommended approach speed for landings in the Pilatus PC-12 NG?
• What kind of avionics system does the Pilatus PC-12 NG use?
• What does PX Oxygen AUTO signify for pilots regarding altitude management?
• What is the main purpose of the Essential Bus?
• What is the total usable fuel weight in the Pilatus PC-12 NG?
• What is the effect of exceeding a cabin altitude of 15,000 feet without proper oxygen?
• What is likely to happen if the cabin exceeds the CPCS limit of 10,000 feet without intervention?
• At what weight is the Vo (Design Maneuvering Speed) 132?
• What maintenance actions are typically performed on the propeller of the Pilatus PC-12 NG?
• Which battery provides power for engine start in the Pilatus PC-12 NG?
• What is the maximum takeoff weight of the Pilatus PC-12 NG?
• What is the gear width of the aircraft?
• How does the Pilatus PC-12 NG handle asymmetric thrust in-flight?
• What type of emergency descent procedure may be employed in the Pilatus PC-12 NG?
• What is the prohibited RPM range for the engine?
• What is the fuel capacity of the Pilatus PC-12 NG?
• What does the EPS BUS power in the aircraft?
• What is the purpose of the Maximum Operating Range (MOR) in the Pilatus PC-12 NG?
• Which scenario would require the use of P3 air in the Pilatus PC-12 NG?
• What occurs when the fuel temperature falls below 21C?
• If an INOP item is listed in the MEL, what should you do?
• What RPM will the overspeed governor maintain?
• What is the recommended altitude for turbocharging efficiency in the Pilatus PC-12 NG?
• How does the Pilatus PC-12 NG perform during icing conditions?
• What type of oxygen system is equipped on the Pilatus PC-12 NG?
• What component assists with visibility in the cockpit for nighttime operations in the Pilatus PC-12 NG?
• What is the length of the propeller used in the aviation system?
• What is the maximum number of passengers the Pilatus PC-12 NG can accommodate?
• What is the function of the Static Source on the Pilatus PC-12 NG?
• What type of emergency equipment is provided on the Pilatus PC-12 NG?
• What is the purpose of the Outflow Valve in the cabin pressure control system?
• What type of engine is used in the Pilatus PC-12 NG?
• How many fuel nozzles are installed in the Pilatus PC-12 NG?
• Which altitude marking indicates a critical threshold for cabin pressure?
• How much amperage is required from a GPU to run all systems in the Pilatus PC-12 NG?
• What is the consequence of operating the propeller above the governed RPM?
• What does CSU stand for in the context of the propeller?
• What drives the Low-Pressure Engine Driven pump in the Pilatus PC-12 NG?
• What is the function of the Power Junction Box (PJB)?
• How is the Pitot-static system used in the Pilatus PC-12 NG?
• What system is employed in the Pilatus PC-12 NG for monitoring airspeed?
• How can the pilot manage engine power during descent in the Pilatus PC-12 NG?
• What happens when balancing fuel in the Pilatus PC-12 NG?
• What is the maximum Ng percentage during take-off?
• What is the takeoff distance required for the Pilatus PC-12 NG at maximum weight?
• What is the climb rate for the Pilatus PC-12 NG at sea level?
• What is the maximum flap operating speed at Flaps 15?
• What is the primary function of the Ng Governor?
• Where are the fuel drains located in the Pilatus PC-12 NG?
• What is the maximum blade angle range for reverse thrust?
• What is the function of the gear warning system in the Pilatus PC-12 NG?
• What is the landing distance required for the Pilatus PC-12 NG at maximum weight?
• What type of pump does the CSU contain?
• Does the Pilatus PC-12 NG have a wing-to-wing fuel transfer system?
• What is the stall speed in landing configuration for the Pilatus PC-12 NG?
• What type of autopilot system is installed in the Pilatus PC-12 NG?