Flight Autopilot Control & Guidance Questions PDF

Okay, here's the conversion of the documents and images into a structured markdown format: ### ROP (Runway Overrun Protection) function will | | True | False | | -------------------------------------------------------------------- | :---: | :---: | | deploy automatically the reverse in case of runway too short for landing | | ✓ | | automatically brake in case of runway too short for landing | | ✓ | | warn the crew in case of runway too short for landing | ✓ | | ### TOS (Take-Off Securing) function will | | True | False | | --------------------------------------------------------------- | :---: | :---: | | warn the crew if the take-off is initiated on a taxiway | ✓ | | | display other traffic located on the take-off runway | | ✓ | --- ### BTV (Brake to Vacate) function will : | | True | False | | --------------------------------------------------- | :---: | :---: | | improve Runway Occupation Time (ROT) | ✓ | | | automatically brake until an exit selected by the pilot | ✓ | | ### Autopilot is automatically disengaged in case of | | True | False | | --------------- | :---: | :---: | | A lot of fog | ✓ | | | Computer failures | ✓ | | | Loss of surfaces | ✓ | | | Sensors failures | ✓ | | --- ### The autothrust function | | True | False | | -------------------- | :---: | :---: | | Holds a thrust or a power | ✓ | | | Holds a pitch angle | | ✓ | | Holds a speed or a mach | ✓ | | | Holds a flight path angle | | X | ### The autothrust function | | True | False | | ----------------------------------------------------------------- | :---: | :---: | | AoA protection | ✓ | | | Bank angle protection | | ✓ | | Pitch protection | | X | | The aircraft is protected against stall thanks to | | X | --- ### To engage the autopilot, the pilot uses the push button AP1 or AP2 which is on the... Select one: 1. Stick 2. ECAM 3. FCU✓ 4. PFD Your answer is correct. The correct answer is: FCU --- ### For lateral manual control law, the control objective is Select one: 1. Roll rate✓ 2. Pitch rate 3. Vertical load factor 4. Bank angle Your answer is correct. The correct answer is: Roll rate --- ### Which of the following AP modes forces the thrust to Idle and controls the aircraft speed by adapting the vertical slope Select one: 1. FPA 2. Open Climb 3. Open Descent✓ 4. VS Your answer is correct. The correct answer is: Open Descent --- ### The colour of the Flight Director bars in the PFD is Select one: 1. Blue x 2. Green 3. Red 4. Violet Your answer is incorrect. The correct answer is: Green --- ### What advantages have side-sticks in the AIRBUS family "fly-by-wire” fleet among the following sentences? | | Vraie | Fausse | | ------------------------------------------------------------------------------------------------------- | :----: | :-----: | | The pilot feels in a better way his aircraft and the aerodynamical efforts thanks to the mechanical feedback | | ✓ | | Conception is much easier and allows suppressing complex mechanical mechanisms | ✓ | | | captain can see the first officer inputs and may correct if necessary thank to side-sticks motorisation | | ✓ | | they simplify safety analyses | ✓ | | ### What gains and advantages have the EHA and EBHA actuator among the following sentences? | | Vraie | Fausse | | -------------------------------------------------------------------------------------------- | :----: | :-----: | | Are less problematic because they don't dissipate any heat | | ✓ | | Weight gains at aircraft level thanks to a hydraulic circuit suppression | ✓ | | | Thanks to them, the all hydraulic circuits can be fully removed | | ✓ | | Their weight are light so these actuators are much easier to manipulate during maintenance tasks | ✓ | | --- ### In a hydraulic servocontrol with electric command, the stand-by mode has the following characteristics | | True | False | | ----------------------------------------------------------------------------------------------------------------------------------------- | :---: | :---: | | The solenoid valve is energized and a current control of the servovalve leads to move the surface | | ✓ | | The mode selector valve connects both chambers of the spool of the servocontrol | ✓ | | | The fluid reserve is empty in order to have the right damping of the servocontrol | | ✓ | ### The AOC function Select one: 1. is not used to send position reports to the airline 2. provides the means to optimize cockpit workflow by uplinking from the airline a number of FMS parameters✓ 3. allows exchanges between Aircraft and Air Traffic Control --- ### An RNP (Required Navigation Performance)-capable aircraft is able to Select one: 1. Communicate over voice through datalink 2. Precisely navigate along a pre-defined flight path by using GPS sensors ✓ 3. Is based on the integrity of the radio altimeter --- ### FANS (Future Air Navigatoin) objective is: Select one or more: 1. Reduce crew workload by uploading aircraft performance data X 2. Update meteo model with data receive from the airline operation center 3. To reduce voice congestion Your answer is partially correct. You have selected too many options. The correct answer is: To reduce voice congestion --- ### The acronym 'OOOI': Select one or more 1. Stands for 'Out Off On In' reports ✓ 2. Are sent to the Air Traffic Controllers 3. Is used to pay the pilots Your answer is partially correct. You have correctly selected 1. The correct answers are: Stands for 'Out Off On In' reports, Is used to pay the pilots --- ### The Cost Index is: Select one: 1. the ratio between the (fuel cost + time cost + fixed costs) and the fuel cost. 2. **the ratio between the time cost and the fuel cost.** ✓ 3. the ratio between the fuel cost and the time cost Your answer is correct. The correct answer is: the ratio between the time cost and the fuel cost. --- ### The flight management function is integrated: Select one: 1. In a laptop available in the cockpit and on ground. 2. **In a dedicated avionics equipment on the aircraft.** ✓ 3. In the airline and controller networks Your answer is correct. The correct answer is: In a dedicated avionics equipment on the aircraft. --- ### The CRUISE FLIGHT LEVELS are : Select one: 1. Set by the crew from the Airline Flight Planning and FMS information after ATC clearance. ✓ 2. Provided by the ATC and entered into the FMS by the crew. X 3. Automatically set by the FMS OPTIMUM CRUISE ALT function. Your answer is incorrect. The correct answer is: Set by the crew from the Airline Flight Planning and FMS information after ATC clearance. --- ### The OPTIMUM SPEEDS are: Select one: 1. Computed by the FMS and entered on the FCU by the crew. 2. Provided by the ATC and entered on the FCU by the crew. 3. **Automatically computed by the FMS.** ✓ Your answer is correct. The correct answer is: Automatically computed by the FMS. --- ### How the Top Of Descent point is positioned in the Flight Plan?: Select one: 1. The position is provided by the ATC, then the pilot insert it in the Flight Plan. 2. The position is provided by the Company Route in the NAV Data Base, 3. **The position is computed by the FMS according to descent constraints and the aircraft descent capability.** ✓ Your answer is correct. The correct answer is: The position is computed by the FMS according to descent constraints and the aircraft descent capability. --- ### In flight with a FBW aircraft : 1. In normal law, the aircraft should exceptionaly leave the protected flight envelope. 2. Fly-by-wire aircraft has always an active protection of the flight envelope. 3. Active protections are engaged when a pilot exceed the normal flight envelope. 4. In case of engine failure, alternate law is always active. 5. Alternate law (or secondary law) indicates that some protections are lost. 6. In direct law the flight envelope is not protected. ### The combination of WRONG responses is : Select one: 1. A. 2; 4; 6 2. B. 1; 3; 5 3. **C. 2; 4** 4. D. 1; 2; 3; 5; 6 × Your answer is incorrect. The correct answer is: 2; 4 --- ### The optimum cruise speeds computed by the FMS take into account Select one or more: 1. a. the distance to destination X 2. b. The cost index defined by the Airline ✓ 3. c. The current A/C altitude and weight ✓ Your answer is incorrect. The correct answers are: The current A/C altitude and weight, The cost index defined by the Airline --- ### In the FMS, the performance model is used: Select one or more: 1. a. to optimize the distance between 2 waypoints 2. b. to display the optimum altitude in the cockpit ✓ 3. c. to compute the vertical trajectory in climb and descent phases ✓ Your answer is correct. The correct answers are: to compute the vertical trajectory in climb and descent phases, to display the optimum altitude in the cockpit --- ### The fonctions of the autothrust are: 1. N1 limit computing for engine over limit protection. 2. To maintain selected or managed Speed/Mach. 3. To performs thrust reduction during flare in autoland mode. 4. To ensure protection against excessive angle-of-attack (alpha floor function). 5. Unable to operate independantly of the AP/FD. 6. The A/THR can operate independently or with the AP/FD. 7. To perform automatic reverse selection at landing. 8. To calculate maximum flexible temperature for take off. A) 1; 2; 4; 5; 6; 8 B) 2; 3; 4; 6; 7; 8 C) 3; 4; 5; 6; 7 D) 1; 2; 3; 4; 6 Select one: 1. **D ✓** 2. A 3. C 4. B --- ### The Flight Control Unit or Master Control Panel is used to : A) Send orders to the flight control system.\ B) Send orders to the Autopilot.\ C) To initialize the Flight management Sytem.\ D) To initiate the Flight plan. Select one: 1. D 2. A 3. **B ✓** 4. C Your answer is correct. The correct answer is: B --- ### By pushing the APP push button of the FCU, the pilot, A) Indicates to the FMGS to arm the Localizer only. B) Indicates to capture the ILS (Instrument Landing System). C) Indicates to switch to the Approach mode of the Flight Management System. D) Indicates to cancel the Approach. Select one: 1. C 2. D 3. A × 4. B Your answer is incorrect. The correct answer is: B --- ### The functions of the Autopilot are : 1. Stabilization of the aircraft around the CG. 2. Acquisition and tracking of a flight path. 3. Automatic landing and Go Around.(AUTOLAND) 4. Decrabe at landing 5. Autobrake ### The combination of correct answer are : A) 1; 2; 3; 4; 5 B) 2; 3; 4 C) 1; 2; 4; 5 D) 1; 2; 3; 4 Select one: 1. A 2. C 3. B 4. D --- ### What is the correct affirmation? A) An automatic landing system is fail-passive if, in the event of a failure, there is no significant out-of-trim condition or deviation of flight path or attitude - but the landing is not completed automatically. B) An automatic landing system is fail-passive if, in the event of a failure, there is significant out-of-trim condition or deviation of flight path or attitude - but the landing is completed automatically. C) An automatic landing system is fail-passive if, in the event of a failure, there is significant out-of-trim condition or deviation of flight path or attitude - but the landing is not completed automatically. D) An automatic landing system is fail-passive if, in the event of an engine failure, there is no significant out- of-trim condition or deviation of flight path or attitude - but the landing is not completed automatically. Select one: 1. C 2. B 3. D 4. **A** ✓ ### The flight parameters, which are not displayed on the Primary Flight Display are ? 1. Angle of attack, 2. Vertical speed 3. Roll rate 4. Sideslip 5. Pitch angle. 6. Bank angle, 7. Yaw rate Select one: 1. A. 1; 3; 7 2. 1; 2; 5; 6 3. C. 2; 4; 5; 6; 7 4. D.1; 3; 4; 7 Your answer is incorrect. The correct answer is: 1; 3; 4; 7 --- ### The main characteristic of the normal law of an AIRBUS airplane is : 1. The aircraft maintains the angle of attack when stick is released. 2. The aircraft is autotrimed and maintain attitude when stick is released. 3. When in alternate law ; lowering the landing gear switches the FCS to the direct law. 4. Changing the configuration needs the pilot to change aircrfat attitude. ### The combination of CORRECT answers is : Select one: 1. 2; 3 2. B. 1; 2 x 3. 1; 3 4. D.2; 4 Your answer is incorrect. The correct answer is: 2; 3 --- ### Wat is the correct affirmation ? ### The main characteristic of the Direct law is : Select one: 1. **Autopilot is lost and control surface motion is directly related to the side stick motion** ✓ 2. An artificial feel is introduced in the direct command of the FBW system 3. Control surface motion is directly related to the side stick movement. 4. The autopilot commands directly the control surface Your answer is correct. The correct answer is: Autopilot is lost and control surface motion is directly related to the side stick motion --- ### About the PIO (Pilot induced Oscillations) 1. They are controlable pitch oscillations. 2. They are caused by pilot's efforts to control the aircraft. 3. The are induced by strong crosswind in the landing phases. 4. When there is a 180° of phase shift between pilot's input and aircraft attitude ### The correct affirmations are : Select one: 1. 2; 4 2. 1; 2; 3 3. 1; 2; 3; 4 4. D.2; 3; 4 Your answer is correct. The correct answer is: 2; 4 --- ### What advantages have side-sticks in the AIRBUS family "fly-by-wire” fleet among the following sentences? | | Vraie | Fausse | | ------------------------------------------------------------------------------------------------------- | :----: | :-----: | | Conception is much easier and allows suppressing complex mechanical mechanisms | ✓ | | | They simplify safety analyses | | ✓ | | The pilot feels in a better way his aircraft and the aerodynamical efforts thanks to the mechanical feedback | | ✓ | | captain can see the first officer inputs and may correct if necessary thank to side-sticks motorisation | ✓ | | ### What gains and advantages have the EHA and EBHA actuator among the following sentences? | | Vraie | Fausse | | -------------------------------------------------------------------------------------------- | :----: | :-----: | | Weight gains at aircraft level thanks to a hydraulic circuit suppression | ✓ | | | Their weight are light so these actuators are much easier to manipulate during maintenance tasks | | ✓ | | Thanks to them, the all hydraulic circuits can be fully removed | ✓ | | | Are less problematic because they don't dissipate any heat | | ✓ | --- ### In a hydraulic servocontrol with electric command, the stand-by mode has the following characteristics | | True | False | | ----------------------------------------------------------------------------------------------------------------------------------------- | :---: | :---: | | The solenoid valve is energized and a current control of the servovalve leads to move the surface | | ✓ | | The fluid reserve is empty in order to have the right damping of the servocontrol | ✓ | | | The mode selector valve connects both chambers of the spool of the servocontrol | ✓ | | ### Airport Navigation system provides the crew with | | True | False | | ------------------------------------------------------------ | :---: | :---: | | oral indications to help the crew to navigate during taxi phase | | | | a prediction of the fuel used during taxi phase | | | | an interactive airport map | | | --- ### BTV (Brake to Vacate) function will : | | True | False | | --------------------------------------------------- | :---: | :---: | | improve Runway Occupation Time (ROT) | ✓ | | | automatically brake until an exit selected by the pilot | ✓ | | ### Airport Navigation system provides the crew with: | | True | False | | ------------------------------------------------------------ | :---: | :---: | | an interactive airport map | | | | aural indications to help the crew to navigate during taxi phase | | | | a prediction of the fuel used during taxi phase | | | --- ### ROP (Runway Overrun Protection) function will: | | True | False | | -------------------------------------------------------------------- | :---: | :---: | | warn the crew in case of runway too short for landing | ✓ | | | automatically brake in case of runway too short for landing | | ✓ | | deploy automatically the reverse in case of runway too short for landing | | ✓ | ### BTV (Brake to Vacate) function will : | | True | False | | --------------------------------------------------- | :---: | :---: | | improve Runway Occupation Time (ROT) | | X | | automatically brake until an exit selected by the pilot | | X | both --- ### Concerning the future of airport navigation | | True | False | | ------------------------------------------------------------------------------------------------------- | :----: | :-----: | | none | | X | | all the functions will be provided on EFB - Electronic Flight Bag - as evolution is easier and development costs are lower | | ✓ | | there is no need to compute a trajectory on ground since ATC - Air Traffic Control - clearances are sufficient to navigate on ground | | ✓ | ### TOS (Take-Off Securing) function will | | True | False | | ------------------------------------------------------------------ | :---: | :---: | | warn the crew when the aircraft is about to enter a runway during taxi phase | | X | | display other traffic located on the take-off runway | X | | | warn the crew if the take-off is initiated on a taxiway | ✓ | | --- ### The autothrust function | | True | False | | ----------------------------------------------------- | :---: | :---: | | AoA protection | | | | Pitch protection | | | | The aircraft is protected against stall thanks to | | | | Bank angle protection | | | ### To engage the autopilot, the pilot uses the push button AP1 or AP2 which is on the... Select one: 1. FCU✓ 2. Stick 3. PFD 4. ECAM --- ### The slowest loop is the... Select one: 1. Guidance loop x 2. Actuator loop 3. Navigation loop 4. Control loop The correct answer is: Navigation loop --- ### The fastest loop is the... Select one: 1. Navigation loop 2. **Actuator loop** 3. Guidance loop 4. Control loop × The vertical autopilot mode during a final approach is Select one: 1. Heading mode (HDG) 2. LOC mode (LOC) 3. Vertical speed mode (V/S) 4. **Glide mode (GS)✓** The correct answer is: Glide mode (GS) --- ### For the Autoland function certification, you need to: | | True | False | | -------------------------------------------------- | :---: | :---: | | none of the above | | ✓ | | perform desktop simulations for statistical analysis only | | ✓ | | perform both flight tests and desktop simulations | ✓ | | | perform flight tests only | | ✓ | ### RNP AR procedure can be performed: | | True | False | | :--------------------------------------------------------------------------------------- | :---: | :---: | | in mountainous area only in VFR conditions (excellent visibility) | | ✓ | | in all kind of areas (including challenging ones (mountainous) with no visibility down to decision altitude | ✓ | | | everywhere assuming overflown areas are unpopulated | | ✓ | --- ### FANS (Future Air Navigatoin) objective is: Select one or more: 1. Update meteo model with data receive from the airline operation center 2. Reduce crew workload by uploading aircraft performance data 3. **To reduce voice congestion** ✓ The correct answer is: To reduce voice congestion ### FANS function | | True | False | | ------------------------------------------------------------------ | :---: | :---: | | contribute voice congestion reduction | ✓ | | | provide enhanced surveillance capability over the ocean through ADS-C | ✓ | | | is used to report aircraft position to the airline operation center | | X | --- ### The FMS Datalink function is not used to Select one: 1. downlink periodic position reports to Air Traffic Control 2. uplink the winds data along the planned route 3. **provide a passenger list to the cabin crew** ✓ The correct answer is: provide a passenger list to the cabin crew ### The Automatic Dependent Surveillance – Contract service (ADS-C) Select one: 1. is part of the AOC function 2. allows the aircraft to receive clearance uplinks 3. **provides periodic position reports to the ATC** ✓ The correct answer is: provides periodic position reports to the ATC --- ### The main benefit expected from RNP procedure is to: Select one or more: 1. Offer to the passengers a fantastic view on mountain in a safe manner 2. **Increase Airport access, reduce fuel consumption and improve safety** ✓ 3. Allow free flight operations (reduce Air Traffic Control task) The correct answer is: Increase Airport access, reduce fuel consumption and improve safety ### FANS B: | | True | False | | --------------- | :---: | :---: | | in Europe | | | | over the ocean | | | | is used over ATN network | | | --- ### The term "Datalink" on an aircraft refers to Select one: 1. a database which contains the navigation waypoints 2. **bi-directional data exchanges between the aircraft and ground stations** ✓ 3. the network between the avionics in the aircraft The correct answer is: bi-directional data exchanges between the aircraft and ground stations ### An aircraft certified to operate an RNP AR procedure: | | True | False | | ------------------------------------------------------------------------------------------- | :---: | :---: | | must have cockpit displays designed to be used by the flight crew to monitor the deviations compared to the procedure trajectory | ✓ | | | must have received an Acknowledgment from Cabin Crew to proceed (AR=Acknowledgment Required) | | ✓ | | must not exceed a given size and weight | | ✓ | --- ### What are the aircraft failures taken into account by the FMS for the predictions: Select one: 1. **Only engine(s) failure(s),** ✓ 2. Engine(s) failure(s) + landing gear jamming, 3. No aircraft failure, The correct answer is: Only engine(s) failure(s), --- ### The flight management function is integrated: Select one: 1. In a laptop available in the cockpit and on ground. 2. In the airline and controller networks 3. **In a dedicated avionics equipment on the aircraft.** ✓ The correct answer is: In a dedicated avionics equipment on the aircraft. --- ### An offset lateral revision can be used: Select one: 1. Without asking the Air Traffic Control 2. to create informative waypoints for the pilotsWhen modification are published by authorities.When modification are published by authorities. 3. **To avoid weather phenomena** ✓ The correct answer is: To avoid weather phenomena --- ### The OPTIMUM SPEEDS criteria in all engine operative is: Select one: 1. to provide the minimum fuel consumption on the trip. 2. to maximize the traffic flow on the route. 3. **to provide the minimum operating cost on the trip.** ✓ The correct answer is: to provide the minimum operating cost on the trip. ### On the FMS, the Aircraft Performance Data are: Select one: 1. **Provided by a specific data base downloaded on the FMS system.** 2. Included in the Navigation Data Base. 3. Included into the FMS software and frozen before the Aircraft certification. x The correct answer is: Provided by a specific data base downloaded on the FMS system. --- ### In descent, what "Too Steep segment" means ?: Select one: 1. It can be flown with some airbrakes defection, 2. It can be flown only with full airbrakes defection, 3. **It can't be flown even with full airbrakes defection,** ✓ The correct answer is: It can't be flown even with full airbrakes defection, ### The vertical flight path is computed by: Select one: 1. the Airline's ground tools and uploaded into the FMS by ACCARS. 2. the ATC and uploaded into the FMS by ACCARS. 3. **the FMS according to ATC constraints and the aircraft performance characteristics.** --- ### On Airbus aircraft: the Take Off speeds V1, Vr, V2 are: Select one: 1. the Airline's ground tools and uploaded into the FMS by ACCARS. 2. Provided by the ATC according to the runway characteristics. 3. **Computed by the Airline according to the Aircraft Flight Manual and the runway characteristics.** ✓ The correct answer is: Computed by the Airline according to the Aircraft Flight Manual and the runway characteristics. --- ### ROP (Runway Overrun Protection) function will | | True | False | | -------------------------------------------------------------------- | :---: | :---: | | warn the crew in case of runway too short for landing | ✓ | | | automatically brake in case of runway too short for landing | | X | | deploy automatically the reverse in case of runway too short for landing | ✓ | | ### TOS (Take-Off Securing) function will | | True | False | | -------------------------------------------------------------- | :---: | :---: | | warn the crew if the take-off is initiated on a taxiway | ✓ | | | display other traffic located on the take-off runway | | X | --- ### Airport Navigation system provides the crew with: True False | | True | | ------------------------------------------------------------ | :---: | | aural indications to help the crew to navigate during taxi phase | | | an interactive airport map | | | a prediction of the fuel used during taxi phase | | ### ROP (Runway Overrun Protection) function will: True False | | True | False | | -------------------------------------------------------------------- | :---: | :---: | | deploy automatically the reverse in case of runway too short for landing | | ✓ | | automatically brake in case of runway too short for landing | x | | | warn the crew in case of runway too short for landing | ✓ | | --- ### TOS (Take-Off Securing) function will | | True | False | | ------------------------------------------------------------------ | :---: | :---: | | warn the crew when the aircraft is about to enter a runway during taxi phase | × | | | display other traffic located on the take-off runway | X | | | warn the crew if the take-off is initiated on a taxiway | ✓ | | ### BTV (Brake to Vacate) function will : | | True | False | | --------------------------------------------------- | :---: | :---: | | automatically brake until an exit selected by the pilot |X | | | both | ✓ | | | improve Runway Occupation Time (ROT) | X | | --- ### Concerning the future of airport navigation True False | | True | False | | ------------------------------------------------------------------------------------------------------- | :----: | :-----: | | none | | x | | all the functions will be provided on EFB - Electronic Flight Bag - as evolution is easier and development costs are lower | X | | | there is no need to compute a trajectory on ground since ATC - Air Traffic Control - clearances are sufficient to navigate on ground | | ✓ | ### TOS (Take-Off Securing) function will | | True | False | | ------------------------------------------------------------------ | :---: | :---: | | warn the crew if the take-off is initiated on a taxiway | ✓ | | | warn the crew when the aircraft is about to enter a runway during taxi phase | X | | | display other traffic located on the take-off runway | | ✓ | --- ### The autothrust function | | True | False | | ------------------------------------------------- | :---: | :---: | | Pitch protection | | | | AoA protection | | | | The aircraft is protected against stall thanks to | | | | Bank angle protection | | | ### To engage the autopilot, the pilot uses the push button AP1 or AP2 which is on the... Select one: 1. **FCU** 2. ECAM 3. Stick 4. PFD --- ### The slowest loop is the... Select one: 1. Control loop 2. Actuator loop 3. **Navigation loop**✓ 4. Guidance loop --- ### The fastest loop is the... Select one: 1. Control loop 2. **Actuator loop** 3. Guidance loop 4. Navigation loop The vertical autopilot mode during a final approach is Select one: 1. LOC mode (LOC) 2. Vertical speed mode (V/S) 3. **Glide mode (GS)** ✓ 4. Heading mode (HDG) --- ### For the Autoland function certification, you need to: | | True | False | | ------------------------------------------------------ | :---: | :---: | | none of the above | | ✓ | | perform both flight tests and desktop simulations | ✓ | | | perform desktop simulations for statistical analysis only | | ✓ | | perform flight tests only | | ✓ | ### RNP AR procedure can be performed: | | True | False | | --------------------------------------------------------------------------------------------------------- | :---: | :---: | | in all kind of areas (including challenging ones (mountainous) with no visibility down to decision altitude) | ✓ | | | in mountainous area only in VFR conditions (excellent visibility) | | ✓ | | everywhere assuming overflown areas are unpopulated | | ✓ | --- ### FANS (Future Air Navigatoin) objective is: Select one or more: 1. Reduce crew workload by uploading aircraft performance data 2. **To reduce voice congestion** ✓ 3. Update meteo model with data receive from the airline operation center ### FANS function | | True | False | | ----------------------------------------------------------------- | :---: | :---: | | contribute voice congestion reduction | | ✓ | | provide enhanced surveillance capability over the ocean through ADS-C | ✓ | | | is used to report aircraft position to the airline operation center | | X | --- ### The FMS Datalink function is not used to Select one: 1. **provide a passenger list to the cabin crew** ✓ 2. uplink the winds data along the planned route 3. downlink periodic position reports to Air Traffic Control ### The Automatic Dependent Surveillance – Contract

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