Test
T-6 Flight Controls
Este test tiene tipos de pregunta que se abren en el reproductor de siempre.
Preguntas del test (24)
1For the aileron system, the aileron trailing edge travel is limited to [blank_start]20[blank_end]° up and [blank_start]11[blank_end]° down.
- A20
- B11
2Each primary flight control surface on the T-6A is "mass balanced." This simply means that the [blank_start]center of gravity[blank_end] of each control surface falls along its [blank_start]pivot[blank_end] or hinge line.
- Acenter of gravity
- Bpivot
3Which of the following is not a part of the aileron control system?
- ALeft and right aileron
- BBellcranks
- CTAD
- Dpush-pull rods
- Efront and rear cockpit control sticks
4For the elevator, the trailing edge deflection is [blank_start]18[blank_end]° up and [blank_start]16[blank_end]° down.
- A18
- B16
5What is the purpose of the bobweight located on the forward control stick?
- AProvides for static balancing of the elevator
- BEnhances control feedback and helps prevent overstressing of the airframe
- CProvides a connection between the two control stick
- DMechanically limits the amount of elevator travel
6Centering springs are installed to provide a tendency for the rudder to return to the neutral position and to enhance control feedback.
- AVerdadero
- BFalso
7The rudder deflection limits are [blank_start]24[blank_end]° in either direction.
- A24
8Rudder pedal position is adjusted with a hand crank located on the
- Alower portion of the center console.
- Bright side of the cockpit.
- Cupper portion of the center console.
- Dleft console.
9The [blank_start]rear[blank_end] cockpit switch has priority in the event of conflicting input trim between the pilots.
- Arear
10In the event of a trim system [blank_start]malfunction[blank_end], a trim interrupt button is available for rapid disconnect of all trim systems
- Amalfunction
11Maximum trim displacement of the [blank_start]ailerons[blank_end] is limited to one aileron at [blank_start]6[blank_end]° trailing edge up, with the opposite aileron at [blank_start]6[blank_end]° trailing edge down.
- Aailerons
- B6
- C6
12Elevator trim tab movement is limited to [blank_start]5.5[blank_end]° up and [blank_start]22[blank_end]° down.
- A5.5
- B22
13Which flight control electromechanical trim system(s) utilize movement of the actual primary control surface?
- AFlaps
- BAileron
- CRudder
- DElevator
14Visual indication of pitch, roll, and yaw trim can be found on the
- Atrim position indicators located on both trim panels.
- BTAD control panel on the center console.
- Ctriple trim indicator on the right instrument panel.
- Dtrim annunciator system.
15A primary purpose of the TAD system is to assist the pilot
- Ain maintaining roll trim.
- Bby maintaining reduced control stick forces.
- Cin maintaining directional trim.
- Din maintaining pitch trim.
16The TAD computes input to the rudder trim system based on
- Aengine torque, airspeed, altitude, and temperature.
- Baltitude, airspeed, pitch rate, and propeller RPM.
- Cengine torque, rudder pedal control forces, and altitude.
- Dengine torque, airspeed, altitude, and pitch rate.
17In addition to the TRIM OFF annunciator, actuating the trim interrupt button will also illuminate the _____ annunciator light.
- ARUDDER INOP
- BNO TRIM
- CTAD OFF
- DELEVATOR FAIL
18The primary aircraft flight controls consist of the
- Aailerons, Trim Aid Device, and elevator.
- Belectromechanical trim system, TAD, ailerons, and rudder.
- Ccontrol stick, PCL, and rudder pedals.
- Dailerons, elevator, and rudder.
19The aileron ground adjustable trim tabs are for maintenance use only and should not be tampered with by the aircrew.
- AVerdadero
- BFalso
20Which statement best describes the purpose of the bobweight attached to the forward control stick?
- AProvides higher stick forces as G-loading increases, helps prevent overstressing the airframe.
- BPrevents aircraft overcontrolling by the Trim Aid Device.
- CProvides increased aileron sensitivity during high speed flight.
- DProvides increased rudder authority during low altitude turns.
21Which of the following is not included in the rudder control system?
- ABellcrank
- BBobweight
- CCables
- DCentering springs
22The Trim Aid Device (TAD) computer relays trim input to the
- Arudder pedals.
- Baileron trim system.
- Crudder trim tab actuator.
- Delevator trim tab actuator.
23The TAD maintains a takeoff trim setting until _____ KIAS and no weight on the wheels.
- A40
- B60
- C80
- D100
24A green TAD OFF annunciator will illuminate when
- Athere is an internal failure of the TAD system.
- Bthere is a failure of the rudder tab actuator.
- Cthe TRIM DISCONNECT switch is placed in the YAW CONNECT position.
- Dthe TRIM AID switch is set to off.
Información
- Descripción
- T-6/A Texan II Test sobre T-6 Flight Controls, creado por Ryan Curtis el 06/12/2018.
- Autor
- Ryan Curtis
- Idioma
- English
- Visitas
- 2
- Historial
- Creado el 6 dic 2018 · actualizado el 7 dic 2018
- Etiquetas
- Valoración
- Aún sin valoraciones Valora este test