Quiz
T-6 Flight Controls
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Fragen in diesem Quiz (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.
- ARichtig
- BFalsch
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.
- ARichtig
- BFalsch
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.
Informationen
- Beschreibung
- T-6/A Texan II Quiz am T-6 Flight Controls, erstellt von Ryan Curtis am 06/12/2018.
- Autor
- Ryan Curtis
- Sprache
- English
- Aufrufe
- 2
- Verlauf
- Erstellt am 6 Dez 2018 · aktualisiert am 7 Dez 2018
- Schlagwörter
- Bewertung
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