2A852 CDC Volume 5

71 Questions | By Mkenney886 | Last updated: Mar 21, 2022 | Total Attempts: 88

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1.

The pilot’s elevator input system is connected to the
- A.
  
  Outboard elevators
- B.
  
  Inboard elevators
- C.
  
  Upper rudder
- D.
  
  Lower rudder
2.

The copilot’s elevator input system is connected to the
- A.
  
  Outboard elevators
- B.
  
  Inboard elevators
- C.
  
  Upper rudder
- D.
  
  Lower rudder
3.

Control of the aircraft in the yaw axis is accomplished by the
- A.
  
  Elevators
- B.
  
  Ailerons
- C.
  
  Rudders
- D.
  
  Spoilers
4.

What type of cable system does the rudder input system incorporate that run from the flight station to the upper and lower rudder servo input quadrants?
- A.
  
  Triple cable system.
- B.
  
  Single cable system.
- C.
  
  Double cable system.
- D.
  
  Quadruple cable system
5.

When are leading-edge slats and trailing-edge flaps used
- A.
  
  Coordinated turns.
- B.
  
  Landings and takeoffs
- C.
  
  Aileron augmentation
- D.
  
  Pitch and yaw maneuvers
6.

The slat surface is extended and retracted by
- A.
  
  Two telescoping ballscrew actuators.
- B.
  
  Three telescoping ballscrew actuators
- C.
  
  Two variable slat drive roller carriages
- D.
  
  Three variable slat drive roller carriages
7.

The flap and slat power package receives hydraulic pressure from the
- A.
  
  Number one and number two hydraulic systems
- B.
  
  Number one and number four hydraulic systems
- C.
  
  Number two and number four hydraulic systems
- D.
  
  Number two and number three hydraulic systems
8.

What is not included in the mechanical flight control system?
- A.
  
  Cables.
- B.
  
  Torque tubes
- C.
  
  Push-pull tubes
- D.
  
  Electrically powered actuators.
9.

Some aircraft incorporate flight control systems that automatically revert to servo-tab control
- A.
  
  In case of total electrical system failure
- B.
  
  In case of total hydraulic system failure
- C.
  
  To limit the external wind forces from damaging the aircraft while it is parked.
- D.
  
  To limit the external wind forces from damaging the aircraft while it is tied down.
10.

Hydraulic powered actuators convert hydraulic pressure into
- A.
  
  Control surface movements
- B.
  
  Artificial stall warning.
- C.
  
  Gust lock limit
- D.
  
  Fly-by-wire.
11.

Artificial feel systems provide
- A.
  
  Increased resistance to the flight controls at lower speeds
- B.
  
  Decreased resistance to the flight controls at lower speeds.
- C.
  
  Increased resistance to the flight controls at higher speeds
- D.
  
  Decreased resistance to the flight controls at higher speeds
12.

Electronic flight control computers can be programmed to prevent undesirable and dangerous characteristics, such as
- A.
  
  Stalling.
- B.
  
  Gust lock.
- C.
  
  Aileron trim.
- D.
  
  Artificial feel.
13.

On the horizontal stabilizer pitch trim system, hydraulic motor torque is transferred to the nut and screw drives through a
- A.
  
  Step-down transformer
- B.
  
  Torque synchro
- C.
  
  Gear train.
- D.
  
  Lever.
14.

With flaps up, limit switches cut off electrical power to the screw drive unit when the horizontal stabilizer reaches
- A.
  
  1.5° aircraft NOSE DOWN or 6.0° aircraft NOSE UP
- B.
  
  1.5° aircraft NOSE DOWN or 8.0° aircraft NOSE UP.
- C.
  
  2.5° aircraft NOSE DOWN or 6.0° aircraft NOSE UP.
- D.
  
  2.5° aircraft NOSE DOWN or 8.0° aircraft NOSE UP.
15.

What is energized by simultaneous actuation of the horizontal stabilizer trim control wheel switches?
- A.
  
  Flap direction solenoid
- B.
  
  Trim direction solenoid
- C.
  
  Rudder direction solenoid
- D.
  
  Aileron direction solenoid.
16.

Horizontal stabilizer pitch trim, console switches provide a means of operating the actuator
- A.
  
  Generator drive.
- B.
  
  Synchro drive
- C.
  
  Screw drive.
- D.
  
  Nut drive.
17.

Pitch trim position is displayed by a dial-type indicator, incorporating a scale graduated in degrees from
- A.
  
  –5° to +15°.
- B.
  
  –6° to +14°.
- C.
  
  –7° to +13°.
- D.
  
  –8° to +12°.
18.

The pitch trim actuator screw drive and nut drive receive hydraulic power from
- A.
  
  Two hydraulic systems operating at 2000 pounds per square inch (PSI).
- B.
  
  Two hydraulic systems operating at 3000 pounds per square inch (PSI).
- C.
  
  Three hydraulic systems operating at 2000 pounds per square inch (PSI).
- D.
  
  Three hydraulic systems operating at 3000 pounds per square inch (PSI).
19.

What flight control surface indicator is designed to display percentage of surface extension?
- A.
  
  Flap position indicator
- B.
  
  Rudder trim position indicator
- C.
  
  Aileron trim position indicator
- D.
  
  Horizontal stabilizer trim position indicator
20.

Synchro position indicating systems convert mechanical shaft angles to
- A.
  
  Mechanical shaft degrees
- B.
  
  Electrical shaft degrees
- C.
  
  Mechanical signals.
- D.
  
  Electrical signals
21.

What type of operating power is required by a selsyn position indicating system?
- A.
  
  26 VAC.
- B.
  
  28 VDC.
- C.
  
  115 VAC.
- D.
  
  120 VDC.
22.

The selsyn position indicating system transmitter consists of a circular resistance winding with three taps positioned how many degrees apart?
- A.
  
  45
- B.
  
  90
- C.
  
  120
- D.
  
  180
23.

Manual pitch and roll axis attitude adjustments are allowed by the
- A.
  
  Flight control augmentation system (FCAS).
- B.
  
  Stability augmentation system (SAS).
- C.
  
  Flight management system (FMS).
- D.
  
  Flight control set (FCS).
24.

The flight control set (FCS) roll axis must be engaged for selection of heading select (HDG SEL) or
- A.
  
  Mach number hold (MACH HOLD).
- B.
  
  Navigation/localizer (NAV/LOC).
- C.
  
  Altitude hold (ALT HOLD).
- D.
  
  Glide slope (G/S).
25.

The flight control set (FCS) pitch axis must be engaged for selection of altitude hold (ALT HOLD) or
- A.
  
  Mach number hold (MACH HOLD).
- B.
  
  Tactical Air Navigation (TACAN).
- C.
  
  Navigation/localizer (NAV/LOC).
- D.
  
  Heading select (HDG SEL).