The PFD bezel controller provides the following functions: A) HDG. B) STD. C) BARO. D) Both B and C. The EFIS shows information: A) In front of each pilot´s panel. B) In a display located on the center instrument panel. C) In the center pedestal. D) None of the above. The EHSI (Horizontal Situation Indicator) receives inputs from: A) The C-14 directional gyro. B) The VG14A vertical gyro. C) The flight guidance processor (FPG). D) The flight director. The MAX SPD WARNING is active in following FC modes: A) SPD. B) VS. C) VNAV. D) All of the above. The MIN SPD is active in the following mode: A) SPD. B) VS. C) VNAV. D) All of the above. If the flight director fail: A) A large red X will cover the face of the PFD. B) The flight director command bar change a red colour bar. C) The flight director command bar disappear, and the amber FD FAIL warning appears in the top left center of the display. D) The HDG and SPD annunciations turn in red colour. An unusual attitude condition is defined as: A) Bank greater than 65° roll and pitch greater than 30° up or 20° down. B) Bank greater than 60° roll and pitch greater than 20° up or 30° down. C) Bank greater than 70° roll and pitch greater than 35° up or 25° down. D) Bank greater than 65° roll and pitch greater than 20° up or 30° down. The autopilot is normally disengaged in one of the three ways: A) Depressing the AP TRIM DISC switch on either yoke. B) Electrically trimming the elevator trim system. C) Depressing the go-around button on either throttle. D) All of the above. The VG-14A vertical gyro system is powered by: A) The DC GEN1 B) The AC system (Inverter) C)The battery in EMER position. D) None of the above. The GPWS provides visual and aural warnings of terrain in ____ modes. A) 4 B) 5 C) 6 D) 7.
