controls

Question 1

Purpose

Answer 1

provides control on lonigtudinal, lateral, and vertical axes

Question 2

Flight Control Computer (FLCC)

Answer 2

principal component, receives input from side stick controller, rudder pedals, trim, autopilot, interial sensors, & air data

Question 3

side stick controller

Answer 3

stick grip and force sensing transducer, right console, pitch & roll

Question 4

manual trim panel

Answer 4

provides pitch, roll, & yaw trim commands

Question 5

rudder pedal assembly

Answer 5

commands position of rudder, located forward of center of cockpit on the floor

Question 6

flight control panel

Answer 6

controls and indicators for flight control malfunctions, performs & monitors self-tests

Question 7

flight control accumulators

Answer 7

one each hydraulic system, supplies hydraulic pressure to ISA when demand is higher than pump delivery 3 secs of pressure in case of fail

Question 8

flaperons

Answer 8

ctrl roll movement, 23 deg. up and 20 deg. down, func. as ailerons and flaps

Question 9

integrated servoactuators ISA

Answer 9

electrically commanded, hydraulically powered, one is mech. connected to each primary FLT Ctrl surfaces, powered by both A & B hydr. sys.

Question 10

horizontal stab

Answer 10

ctrl pitch, 21 deg. up or down, symmetrically for pitch, asymmetrically to augment roll maneuvers

Question 11

Leading edge flaps

Answer 11

2nd FLT ctrl spanning the length of each wing,provides high lift and optimized FLT perform. 2deg up and 20 deg down

Question 12

electronic component assembly

Answer 12

microprocessor schedules LEF position, receives signals from multiple sources (Angle of Attack, Airspeed, Altitude)

Question 13

rudder

Answer 13

ctrl yaw, 30 deg left & right

Question 14

AOA

Answer 14

send signals to EAC/FLCC located each side of radome