Secondary Flight Contols Flashcards
Examples of secondary flight controls
Flaps, trimming devices, slats, spoilers, speed brakes
Anything that doesn’t control a/c attitude but provides a finer control over the a/c and ease pilot workload
Flap operation
Flight deck selector - flap shaped to be tactile distinctive - produces an input to the slat/flap computers - control monitor and test the operation of the flaps
Electrically controlled hydromechanical unit drives the transmission which drives the flaps
Leading edge slats
Variable posn = retracted, intermediate, fully extended - slat with a slot
Leading edge flaps only have 2 posn
Operation of leading edge devices - sequence
Leading edge flaps extend fully - slats to the intermediate posn when the trailing edge flaps move into the intermediate posn
When trailing is fully lowered - slats extend fully
Sequence is reversed for retraction
Leading edge devices operation
Hydraulic motor drives a gearbox which drives a series of torque shafts
Leading edge devices - alternate operation
Can be extended electrically but some a/c - cant get it back up once extended
LRS - flap limiter
Retracts the flaps to the mid posn if the airspeed exceeds a predetermined speed
Automatically returns to fully extended when the speed reduces
Flap asymmetry protection
Interrupts flap movement when it is detected - locks it out
Isolates the flap selector lever
Sends a warning into the f/d
Autoslat system
Automatically deploys slats to the fully extend posn if the a/c is close to reaching stalling AoA
Alternate flap operation ALT posn
Operates a electrically driven back up system
Disables normal flap control
Arms the alternate mode
Engages electric motors
Disables ink which operates slats in conjunction with flaps
Ideal speed brake location
Fuselage - increase of drag with a limited loss of lift
Speed brake - armed mode
Will not work until certain conditions are met
Req a signal from 2 separate wheels
Ground shutoff valve ensures ground spoilers are used only on the ground
Spoiler operation
Aileron PFCU movement actuates the aileron and simultaneously sends a roll control signal to the spoiler mixer
Flight spoiler hydraulic power is controlled by
Electric motor driven valves - situated in the flight control power system - allows spoilers to be isolated if required
2 spoiler switches individually control the valves
Flap systems are operated by
Screw jacks - forms a mechanical lock