background image

 
 

Roll control 

Roll control is by conventional cable-operated ailerons, augmented by cable-operated, 
hydraulically activated, roll spoilers. The rotational movement of the pilot's control wheel 
activates the roll spoilers while the co-pilot’s control wheel activates the ailerons. An 
interconnect linkage joins the pilot's and co-pilot’s control wheels so that both systems are 
operated from either wheel. A clutch within the linkage can be disengaged manually, by 
means of a roll disconnect handle on the flight compartment centre console, to separate the 
left and right roll control circuits in the event of a jam in either circuit. With the control circuits 
separated, control can be maintained with the un-jammed control wheel. 
 
 

Ailerons 

An aileron is located on each wing outboard of the flaps. Rotation of either control wheel 
actuates the ailerons differentially by means of a cable control loop, with inter-connection to 
applicable roll spoilers. 
 
Geared tabs on the trailing edge of each aileron assist aileron deflection. The tabs are 
geared to a static position, which is aerodynamically neutral relative to the aileron. When the 
aileron is deflected, the geared tab moves in the opposite direction creating a localized lifting 
force about the tab in the direction of aileron deflection, thus assisting aileron movement. 
 
The right aileron trim tab, using an electric actuator built into the aileron, provides aileron 
trim. A L/R AILERON rocker switch, located on the TRIM panel on the centre console 
operates the actuator when depressed to the left or right. The actuator trims aileron control 
pressure by biasing the static neutral position of the trim tab. An indicator adjacent to the L/R 
AILERON rocker switch shows the degree of trim actuator displacement from neutral. 
 

Dash8-200/300 - Flight Controls

Page 15

Summary of Contents for Dash8-200

Page 1: ...FLIGHT CONTROLS CONTROLS AND INDICATORS Rudder and yaw damper Dash8 200 300 Flight Controls Page 1...

Page 2: ...Elevators Dash8 200 300 Flight Controls Page 2...

Page 3: ...Spoiler and aileron Dash8 200 300 Flight Controls Page 3...

Page 4: ...Flaps Dash8 200 300 Flight Controls Page 4...

Page 5: ...Flaps Dash8 200 300 Flight Controls Page 5...

Page 6: ...Miscellaneous controls Dash8 200 300 Flight Controls Page 6...

Page 7: ...Powered flight control surface controls and indications Dash8 200 300 Flight Controls Page 7...

Page 8: ...Powered flight control switches and indications Dash8 200 300 Flight Controls Page 8...

Page 9: ...flight controls consists of wing flaps and trimming systems for the primary flight controls and a flight control gust lock mechanism All flight controls may be operated from either the left or right...

Page 10: ...150 KIAS in response to speed signals from the air data computers ADC s to reduce rudder sensitivity at high speeds Pressure switches armed by ADC speed signals are positioned in each actuator s suppl...

Page 11: ...Rudder control diagram Dash8 200 300 Flight Controls Page 11...

Page 12: ...Rudder control diagram Dash8 200 300 Flight Controls Page 12...

Page 13: ...b on its inboard trailing edge With elevator control input this provides a servo assist which reduces elevator control forces Elevator trim is provided by tabs on each surface outboard of the spring t...

Page 14: ...Elevator control diagram Dash8 200 300 Flight Controls Page 14...

Page 15: ...either control wheel actuates the ailerons differentially by means of a cable control loop with inter connection to applicable roll spoilers Geared tabs on the trailing edge of each aileron assist ai...

Page 16: ...Aileron control diagram Dash8 200 300 Flight Controls Page 16...

Page 17: ...ssary to control the aircraft will illuminate both SPLR switch lights via an under floor limit switch if aileron travel exceeds 50 of control wheel displacement from neutral The switch lights must the...

Page 18: ...Roll spoiler control diagram Dash8 200 300 Flight Controls Page 18...

Page 19: ...LEFT RIGHT PILOTS S Dash8 200 300 Flight Controls Page 19...

Page 20: ...Roll spoilers diagram Dash8 200 300 Flight Controls Page 20...

Page 21: ...flexible shaft coupled to the primary drive system through two transfer gearboxes The purpose for the secondary drive is to maintain symmetrical operation of all flap sections if the primary drive br...

Page 22: ...Flap control diagram Dash8 200 300 Flight Controls Page 22...

Page 23: ...Flap control schematic Dash8 200 300 Flight Controls Page 23...

Page 24: ...extended periods especially while parked may require a maintenance check prior to dispatch Flight crew are urged to report known exposure to strong winds or wind gusts to maintenance CAUTION If the ai...

Page 25: ...ed either by operation of the PUSH OFF switch light or by hydraulic failure Roll control jam Each actuator linkage is connected so that in the event of a jam overpowering force applied to the control...

Page 26: ...ct handle pulled the autopilot must remain disengaged Flap control system If during flap extension or retraction a flap jam occurs the flap system automatically shuts down Flap operation will continue...

Page 27: ...CL RUDDER FULL PRESSURE Remarks RUD PRESS caution light of remaining actuator illuminates if aircraft speed exceeds 150 KIAS RUD PRESS Failure of rudder pressure regulator to adjust pressure to the pr...

Page 28: ...ate using secondary transmission shaft Flap may be operated normally for remainder of flight FLAP POWER Indicates loss of hydraulic supply pressure Applicable ECL FLAP POWER FAILURE Remarks Unless hyd...

Reviews: