CIRRUS AIRPLANE MAINTENANCE MANUAL

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1 POWER CONTROL. DESCRIPTION This section describes those components which furnish a means of controlling engine power. Engine controls for the airplane include the following: control quadrant, throttle control cable, mixture control cable, and governor control cable. - Page Jun 20

2 2. MAINTENANCE PRACTICES A. Control Quadrant (See Figure -) () Servicing - Control Quadrant (a) Acquire necessary tools, equipment, and supplies. Description P/N or Spec. Supplier Purpose Aeroshell ASG22 Synthetic Lubricant 9-00 Any Source Lubricant. (b) Remove RH crew seat. (Refer to 2-) (c) Remove friction lock knob and washer from control quadrant. (d) Remove right mid console trim. (Refer to 2-) (e) Remove right aft console trim. (Refer to 2-) (f) Using a clean, lint-free shop towel, remove contaminates from control quadrant, control cable ends, and attaching hardware. (g) Apply a generous amount of lubricant to groove in engine control power lever. (h) To distribute lubricant on bushing, move engine control power lever through full range of motion several times. (i) Using a clean, lint-free shop towel, remove excessive lubricant from control quadrant. (j) Install right aft console trim. (Refer to 2-) (k) Install right mid console trim. (Refer to 2-) (l) Install friction lock knob and washer to control quadrant. (m) Install RH crew seat. (Refer to 2-) (2) Removal - Control Quadrant (a) Remove RH crew seat. (Refer to 2-) (b) Remove friction lock knob and washer from control quadrant. (c) Remove LH and RH mid console trim. (Refer to 2-), (Refer to 2-) (d) Remove LH and RH aft console trim. (Refer to 2-), (Refer to 2-) (e) Remove right and left aft console trim. (Refer to 2-) (f) Remove throttle control cable from control quadrant. (Refer to -) (g) Remove mixture control cable from control quadrant. (Refer to -) (h) Remove governor control cable from control quadrant. (Refer to -) (i) Serials 20 & subs w/ Perspective Avionics: Remove cable ties and wire loom as required to access TO/GA switch wire harness. Disconnect connectors and de-pin TO/GA switch jack to remove harness from control quadrant. (j) Remove nuts, washers, and bolts securing control quadrant to center console. Remove control quadrant from airplane. (3) Disassembly - Power Control - Serials 20 & subs w/ Perspective Avionics (a) Remove screws securing LH and RH knob caps to center knob. (b) Remove screws securing center knob to power lever. (c) Remove TO/GA switch. (Refer to 22-20) () Assembly - Power Control - Serials 20 & subs w/ Perspective Avionics (a) Install TO/GA switch. (Refer to 22-20) (b) Install screws securing center knob to power lever. (c) Install screws securing LH and RH knob caps to center knob. () Installation - Control Quadrant (a) Position control quadrant to center console and secure with bolts, washers, and nuts. - Page 2 Jun 20

3 (b) Serials 20 & subs w/ Perspective Avionics: At control quadrant, re-route TO/GA switch wire harness. Re-pin jack and connect connectors. Secure TO/GA switch wire harness to existing wire harness with wire loom and cable ties. (c) Install throttle control cable to control quadrant. (Refer to -) (d) Install mixture control cable to control quadrant. (Refer to -) (e) Install governor control cable to control quadrant. (Refer to -) (f) Perform Adjustment/Test - Governor Rigging and Low-Pitch Stop Adjustment. (Refer to -20) (g) Perform Adjustment/Test - Throttle Control Cable. (Refer to -) (h) Perform Adjustment/Test - Mixture Control Cable. (Refer to -) (i) Perform Adjustment/Test - Control Quadrant. (Refer to -) (j) Install LH and RH aft console trim. (Refer to 2-), (Refer to 2-) (k) Install LH and RH mid console trim. (Refer to 2-), (Refer to 2-) (l) Install friction lock knob and washer to control quadrant. (m) Install RH crew seat. (Refer to 2-) () Adjustment/Test - Control Quadrant (a) Acquire necessary tools, equipment, and supplies. Description P/N or Spec. Supplier Purpose Spring Scale 0 lb Any Source Pull test. (b) (c) (d) Loosen friction lock knob so engine control power lever moves as freely. Clean and lubricate exposed surface of control cables. Set engine control power lever to full forward (MAX) position. CAUTION: Maximum pull force required to move engine control power lever from full forward (MAX) to full aft (IDLE) position must not exceed 20 pounds. (e) (f) Connect spring scale to engine control power lever and note force required to pull engine control power lever to full aft (IDLE) position. If pull force is less than 20 pounds, no further testing is required. If pull force is greater than 20 pounds, perform the following steps: Determine which cable is generating excess friction by performing pull test three more times, each time with a different cable disconnected from control quadrant. 2 Replace cable(s) causing excessive friction and repeat pull test until pull force required to move power lever from full forward (MAX) to full aft (IDLE) position does not exceed 20 pounds. Note: Pull force with new cables should not exceed 2 pounds. Engine control power lever must move smooth, without any signs of binding. - Page 3 Jun 20

4 LEGEND. Power Control 2. Mixture Control 3. Friction Lock. Cotter Pin. Nut. Washer. Cam Follower 8. Bushing 9. Rod End. Friction Washer. Friction Lock Knob 2. Friction Lock Tube 3. Bolt. Clevis Pin. Mounting Base. Power Lever. Power Lever Knob 8. Screw 9. Mixture Lever 20. Mixture Lever Knob 2. Cowling Safety Pin 9 Serials 0 thru 20, 20 & subs w/o Perspective Avionics SR20_MM_8B Figure - Control Quadrant Installation - Serials 0002 thru 20, 20 & subs w/o Perspective Avionics (Sheet of 2) - Page Jun 20 Serials 0002 thru 20, 20 & subs w/o Perspective Avionics

5 Serials 20 thru LEGEND. Power Control 2. Mixture Control 3. Friction Lock. Cotter Pin. Nut. Washer. Cam Follower 8. Bushing 9. Rod End. Friction Washer. Friction Lock Knob 2. Friction Lock Tube 3. Bolt. Clevis Pin. Mounting Base 8. Screw 9. Mixture Lever Mixture Lever Knob 2. Cowling Safety Pin 22. Power Lever Upper 23. Power Lever Lower NOTE 2. Spacer TO/GA switch only installed on aircraft with 2. Knob, Center GFC 00 autopilot. 2. Knob, Right 2. Knob, Left Ensure bolt head engages anti-rotation clip. 28. Switch 29. Plug 30. Anti-Rotation Clip SR20_MM_280A Figure - Control Quadrant Installation - Serials 20 & subs w/ Perspective Avionics (Sheet 2 of 2) Serials 20 & subs w/ Perspective Avionics - Page 0 Jan 202

6 B. Throttle Control Cable (See Figure -2) Note: The throttle control cable is lubricated and sealed by the manufacturer and should not require further lubrication. If lubrication at control cable is desired, use only the approved lubricant listed in Chapter 2, Servicing. (Refer to 2-20) () Removal - Throttle Control Cable (a) Remove engine cowling. (Refer to -) (b) At throttle body, remove cotter pin, nut, washers, and bolt securing cable rod end to throttle control arm. (c) Remove cable rod end. (d) Remove nut securing cable support bracket to engine. (e) Pull cable and bracket slightly aft and remove nut, washer, and bolt securing retaining clip to bracket. (f) Remove any clamps or ties securing cable to engine mount. (g) Remove friction lock knob and washer from control quadrant. (h) Remove RH crew seat. (Refer to 2-) (i) Remove right and left aft console trim. (Refer to 2-) (j) At control quadrant, remove cotter pin, nut, washers, spacer, and bolt securing cable rod end to power lever. (k) Remove rubber sleeves, nuts, and washers securing cable to console bracket. Note: Prior to removal, note routing of cable and location of anti-chafing spiral wrap to facilitate installation. Remove as much sealant as possible from cable and cable fitting on firewall. (l) Gently pull cable aft through firewall, ensuring that the control cable does not inadvertently pull other components loose. Remove cable from airplane. (2) Installation - Throttle Control Cable (a) Acquire necessary tools, equipment, and supplies. Description P/N or Spec. Supplier Purpose High Temperature Silicone Sealant RTV 3 Dow Corning Sealant. Fiber Frax Paper 90J, TON-0 UniFrax Firewall insulation. (b) Ensure cable fitting on firewall is clear and free of old sealant. CAUTION: When routing the cable, ensure the cable does not interfere with airplane control rigging, wires, or hoses. - Page Jun 20 (c) (d) (e) (f) (g) (h) Route cable forward through the firewall to the engine compartment. Install rod ends to both ends of cable. At console, install washers, nuts, and rubber sleeves securing cable to support bracket. Position cable rod end to power lever and secure with bolt, spacer, washers, nut, and cotter pin. Route cable through engine mounting bracket and loosely install retaining clip, washer, and nut. Route cable through baffling hole. Install rod linkage and rubber bushing seal.

7 (i) At throttle body, secure cable rod end to throttle control arm with bolt, washers, nut, and cotter pin. (j) Wrap fiber paper around portion of cable which passes through firewall fitting so a tight fit is achieved at the cable/firewall interface. (k) Adjust slack in cable, tighten throttle bracket retaining clip nut, align throttle bracket with fuel injection manifold bracket, and install nut. (l) Install clamps or ties securing cable to engine mount. (m) Perform Adjustment/Test - Throttle Control Cable. (Refer to -) (n) Solvent clean firewall fitting and fitting/cable interface. (Refer to 20-30) (o) Fillet seal firewall fitting and fitting/cable interface with silicone sealant. (Refer to 20-) (p) Install right and left aft console trim. (Refer to 2-) (q) Install friction lock knob and washer to control quadrant. (r) Install RH crew seat. (Refer to 2-) (s) Install engine cowling. (Refer to -) (3) Adjustment/Test - Throttle Control Cable (a) Adjust cable jamnuts so power control lever in full forward and aft positions, causes throttle body control arm to make contact with throttle body control arm stops on both sides of travel. (b) Ensure power control lever is only limited by throttle body control arm stops and has positive clearance to console slot in both full forward and full aft positions. (c) Perform Adjustment/Test - Governor Rigging and Low-Pitch Stop. (Refer to -20) (d) Upon adjustment completion, tighten jam nuts. Verify minimum rod end thread engagement of 0.32 inch (0.9 cm). Install cotter pins to rod end nuts. - Page Jun 20

8 FIREWALL (REF) ENGINE CONTROL QUADRANT (REF) ENGINE PAD STUD (REF) 3 THROTTLE CONTROL ARM (REF) LEGEND. Throttle Control Cable 2. Support 3. Jam Nut. Bolt. Washer. Rod End. Nut 8. Cotter Pin 9. Spacer. Retaining Clip. Cable Pass Through 2. Fiberfrax Paper 3. Spring SR20_MM_8A - Page 8 Jun 20 Figure -2 Throttle Control Cable Installation

9 C. Mixture Control Cable (See Figure -3) Note: The mixture control cable is lubricated and sealed by the manufacturer and should not require further lubrication. If lubrication at control cable is desired, use only the approved lubricant listed in Chapter 2, Servicing. (Refer to 2-20) () Removal - Mixture Control Cable (a) Remove engine cowling. (Refer to -) (b) Remove cotter pin, nut, washers, and bolt securing cable rod end to fuel pump control arm. (c) Remove cable rod end. (d) Remove retaining clip, nut, washers, spacer, and bolt securing cable to engine bracket. (e) Remove clamps or cable ties securing cable to engine mount. (f) Remove friction lock knob and washer from control quadrant. (g) Remove RH crew seat. (Refer to 2-) (h) Remove right and left aft console trim. (Refer to 2-) (i) Remove nut, washer, and bolt securing clamp to center console rib and remove clamp from cable. (j) Remove cotter pin, nut, spacer, and bolt securing cable rod end to mixture lever. (k) Remove rubber sleeve, nut, and washer securing cable to console bracket. Note: Prior to removal, note routing of cable and location of anti-chafing spiral wrap to facilitate installation. Remove as much sealant as possible from cable and cable fitting on firewall. (l) Gently pull cable aft through firewall, ensuring that cable does not inadvertently pull other components loose. Remove cable from airplane. (2) Installation - Mixture Control Cable (a) Acquire necessary tools, equipment, and supplies. Description P/N or Spec. Supplier Purpose High Temperature Silicone Sealant RTV 3 Dow Corning Sealant. Fiber Frax Paper 90J, TON-0 UniFrax Firewall insulation. (b) Ensure cable fitting on firewall is clear and free of old sealant. CAUTION: When routing cable, ensure the cable does not interfere with airplane control rigging, wires, or hoses. (c) (d) (e) (f) (g) (h) Route cable forward through the firewall to the engine compartment. Install rod ends to both ends of cable. At console, install washers, nuts, and rubber sleeves securing cable to support bracket. Position cable rod end to mixture lever and secure with bolt, spacer, bearing, washer, nut, and cotter pin. Insert cable into engine bracket, align retaining clip over cable bracket, and install bolt, washers, spacer, and nut. Position cable rod end to fuel pump control arm and secure with bolt, washers, nut, and cotter pin. - Page 9 Jun 20

10 (i) Wrap fiber paper around portion of cable which will pass through firewall fitting so a tight fit is achieved at the cable/firewall interface. (j) At center console rib, attach clamp to cable and secure with bolt, washer, and nut. (k) Install clamps or ties securing cable to engine mount. (l) Perform Adjustment/Test - Mixture Control Cable. (Refer to -) (m) Solvent clean firewall fitting and fitting/cable interface. (Refer to 20-30) (n) Fillet seal firewall fitting and fitting/cable interface with silicone sealant. (Refer to 20-) (o) Install right and left aft console trim. (Refer to 2-) (p) Install friction lock knob and washer to control quadrant. (q) Install RH crew seat. (Refer to 2-) (r) Install engine cowling. (Refer to -) (3) Adjustment/Test - Mixture Control Cable (a) Adjust cable jamnuts so mixture control lever in full forward and aft positions causes fuel pump control arm to make contact with fuel pump control arm stops on both sides of travel. (b) Ensure mixture control lever is only limited by fuel pump control arm stop and has positive clearance to console slot in both full forward and full aft positions. (c) Upon adjustment completion, tighten jam nuts. Verify minimum rod end thread engagement of 0.32 inch (0.9 cm). Install cotter pins to rod end bearing nuts. - Page Jun 20

11 8 3 3 ENGINE CONTROL QUADRANT (REF) 3 2 FIREWALL (REF) CONSOLE RIB (REF) ENGINE MOUNT (REF) MIXTURE CONTROL ARM (REF) FUEL PUMP (REF) LEGEND. Mixture Control Cable 2. Bracket 3. Jam Nut. Bolt. Washer. Rod End. Nut 8. Cotter Pin 9. Spacer. Retaining Clip. Cable Pass Through 2. Fiberfrax Paper 3. Clamp SR20_MM_20A Figure -3 Mixture Control Cable Installation - Page Jun 20

12 D. Governor Control Cable (See Figure -) Note: The governor control cable is lubricated and sealed by the manufacturer and should not require further lubrication. If lubrication at control cable is desired, use only the approved lubricant listed in Chapter 2, Servicing. (Refer to 2-20) () Removal - Governor Control Cable (a) Remove engine cowling. (Refer to -) (b) Remove cotter pin, nut, washers, and bolt securing cable rod end to governor control arm. (c) Remove cable rod end. (d) At cable support bracket mounted to engine, remove retaining clip nut, washers, and bolt and remove cable from support bracket. (e) Remove any clamps or ties securing cable to engine mount. (f) Remove friction lock knob and washer from control quadrant. (g) Remove RH crew seat. (Refer to 2-) (h) Remove right and left aft console trim. (Refer to 2-) (i) At control quadrant, remove cotter pin, nut, washers, and bolt securing cable rod end to throttle cam follower. (j) Remove rubber sleeve, nut, and washer securing cable to console bracket. Note: Prior to removal, note routing of cable and location of anti-chafing spiral wrap to facilitate installation. Remove as much sealant as possible from cable and cable fitting on firewall. (k) Gently pull cable aft through firewall, ensuring that cable does not inadvertently pull other components loose, and remove from airplane. (2) Installation - Governor Control Cable (a) Acquire necessary tools, equipment, and supplies. Description P/N or Spec. Supplier Purpose High Temperature Silicone Sealant RTV 3 Dow Corning Sealant. Fiber Frax Paper 90J, TON-0 UniFrax Firewall insulation. (b) Ensure cable fitting on firewall is clear and free of old sealant. CAUTION: When routing cable, ensure the cable does not interfere with airplane control rigging, wires, or hoses. (c) (d) (e) (f) (g) (h) Route cable forward through the firewall to the engine compartment. Install rod ends to both ends of cable. At console, install washers, nuts, and rubber sleeves securing cable to support bracket. At control quadrant, position cable rod end to throttle cam follower and install bolt, washers, nut, and cotter pin. Insert cable into support bracket, align retaining clip over bracket, and install bolt, washers, and nut. At governor, secure rod end bearing to governor control arm with bolt, washers, nut, and cotter pin. - Page 2 Jun 20

13 (i) Wrap fiber paper around portion of cable which will pass through firewall fitting so a tight fit is achieved at the cable/firewall interface. (j) Install clamps or ties securing cable to engine mount. (k) Perform Adjustment/Test - Governor Rigging and Low-Pitch Stop. (Refer to -20) (l) Solvent clean firewall fitting and fitting/cable interface. (Refer to 20-30) (m) Fillet seal firewall fitting and fitting/cable interface with silicone sealant. (Refer to 20-) (n) Install right and left aft console trim. (Refer to 2-) (o) Install friction lock knob and washer to control quadrant. (p) Install RH crew seat. (Refer to 2-) (q) Install engine cowling. (Refer to -) - Page 3 Jun 20

14 ENGINE CONTROL QUADRANT (REF) FIREWALL (REF) 2 GOVERNOR CONTROL ARM (REF) 8 9 LEGEND. Governor Control Cable 2. Bracket 3. Jam Nut. Bolt. Washer. Rod End. Nut 8. Cotter Pin 9. Retaining Cliper. Cable Pass Through. Fiberfrax Paper SR20_MM_88A - Page Jun 20 Figure - Governor Control Cable Installation

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