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CIRRUS SR-20 

N699YZ, Serial No. SR-20-2448 

(revised 09/11/2018) 

 
 
General, POH Section 1 

 

1. Engine Model: Lycoming 10-390-C3136 

2. Engine Horsepower rating: 215hp @ 2700 rpm 

3. Propellor type:  Three-blade, constant-speed Hartzell 

4. Fuel capacity: 58.5 gallons total, 56.0 gallons useable 

5. Fuel type: 100 LL (blue), 100 (green) 

6. Oil capacity: 7 quarts (note; min. Quantity, 6 qts.) 

7. Oil grades: Above 40

 - SAE 40, all temps SAE 15W-50 or SAE 20W-50 

8. Maximum gross weight for takeoff: 3,150 lbs. 

9. Maximum gross weight for landing: 3,150 lbs.  

10.N699YZ empty weight (see book at dispatch counter): 2145 lbs.  

11.N699YZ payload with full fuel (book on dispatch counter): 668 lbs.  

12.N699YZ useful load: 849 lbs. 

13. Wing loading: 22 lbs per square foot. (A 182 is 17 lbs/ft

)

²

 

14.Power loading: 15 lbs. per hp.(A 182 is 13 lbs/hp) 

15. V

: Operating Maneuvering Speed- maximum speed at which application of full 

control movement will not overstress the airplane. 113 KIAS.  
 

16.V

pd

: Maximum parachute deployment speed. 135 KIAS 

Cirrus  SR-20 POH Summary

 

Page 1 of 18 

Summary of Contents for SR-20 N699YZ

Page 1: ...W 50 or SAE 20W 50 8 Maximum gross weight for takeoff 3 150 lbs 9 Maximum gross weight for landing 3 150 lbs 10 N699YZ empty weight see book at dispatch counter 2145 lbs 11 N699YZ payload with full fuel book on dispatch counter 668 lbs 12 N699YZ useful load 849 lbs 13 Wing loading 22 lbs per square foot A 182 is 17 lbs ft 14 Power loading 15 lbs per hp A 182 is 13 lbs hp 15 V Operating Maneuvering...

Page 2: ...ooth runway surface no smoking 28 Maximum demonstrated parachute deployment speed 135 KIAS 29 Multi function display limitation Not approved as a primary navigation instrument Information may be used for advisory purposes only 30 Flight into known icing conditions Prohibited 31 Battery requirements Battery 1 IFR and VFR Battery 2 IFR 32 Alternator requirements Alternator 1 IFR and VFR Alternator 2...

Page 3: ...eck both 40 Engine airstart procedure Battery master switches on power level open mixture rich switch fuel tanks ignition switch on both fuel pump onboost alternate induction air on alternator master switches off engage starter if prop not windmilling slowly increase power lever alternator master switches on when engine starts 41 If a partial power loss occurs or the engine starts running rough wh...

Page 4: ...s off ignition switch off fuel pump off ELT on located below CB panel seat belts and harnesses tightened loose items secure and assume emergency landing body position 50 Describe the emergency landing body position Cross your arms across your chest firmly grasp the shoulder harness and hold your upper torso erect The landing force is equivalent to a drop from 10 feet above the ground 51 An alterna...

Page 5: ...urn the ALT 2 master switch off and land as soon as practical Essential bus loads will now be powered from ALT 1 BAT 1 and BAT 2 57 LOW VOLTS warning light illuminated procedure Cause Voltage is 24 5 volts or less and you are on battery power only because both alternators have failed or are off Procedure If both alternators have failed land as soon as possible 58 Communications failure procedure C...

Page 6: ...After engine start 69 How do you start a flooded engine Turn fuel pump off allow fuel to drain from the intake tubes mixture full lean power lever full open crank the engine through several revolutions When it starts retard the power lever and slowly advance the mixture to full rich 70 How do you maintain directional control when taxiing With rudder and differential braking In crosswind conditions...

Page 7: ...n 79 What is the short field approach speed and the restriction that applies to braking 78 KIAS Apply normal brake pressure and announce simulating max braking 80 What is the crosswind landing technique Use full flaps and avoid prolonged slips 81 If the ELT activates after a hard landing how do you turn it off Press the reset button on the ELT control panel that s located below the circuit breaker...

Page 8: ...e following information Yes but the airplane is at its forward CG limit Basic empty weight 2145 lbs Empty moment 1 000 306 211 Fuel 56 gallons useable Pilot 210 lbs Front seat passenger 170 lbs Rear seat passenger 140 lbs 88 Just after takeoff in the previous problem the pilot realizes that his wallet pilot certificate and medical is in his car Is he legal to immediately return and land Yes the ma...

Page 9: ...ched to the instrument panel bolster the rounded portion that extends across the cockpit beneath the instrument panel Aileron Align the force and aft line that s etched on the control yoke with the centering indication that s marked on the bolster 95 If the elevator control system or aileron control system failed due to something other than a jammed elevator or a jammed aileron how could you contr...

Page 10: ...before each flight What must you ensure The nozzle is unobstructed the pin has not been pulled and the canister has not been damaged 106 Are the rudder pedals connected to the nose gear for steering No 107 So how do you steer the airplane Differential braking 108 Describe the brake system A master cylinder for each rudder pedal one hydraulic fluid reservoir a parking brake valve and a single disc ...

Page 11: ... the cruise power settings and 2 700 rpm at full power 116 How does the mixture control lever function It is mechanically linked to the mixture control valve in the engine driven fuel pump and controls the mixture at that point 117 Which battery master switch activates the engine s start ignition switch BAT 1 118 Describe the function location and operation of the alternate air control knob It ope...

Page 12: ...s are filled to the tabs 26 gallons 13 in each fuel tank 125 Left fuel tank is empty right tank has 10 gal Will the FUEL caution light be on No both tanks must have approximately 8 5 gallons for the light to activate 126 What problem can occur when the fuel tanks are full or less Prolonged uncoordinated flight such as skips or skids for more than 30 seconds can uncover the fuel tank outlets and ca...

Page 13: ...lkhead 132 Why do you think that ALT 2 is regulated to a higher voltage than ALT 1 This is not explained well in the POH Voltage is like water pressure Because ALT 2 has more pressure it prevents ALT 1 from powering the essential buses during normal operation of the electrical system ALT 1 can power the essential buses only if ALT 2 fails 133 Why should the batteries and alternators not be turned ...

Page 14: ...e center console that can be used for portable entertainment equipment 144 List the exterior lights Position lights Anti collision lights Landing lights Recognition Halo lights 145 List the interior lights Dimmable incandescent instrument bezel lights dimmable red LED instrument panel flood lights reading lights that are dimmable for the two front seats and a dimmable overhead dome light 146 Three...

Page 15: ...ere is the ELT located and where is it s control panel located It is installed behind the aft cabin bulkhead and the control panel is installed immediately below the circuit breaker panel next to the pilot s right leg 155 How can you tell if the ELT is transmitting A flashing light on the control panel 156 Where is the hour meter located Inside the armrest storage compartment 157 What warnings app...

Page 16: ...Nose wheel 40 psi Main wheels 53 psi 165 Installation of the oil dipstick can be difficult How should you do it Point the dipstick s finger loop toward the airplane s nose or tail and allow the dipstick to rotate as you push it into the engine 166 When cleaning the windshield and windows what hand motion should you use Linear straight back and forth Circular motion causes spirals in the plexiglas ...

Page 17: ...ft and right Vertical speed test Press VS button and note that VS light illuminates VS 0 Rotate the VS control knob to 500 fpm up and the control yoke should move aft after a short delay Rotate the VS control knob to 500 fpm down and the control yoke should move forward after a short delay Altitude hold test Depress the ALT button Note that ALT annunciator comes on VS annunciator goes out and yoke...

Page 18: ...oach mode Provides increased sensitivity for VOR or GPS approaches GS glideslope mode Autopilot will capture and track an ILS glideslope The airplane must be 60 or more below the glideslope centerline during the approach to the intercept point and with 50 needle deviation of the localizer centerline at the point of intercept usually the outer marker When these conditions have existed for 10 second...

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