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N699YZ, Serial No. SR-20-2448
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
14. Power loading: 15 lbs. per hp.(A 182 is 13 lbs/hp)
15. V₀: Operating Maneuvering Speed- maximum speed at which application of full
control movement will not overstress the airplane. 113 KIAS.
16. V
: Maximum parachute deployment speed. 135 KIAS
pd
Cirrus SR-20 POH Summary
CIRRUS SR-20
(revised 09/11/2018)
) ²
Page 1 of 18
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Summary of Contents for Cirrus SR-20 N699YZ
- Page 1 14. Power loading: 15 lbs. per hp.(A 182 is 13 lbs/hp) 15. V₀: Operating Maneuvering Speed- maximum speed at which application of full control movement will not overstress the airplane. 113 KIAS. 16. V : Maximum parachute deployment speed. 135 KIAS pd Cirrus SR-20 POH Summary Page 1 of 18...
- Page 2 (normal); fuel flow, manifold Cirrus SR-20 POH Summary Page 2 of 18...
- Page 3 43. Propellor governor failure procedure: If RPM will not increase, check oil pressure and land as soon as practical. If RPM overspeeds or will not decrease, adjust power lever to keep RPM within limits, reduce to 80 knots, and land as soon as practial. Cirrus SR-20 POH Summary Page 3 of 18...
- Page 4 Wy? Switch off electrical components in order to prevent accidental circuit breaker disconnection and loss of power to flight-critical systems. Cirrus SR-20 POH Summary Page 4 of 18...
- Page 5 60. Electric trim/autopilot failure: Maintain airplane control manually (override the autopilot or trim) and disengage the autopilot if it was engaged. Pull the PITCH TRIM, ROLL TRIM, or AUTOPILOT CB as required. Land as soon as practical. Cirrus SR-20 POH Summary Page 5 of 18...
- Page 6 71. How do you check the autopilot disconnect be checked before takeoff? Even though it’s not a Cirrus checklist item, this action should always occur: Press the HDG button to engage the autopilot. Check control forces. Now, press the yoke’s autopilot disconnect button (the coolie hat) to ensure autopilot disconnect.
- Page 7 73. What is the rpm tolerance during the mag check? 175 rpm max drop and both drops must be within 50 rpm of each other. 74. Is an idle check required before takeoff? It’s not on Cirrus’s checklist, but that’s not good. At the conclusion of an engine runup, particularly with a fuel injected engine, an idle check is mandatory.
- Page 8 Aluminum. 90. What is the rudder-aileron interconnect? It provides a maximum of 8° down aileron with full rudder deflection. Right rudder will cause right roll input and left Cirrus SR-20 POH Summary Page 8 of 18...
- Page 9 99. What is the primary heading source for the multifunction display? The PFD. 100. What adjustments can be made for the front seats? Fore and aft and seat-back tilt. Cirrus SR-20 POH Summary Page 9 of 18...
- Page 10 This valve proportions fuel in response to the pilot operated mixture control lever position and automatically provides altitude compensation to supply the proper full rich mixture at any altitude. Fuel is Cirrus SR-20 POH Summary Page 10 of 18...
- Page 11 (throttle). Moving the power lever forward reduces governor oil pressure and allows centrifugal force to decrease propeller Cirrus SR-20 POH Summary Page 11 of 18...
- Page 12 There are two batteries and two alternators. BAT 1 and ALT 1 supply the main distribution bus which powers MAIN BUS 1, MAIN BUS 2, NON-ESSENTIAL BUS 1, and NON-ESSENTIAL BUS 2. BAT 2 and ALT 2 Cirrus SR-20 POH Summary Page 12 of 18...
- Page 13 How can you check to see if the distribution buses isolation diode has failed? Turn on only BAT 2 and the avionics switch and COM 2 or NAV 2. If either one works, the diode has failed. Cirrus SR-20 POH Summary Page 13 of 18...
- Page 14 (Note: This control is located between the HEAT and COLD selectors and is only marked with a defroster symbol and a human body symbol.) Cirrus SR-20 POH Summary Page 14 of 18...
- Page 15 Where is the hour meter located? Inside the armrest storage compartment. 157. What warnings apply to the Cirrus airplane parachute system: The system does not require electrical power and can be activated at any time. The solid-propellant rocket flight path is upward from the parachute cover. Stay clear of the parachute canister area when the airplane is occupied.
- Page 16 SUPPLEMENTS, POH Section 9 Garmin GTX 335-Transponder 168. Do you turn the transponder to STBY after engine start? No, that occurs automatically when you turn on the avionics power. Cirrus SR-20 POH Summary Page 16 of 18...
- Page 17 Note that autopilot disconnects. Move control yoke to confirm that pitch and roll control is free with no control restriction or binding. If a pilot is in the copilot’s seat, repeat the disconnect test using the copilot’s disconnect switch. Cirrus SR-20 POH Summary Page 17 of 18...
- Page 18 ● VS (vertical speed) mode: Autopilot will synchronize to and hold the vertical speed at the time the mode was selected. Vertical speed will change by 100 rpm for each click of the VS knob. Cirrus SR-20 POH Summary Page 18 of 18...
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