17.V
S50%
and V
SO
: Stall speed with 50% and 100% flaps extended.
LIMITATIONS, POH Section 2
18.V
NE
, V
NO
, V
O
, V
PD
: 201 KIAS, 164, 133, 150
50%
/110
100%
, 135
19.Zero fuel weight: 2,814 lbs.
20.Maximum weight in baggage compartment: 130 lbs.
21.Center of gravity reference datum: 100 inches forward of firewall
22.Flap limitations: Takeoff- 0% or 50%. Landing- 100%, however 0% or 50% can
be used if malfunction or other conditions deem it appropriate.
23.Allow flight load factors: Flaps up -+3.8g, -1.9g. Flaps ex1.9g, -0g.
24.Maximum fuel imbalance limit: 7.5 gallons (¼ tank)
25.Maximum operating altitude: 17,500 ft. MSL
26.Temperature limit and paint limitations: 150
℉
(66
℃
), approved white paint.
27.Runway surface and smoking limitations: Smooth 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- IFR.
33.List remaining equipment that’s required for all operations: Ammeter, low volts,
and alternator annunciators; ELT; fire extinguisher; flaps system and flap position
lights; pitch and bank trim systems and indicators; fuel boost pump, quantity
indicator, and selector valve; alternate engine-air induction system; alternate
static source; anti-collision lights; standby altimeter and airspeed indicators;
magnetic compass; pitot system, static system (normal); fuel flow, manifold
Cirrus SR-20 POH Summary
Page 2 of 18
