Cirrus DESIGN SR20 Information Manual page 139

Cirrus Design
SR20
Conditions:
• Weight ...................................3000 LB
• Temperature ................. Standard Day
• Winds ..........................................Zero
• Mixture ............................. See Tables
• Total Fuel........................... 56 Gallons
• Fuel Remaining For Cruise accounts for 10.1 gallons for 45 minutes IFR reserve
fuel at 75% power and fuel burn for descent.
• Range and endurance shown includes descent to final destination at 160 KIAS and
500 fpm.
• Range is decreased by 5% if nose wheel pant and fairings removed.
• Range is decreased by 15% if nose and main wheel pants and fairings removed.
75% POWER
Press Climb
Alt Fuel
FT Gal
0 0.0
2000 0.6
4000 1.3
6000 2.0
8000 2.9
10000 3.8
12000 5.0
14000 6.8
P/N 13999-002 Info Manual
September 2011
Range / Endurance Profile
Fuel Airspeed
Remaining
For Cruise
Gal KTAS
46.3 143
45.7 147
45.0 150
44.3 152
43.4 155
42.5
41.3
39.5
Figure 5-17
Sheet 1 of 2
Example:
Power Setting .............................75%
Takeoff Press Alt .................. 2000 FT
Cruise Press Alt.................... 6000 FT
Fuel to Climb ......................... 1.3 Gal.
Cruise Fuel Flow ................ 11.6 GPH
Endurance ................................ 4.0 Hr
Range.................................... 617 NM
True Airspeed .....................152 Knots
• Note •
Fuel Endurance
Flow
GPH Hours
11.6 4.0
11.6 4.0
11.6 4.0
11.6 4.0
11.6 4.0
Section 5
Performance Data
Mixture = Best Power
Range Specific
Range
NM Nm/Gal
576 12.3
594 12.6
606 12.7
617 12.7
627 12.8
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