Range / Endurance Profile - Cirrus SR22 Pilot Operating Handbook

C D
IRRUS ESIGN
SR22

Range / Endurance Profile

Conditions:
• Weight.................................3600 LB for Climb, Avg 3400 LB for Cruise
• Temperature.......................................................................... Standard Day
• Winds ..................................................................................................... Zero
• Mixture......................................................................................... See Tables
• Total Fuel .....................................................................................92 Gallons
Fuel Remaining For Cruise is equal to 92.0 gallons usable, less
climb fuel, less 9.8 gallons for 45 minutes IFR reserve fuel at 65%
power (ISA @ 10,000 ft PA), less descent fuel, less fuel used prior
Range and endurance shown includes descent to final destination
Range is decreased by 5% if nose wheel pant and fairings removed.
Range is decreased by 15% if nose and main wheel pants and fair-
Aircraft with optional Air Conditioning System: Range is
decreased by 1% if system in operation. For maximum range, the
Aircraft with optional Enhanced Vision System: Range is
75% POWER
Press Climb
Alt Fuel Remaining
For Cruise
FT GAL
SL 0.0
2000 0.7
4000 1.5
6000 2.3
8000 3.1
P/N 13772-006
Reissue A
to takeoff.
at 178 KIAS and 500 fpm.
ings removed.
Air Conditioner should be OFF.
decreased by ½%.
Fuel Airspeed
GAL KTAS
81.2 166
79.3 170
77.4 173
75.5 177
73.5 180
S
ECTION
R
• N •
OTE
Fuel
Flow Endurance
GPH HOURS
17.8 4.6
17.8 4.5
17.8 4.5
17.8 4.4
17.8 4.4
5: P
ERFORMANCE
/ E
ANGE NDURANCE
Mixture = Best Power
Range Specific
Range
NM NM/GAL
758
769
780
792
804
D
ATA
P
ROFILE
9.3
9.6
9.8
10.0
10.3
5-35