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w/o PFD.
PFD Attitude Indication — — 1 1
Serials 0435 & subs
w/ PFD.
PFD Airspeed Indication — — 1 1
Serials 0435 & subs
w/ PFD.
PFD Altitude Indication — — 1 1
Serials 0435 & subs
w/ PFD.
PFD Heading Indication — — 1 1
Serials 0435 & subs
w/ PFD.
PFD Slip/Skid Indication — — 1 1
Serials 0435 & subs
w/ PFD.
Magnetometer — — 1 1
Serials 0435 & subs
w/ PFD.
Vertical Speed Indicator — — — —
Multi-Function Display 􀂙 􀂙 􀂙 􀂙
􀂙-Serials 1602,
1644, and 1663
thru 2750 before
PFD Release 7.0
Software Update;
Oil Temperature
Indication must be
operative.
Engine Indicating
Cylinder Head
Temperature Indication
— — — —
Exhaust Gas
Temperature Indication
— — — —
Fuel Flow Indication 1 1 1 1
System,
Instrument,
and/or
Equipment
Kinds of Operation Remarks,
Notes,
and/or
Exceptions
VFR
Day
VFR
Nt.
IFR
Day
IFR
Nt.
Revision A8
P/N 13772-001 2-15
Cirrus Design Section 2
SR22 Limitations
Icing
Flight into known icing conditions is prohibited.
Runway Surface
This airplane may be operated on any smooth runway surface.
• Caution •
Operation on unimproved runway surfaces will cause
additional wear and may require additional maintenance or
inspection. Refer to the Airplane Maintenance Manual.
Manifold Pressure
Indication
1 1 1 1
Oil Pressure Indication 1 1 1 1
Oil Quantity Indicator
(Dipstick)
1 1 1 1
Oil Temperature
Indication
1 1 1 1
Engine Speed 1 1 1 1
Special Equipment
Cirrus Airframe
Parachute (CAPS)
1 1 1 1
Airplane Flight Manual 1 1 1 1 Included w/ POH.
System,
Instrument,
and/or
Equipment
Kinds of Operation Remarks,
Notes,
and/or
Exceptions
VFR
Day
VFR
Nt.
IFR
Day
IFR
Nt.
Revision A8
2-16 P/N 13772-001
Section 2 Cirrus Design
Limitations SR22
Taxi Power
Maximum continuous engine speed for taxiing is 1000 RPM on flat,
smooth, hard surfaces. Power settings slightly above 1000 RPM are
permissible to start motion, for turf, soft surfaces, and on inclines. Use
minimum power to maintain taxi speed.
Fuel Limits
Approved Fuel ............... Aviation Grade 100 LL (Blue) or 100 (Green)
Total Fuel Capacity ...................................... 84.0 U.S. Gallon (318.0 L)
Total Fuel Each Tank ................................... 42.0 U.S. Gallon (159.0 L)
Total Usable Fuel (all flight conditions) ........ 81.0 U.S. Gallon (306.6 L)
Maximum Allowable Fuel Imbalance .............10.0 U.S. Gallon (¼ tank)
The fuel system BOOST pump must be on for takeoff, climb, landing,
and for switching fuel tanks.
Altitude Limits
Maximum Takeoff Altitude.......................................... 10,000 Feet MSL
Maximum Operating Altitude ..................................... 17,500 Feet MSL
The operating rules (FAR Part 91 and FAR Part 135) require the use of
supplemental oxygen at specified altitudes below the maximum
operating altitude. Refer to Oxygen System Limitations in this Section.
Environmental Conditions
For operation of the airplane below an outside air temperature of -10°F
(-23° C), use of cowl inlet covers approved by Cirrus Design and listed
in the Winterization Kit AFM Supplement P/N 13772-118 is required.
Maximum Occupancy
Occupancy of this airplane is limited to four persons (the pilot and
three passengers).
Revision A8
P/N 13772-001 2-17
Cirrus Design Section 2
SR22 Limitations
Systems and Equipment Limits
Cirrus Airframe Parachute System (CAPS)
VPD Maximum Demonstrated Deployment Speed .................133 KIAS
• Note •
Refer to Section 10 – Safety Information, for additional CAPS
guidance.
Primary Flight Display
1. The PFD integrates with separately approved sensor installations.
Adherence to limitations in appropriate installation POH
supplements is mandatory.
2. The Avidyne FlightMax Entegra-Series PFD Pilot’s Guide, P/N
600-00142-000, Revision 03, or latest revision, must be available
to the pilot during all flight operations.
3. Flight under Instrument Flight Rules (IFR) is not permitted with the
PFD or any standby indicator (attitude indicator or magnetic
　
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