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minimum power to maintain taxi speed.
Vertical Speed Indicator — — — —
Engine Indicating
Cylinder Head
Temperature Indication
— — — —
Exhaust Gas Temperature
Indication
— — — —
Fuel Flow Indication 1 1 1 1
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
System, Instrument, and/
or Equipment
Kinds of Operation
(Continued) Remarks, Notes,
and/or
VFR Exceptions
Day
VFR
Nt.
IFR
Day
IFR
Nt.
March 2010
Cirrus Design Section 2
SR22 Limitations
Information Manual 2-17
Fuel Limits
Approved Fuel ............... Aviation Grade 100 LL (Blue) or 100 (Green)
Total Fuel Capacity...................................... 94.5 U.S. Gallon (358.0 L)
Total Fuel Each Tank ................................. 47.25 U.S. Gallon (179.0 L)
Total Usable Fuel (all flight conditions) ........ 92.0 U.S. Gallon (348.0 L)
Maximum Allowable Fuel Imbalance .............10.0 U.S. Gallon (¼ tank)
The fuel pump must be set to BOOST 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.
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).
March 2010
2-18 Information Manual
Section 2 Cirrus Design
Limitations SR22
Systems and Equipment Limits
Cirrus Perspective Integrated Avionics System
1. The Cirrus Perspective by Garmin Integrated Avionics System
Quick Reference Guide for the SR20 and SR22, P/N 190-00821-
02 Rev A or later must be immediately available to the pilot during
flight. The software status stated in the pilot's guide must match
that displayed on the equipment.
2. The Avionics System integrates with separately approved sensor
installations. Adherence to limitations in appropriate installation
POH supplements is mandatory.
3. IFR enroute and terminal navigation is prohibited unless the pilot
verifies the currency of the database or verifies each selected
waypoint for accuracy by reference to current approved data.
4. Instrument approach navigation predicated upon the GPS
Receiver must be accomplished in accordance with approved
instrument approach procedures that are retrieved from the GPS
equipment database. The GPS equipment database must
incorporate the current update cycle.
a. Instrument approaches utilizing the GPS receiver must be
conducted in the approach mode and Receiver Autonomous
Integrity Monitoring must be available at the Final Approach
Fix.
b. Accomplishment of ILS, LOC, LOC-BC, LDA, SDF, MLS or any
other type of approach not approved for GPS overlay with the
GPS receiver is not authorized.
c. Use of the VOR/ILS receiver to fly approaches not approved
for GPS require VOR/ILS navigation data to be present on the
display.
d. Vertical Navigation information may be utilized for advisory
information only. Use of Vertical Navigation information for
Instrument Approach Procedures does not guarantee stepdown
fix altitude protection, or arrival at approach minimums
in normal position to land.
e. IFR non-precision approach approval is limited to published
approaches within the U.S. National Airspace System.
Approaches to airports in other airspace are not approved
unless authorized by the appropriate governing authority.
March 2010
Cirrus Design Section 2
SR22 Limitations
Information Manual 2-19
f. RNAV approaches must be conducted utilizing the GPS
sensor.
g. When conducting missed approach procedures, autopilot (if
installed) coupled operation is prohibited until the pilot has
established a rate of climb that ensures all altitude
requirements of the procedure will be met.
h. The Perspective Integrated Avionics System is compliant with
　
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