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inspection. Refer to the Airplane Maintenance Manual.
Cylinder Head
Temperature Gage
— — — —
Exhaust Gas
Temperature Gage
— — — —
Fuel Flow Gage 1 1 1 1
Manifold Pressure Gage 1 1 1 1
Oil Pressure Gage 1 1 1 1
Oil Quantity Indicator
(Dipstick)
1 1 1 1
Oil Temperature Gage 1 1 1 1
Tachometer 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.
March 2010
Information Manual 2-15
Cirrus Design Section 2
SR20 Limitations
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.
Instrument Procedures
Due to the possibility of CDI needle oscillation, in aircraft configured
with a 2 blade propeller, while conducting instrument procedures that
use a localizer or Simplified Directional Facility (SDF) navaid, engine
speed above 2600 rpm is prohibited.
Fuel Limits
The maximum allowable fuel imbalance is 7.5 U.S. gallons (¼ tank).
Approved Fuel ............... Aviation Grade 100 LL (Blue) or 100 (Green)
Total Fuel Capacity..................................... 60.5 U.S. gallons (229.0 L)
Total Fuel Each Tank .................................. 30.3 U.S. gallons (114.5 L)
Total Usable Fuel (all flight conditions) ....... 56.0 U.S. gallons (212.0 L)
Altitude Limits
Maximum Takeoff Altitude ..........................................10,000 Feet MSL
Maximum Operating Altitude .........................................17,500 ft. 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 11934-S25 is required.
Maximum Occupancy
Occupancy of this airplane is limited to four persons (the pilot and
three passengers).
March 2010
2-16 Information Manual
Section 2 Cirrus Design
Limitations SR20
Systems and Equipment Limits
Cirrus Airframe Parachute System (CAPS)
VPD Maximum Demonstrated Deployment Speed..................135 KIAS
• Note •
Refer to Section 10 – Safety Information, for additional CAPS
guidance.
Multi-Function Display
1. The moving map display must not be used as the primary
navigation instrument. The moving map display provides visual
advisory of the airplane’s GPS position against a moving map.
The information supplements CDI course deviation and
information provided on the GPS navigator.
2. Use of Map page during IFR flight requires an IFR approved GPS
receiver installation operated in accordance with applicable
limitations.
3. Under no circumstances should the Map page terrain
representations be used as a basis for terrain avoidance.
4. The electronic checklists display supplements the Pilot Operating
Handbook checklists and is advisory only. The electronic
checklists must not be used as the primary set of on-board
airplane checklists.
5. The MFD interfaces with separately approved sensor installations.
Adherence to limitations in the appropriate sensor installation
POH Supplements is mandatory.
6. Traffic information shown on the Map page display is provided to
the pilot as an aid to visually acquire traffic. Pilots should
maneuver their aircraft based only on ATC guidance or positive
visual acquisition of the conflicting traffic. Maneuver should be
consistent with ATC instructions. No maneuvers should be made
based solely on a traffic advisory.
1. Serials with ARNAV MFD installed; The ARNAV ICDS 2000 Pilot’s
Operation Handbook,Serials with ARNAV MFD installed; The
ARNAV ICDS 2000 Pilot’s Operation Handbook, P/N 572-0550
March 2010
Information Manual 2-17
Cirrus Design Section 2
SR20 Limitations
dated May 1998 or later revision, must be available to the pilot
during all flight operations
7. Serials with Avidyne MFD installed: The Avidyne FlightMax
　
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