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w/o PFD.
PFD Attitude Indication — — 1 1 Serials 1337 & subs
w/ PFD.
PFD Airspeed
Indication
— — 1 1 Serials 1337 & subs
w/ PFD.
PFD Altitude Indication — — 1 1 Serials 1337 & subs
w/ PFD.
PFD Heading
Indication
— — 1 1 Serials 1337 & subs
w/ PFD.
PFD Slip/Skid
Indication
— — 1 1 Serials 1337 & subs
w/ PFD.
Magnetometer — — 1 1 Serials 1337 & subs
w/ PFD.
Vertical Speed
Indicator
— — — —
Multi-Function Display
-Serials 1582
thru 1878 before
PFD Release 7.0
Software Update;
Oil Temperature
Indication must be
operative.
Engine Indicating
Cylinder Head
Temperature Indication
— — — —
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
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.
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
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
2-16 Information Manual
Section 2 Cirrus Design
Limitations SR20
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.
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
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
Information Manual 2-17
Cirrus Design Section 2
SR20 Limitations
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.
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
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西锐20飞机信息手册CIRRUS DESIGN SR20 AIRPLANE INFORMATION MA(8)
