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Section 2 - Limitations
Propeller
Hartzell, Constant Speed, Three Blade
Model Number ...............................................PHC-J3YF-1MF/F7392-1
Diameter .............................................................74.0” (72.5” Minimum)
or
Model Number ............................................... PHC-J3YF-1RF/F7392-1
Diameter .............................................................74.0” (72.5” Minimum)
Original Issue: 01-20-09
P/N 11934-S43 3 of 14
Cirrus Design Section 9
SR20 Supplements
Kinds of Operation
Flights are allowed along the routes equipped with beacons operating
in RBS mode and with VHF communication coverage.
Equipment List
Environmental Conditions
1. Minimum Operating Temperature ..............................-22°F (-30°C)
2. Maximum Operating Temperature .............................104°F (40°C)
3. Maximum Crosswind Component .....................................20 Knots
4. Flight into known lightning conditions without an approved
Lightening Detection System i.e. L-3 Stormscope® Weather
Information System or equivalent, is prohibited.
Runway Surface
This airplane must be operated on any paved runway surface with no
standing water.
Ground Handling
1. The aircraft must be brought into a hanger if winds speeds exceed
65 knots.
Altitude Limits
Maximum Altitude............................... 13,780 Feet MSL (4,200 MASL)
System, Instrument,
and/or Equipment
Kinds of Operation
Remarks, Notes,
VFR and/or Exceptions
Day
VFR
Nt.
IFR
Day
IFR
Nt.
Communications
Hand Held Transceiver ● ● ● ● Model P855A1
Autopilot ● ● ● ●
Original Issue: 01-20-09
4 of 14 P/N 11934-S43
Section 9 Cirrus Design
Supplements SR20
Placards
Cabin Window, above door latch:
Doors, above and below latch:
Original Issue: 01-20-09
P/N 11934-S43 5 of 14
Cirrus Design Section 9
SR20 Supplements
Section 3 - Emergency Procedures
Forced Landings
If all attempts to restart the engine fail and a forced landing is
imminent, select a suitable field and prepare for the landing. If flight
conditions or terrain does not permit a safe landing, CAPS deployment
may be required. Refer to Section 10, Safety Information, for CAPS
deployment scenarios and landing considerations.
A suitable field should be chosen as early as possible so that
maximum time will be available to plan and execute the forced landing.
For forced landings on unprepared surfaces, use full flaps if possible.
Land on the main gear and hold the nose wheel off the ground as long
as possible. If engine power is available, before attempting an “off
airport” landing, fly over the landing area at a low but safe altitude to
inspect the terrain for obstructions and surface conditions.
• Note •
Use of full (100%) flaps will reduce glide distance. Full flaps
should not be selected until landing is assured.
Original Issue: 01-20-09
6 of 14 P/N 11934-S43
Section 9 Cirrus Design
Supplements SR20
Emergency Landing Without Engine Power
1. Best Glide Speed ........................................................ ESTABLISH
2. Radio............................................. Transmit (121.5 MHz) MAYDAY
giving location and intentions
3. Transponder ........................................................... SQUAWK 7700
4. If off airport, ELT ........................................................... ACTIVATE
5. Power Lever ............................................................................IDLE
6. Mixture ............................................................................. CUTOFF
7. Fuel Selector............................................................................OFF
8. Ignition Switch ..........................................................................OFF
9. Fuel Pump................................................................................OFF
10. Flaps (when landing is assured) ............................................100%
11. Master Switches.......................................................................OFF
12. Seat Belt(s) ................................................................... SECURED
• Note •
The VHF Hand Held Transceiver, Model P855A1, can be
removed from the back of the passenger seat and used as a
personal locating device if it is necessary to leave the airplane
after an accident. Operate the transceiver in accordance with
instructions attached to unit.
Original Issue: 01-20-09
　
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