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March 2010
2-20 Information Manual
Section 2 Cirrus Design
Limitations SR20
8. Serials with Avidyne MFD installed: The Avidyne FlightMax
EX5000C Pilot’s Guide, P/N 600-00108-000, Revision 03 or later,
must be available to the pilot during all flight operations.
Oxygen System
Whenever the operating rules require the use of supplemental oxygen,
the pilot must:
• Use an oxygen system approved by Cirrus Design and listed in
the Oxygen System AFM Supplement Part Number 11934-
S09.
• Secure the oxygen bottle in the right front seat as described in
the AFM Supplement noted above.
Inflatable Restraint System
Serials 1268 thru 1540 after SB 2X-25-14 and serials 1541 and
subsequent; Use of a child safety seat with the inflatable restraint
system is prohibited.
Flap Limitations
Approved Takeoff Settings...........................................UP (0%) or 50%
Approved Landing Settings ............................. Up (0%), 50%, or 100%
Paint
To ensure that the temperature of the composite structure does not
exceed 150° F (66° C), the outer surface of the airplane must be
painted in accordance with the paint colors and schemes as specified
in the Airplane Maintenance Manual. Refer to Airplane Maintenance
Manual (AMM), Chapter 51, for specific paint requirements.
Other Limitations
Smoking
Smoking is prohibited in this airplane.
March 2010
Information Manual 2-21
Cirrus Design Section 2
SR20 Limitations
Placards
REFER TO AFM FOR APPROVED OILS
ENGINE OIL GRADE
BELOW 40° F SAE 30 OR 10W30, 15W50, OR 20W50
ABOVE 40° F SAE 50 OR 20W50
Engine compartment, inside oil filler access:
Wing, adjacent to fuel filler caps:
SR20_FM02_1220D
A V G AS M I N G R A DE 1 0 0 L L OR 1 0 0
15 6 4 8 - 0 0 2
28 U . S. G ALS. ( 10 6 L ITERS) T OTAL U SABLE C APAC I T
1 3 U . S . G A L S . (4 9 L I T E R S ) U S A B L E T O T A B
Y
Serials 1327 & subs.
Serials 1100 thru 1326.
Serials 1005 thru 1099.
AVGAS MIN GRADE 100LL OR 100
28 U.S. GALS. TOTAL USABLE CAP
13 U.S. GALS. USABLE TO TAB
AVGAS MIN GRADE 100LL OR 100
28 U.S. GALS. (106 LITERS) TOTAL USABLE CAP
13 U.S. GALS. (49 LITERS) USABLE TO TAB
Figure 2-5
Placards (Sheet 1 of 7)
March 2010
2-22 Information Manual
Section 2 Cirrus Design
Limitations SR20
Figure 2-5
Upper fuselage, either side of CAPS rocket cover:
WARNING!
STAY CLEAR WHEN AIRPLANE IS OCCUPIED
ROCKET FOR PARACHUTE DEPLOYMENT INSIDE
OPEN
TO
PUSH
Serials 1423 & subs.
ESOLC
E PO
N
Serials 1005 thru 1316. Serials 1317 thru 1422.
OPEN
CLOSE
Doors, above and below latch:
Rudder, and elevator, both sides:
NO PUSH
Left fuselage, on external
power supply door:
EXTERNAL
POWER
28 V DC
SR20_FM02_1221B
Placards (Sheet 2 of 7)
March 2010
Information Manual 2-23
Cirrus Design Section 2
SR20 Limitations
100 KIAS
100%
120 KIAS
50%
Engine control panel:
SR20_FM02_1602A
GALLONS
USABLE
28
RIGHT
USABLE
GALLONS
28
LEFT
PRIME
FUEL
PUMP
BOOST
N O
I
T
C
I
R
F
M
I
X
T
U
R
E
P
O
W
E
R
IDLE CUTOFF
MAX FULL RICH
UP
FLAPS
OFF
CONTROL HANDLES FULLY DOWN BEFORE FLIGHT
CREW SEATS MUST BE LOCKED IN POSITION AND
OFF
Figure 2-5
Placards (Sheet 3 of 7)
March 2010
2-24 Information Manual
Section 2 Cirrus Design
Limitations SR20
Figure 2-5
Serials 1337 & subs with SRV option.
DAY - NIGHT - VFR
Bolster Switch Panel, left edge:
OPERATE PER AIRPLANE FLIGHT MANUAL
FLIGHT INTO KNOWN ICING IS PROHIBITED
(WITH REQUIRED EQUIPMENT)
DAY - NIGHT - VFR - IFR
FOLLOWING FLIGHT OPERATIONS:
THIS AIRCRAFT IS CERTIFIED FOR THE
Instrument Panel Upper left:
INCLUDING APPROVED
NO
NORMAL CATEGORY AIRPLANE
SPINS,
ACROBATIC MANEUVERS,
SPEED: Vo 131 KIAS
MANEUVERING
OPERATE PER AIRPLANE FLIGHT MANUAL
FLIGHT INTO KNOWN ICING IS PROHIBITED
(WITH REQUIRED EQUIPMENT)
FOLLOWING FLIGHT OPERATIONS:
THIS AIRCRAFT IS CERTIFIED FOR THE
NO STEP
RESCUE: FRACTURE AND REMOVE WINDOW
Wing, flap aft edge:
Cabin Door Window, lower edge, centered, applied upside down:
Serials 1005 & subs w/o SRV option.
SR20_FM02_1223E
　
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