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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 OFF
100 KIAS
100%
120 KIAS
50%
11113-005
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
CONTROL HANDLES FULLY DOWN BEFORE FLIGHT
CREW SEATS MUST BE LOCKED IN POSITION AND
Airplane serials 1268 and subsequent
and airplane serials 1005 thru 1267
incorporating SA 02-13.
Airplane serials 1184 thru 1267.
Placards (Sheet 4 of 9)
March 2010
Information Manual 2-23
Cirrus Design Section 2
SR20 Limitations
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
Figure 2-5
Placards (Sheet 5 of 9)
March 2010
2-24 Information Manual
Section 2 Cirrus Design
Limitations SR20
Figure 2-5
FASTEN SEAT BELT • NO SMOKING
FIRE EXTINGUISHER FORWARD LEFT OF PILOT SEAT
Serials 1639 & subs.
Serials 1005 thru 1638.
Serials 1351 & subs.
GRAB HERE
Bolster Panel, both sides:
SR20_FM02_1517E
Serials 1005 thru 1178.
EMERGENCY EXIT
REMOVE EGRESS HAMMER FROM ARMREST LID
STRIKE CORNER OF WINDOW,
KICK OR PUSH OUT AFTER FRACTURING
Cabin Window, above door latch:
Instrument Panel:
UNDER PILOT SEAT FRONT
FIRE EXTINGUISHER
FASTEN SEATBELTS
NO SMOKING
EMERGENCY EXIT
REMOVE EGRESS HAMMER FROM WITHIN
CENTER ARMREST LID. STRIKE CORNER OF
WINDOW. KICK OR PUSH OUT AFTER FRACTURING
Serials 1179 & subs.
Placards (Sheet 6 of 9)
March 2010
Information Manual 2-25
Cirrus Design Section 2
SR20 Limitations
SR20_FM02_1224
12378-001 REV A
Baggage Compartment Door, inside:
Baggage Compartment, aft edge:
AND WEIGHT AND BALANCE INFORMATION
SEE AIRPLANE FLIGHT MANUAL FOR BAGGAGE TIE-DOWN
BAGGAGE STRAP CAPACITY IS 35 LBS EACH MAXIMUM
DISTRIBUTED FLOOR LIMIT 130 LBS
REMOVE CARPET AND ACCESS PANEL
ELT LOCATED BEHIND BULKHEAD
Figure 2-5
Placards (Sheet 7 of 9)
March 2010
2-26 Information Manual
Section 2 Cirrus Design
Limitations SR20
Figure 2-5
C.A.P.S. PARACHUTE RECOVERY SYSTEM
THIS AIRCRAFT IS EQUIPPED WITH A
12390-001
IN INJURY OR DEATH
USE OF THIS DEVICE COULD RESULT
135 KIAS
3. ACTIVATION HANDLE...........PULL DOWN AND
MAXIMUM DEMONSTRATED DEPLOYMENT SPEED
MUST BE WORN AT ALL TIMES
SEAT BELT AND SHOULDER HARNESS
USE FOR EXTREME EMERGENCIES ONLY
6. RESTRAINT SYSTEM............SECURE
5. MASTER SWITCH........................OFF
4. FUEL SELECTOR HANDLE........OFF
ACTIVATION PROCEDURES
!
WARNING
CAPS Deployment Handle Cover, above pilot's right shoulder:
FWD WITH BOTH HANDS
2. THIS COVER.........................................REMOVE
1. FUEL MIXTURE...........................IDLE CUT-OFF
CIRRUS AIRFRAME PARACHUTE SYSTEM
THIS AIRCRAFT IS EQUIPPED WITH A
12390-002
IN INJURY OR DEATH
USE OF THIS DEVICE COULD RESULT
135 KIAS
3. ACTIVATION HANDLE...........PULL DOWN AND
MAXIMUM DEMONSTRATED DEPLOYMENT SPEED
MUST BE WORN AT ALL TIMES
SEAT BELT AND SHOULDER HARNESS
USE FOR EXTREME EMERGENCIES ONLY
6. RESTRAINT SYSTEM............SECURE
5. MASTER SWITCH........................OFF
4. FUEL SELECTOR HANDLE........OFF
　
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