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marks, placards, and minor trim. Refer to SR22 Airplane Maintenance
Manual (AMM), Chapter 51, for specific paint requirements.
Other Limitations
Smoking
Smoking is prohibited in this airplane.
June 2007
Information Manual 2-21
Cirrus Design Section 2
SR22 Limitations
Placards
Upper fuselage, either side of CAPS rocket cover:
WARNING!
STAY CLEAR WHEN AIRPLANE IS OCCUPIED
ROCKET FOR PARACHUTE DEPLOYMENT INSIDE
Serials 0550 & subs.
Y
B A T O T EL B A S U ) S RE T I L 9 8 ( . S L A G . S. U 23.5
TI CAPA C EL BAS U LAT OT )S RET I L 35 1 ( .S LAG .S .U 40.5
4 0 0-8 46 51
0 0 1 RO L L 0 0 1 E D A RG N I M S A G VA
AVGAS MIN GRADE 100LL OR 100
40.5 U.S. GALS. (153 LITERS) TOTAL USABLE CAP
23.5 U.S. GALS. (89 LITERS) USABLE TO TAB
Serials 0002 thru 0549.
Wing, adjacent to fuel filler caps:
SR22_FM02_1372B
Engine compartment, inside oil filler access:
ENGINE OIL GRADE
ABOVE 40° F SAE 50 OR 20W50 OR 20W60
BELOW 40° F SAE 30 OR 10W30, 15W50, OR 20W50
REFER TO AFM FOR APPROVED OILS
Figure 2-5
Placards (Sheet 1 of 7)
June 2007
2-22 Information Manual
Section 2 Cirrus Design
Limitations SR22
Figure 2-5
OPEN
TO
PUSH
Serials 0821 & subs.
DE-ICING FLUIDS
REFER TO AFM FOR APPROVED
DE-ICING FLUID
Left fuselage, on external
power supply door:
EXTERNAL
POWER
28 V DC
Serials 0334 & subs w/ Ice Protection.
ESO LC
E P O
N
Serials 0522 thru 0820.
L EU F O N
L EU F ON
L EU F ON
Serials 0002 thru 0521.
OPEN
CLOSE
Serials 0334 & subs w/ Ice Protection.
Elevator, Rudder, & Elec. Trim Tab (if installed), both sides:
NO PUSH
SR22_FM02_1373A
Doors, above and below latch:
Placards (Sheet 2 of 7)
June 2007
Information Manual 2-23
Cirrus Design Section 2
SR22 Limitations
104 KIAS
100%
119 KIAS
50%
UP
Engine control panel:
SR22_FM02_1374C
N
O
I
T
C
I
R
F
M
I
X
T
U
R
E
Serials 0334 thru 0434.
Serials 0002 & subs.
Serials 0410 & subs
& serials 0002 thru 0409
after incorporating SA 02-13.
MAX
NORMAL
ICE PROTECTION
OFF
CONTROL HANDLES FULLY DOWN BEFORE FLIGHT
CREW SEATS MUST BE LOCKED IN POSITION AND
OFF
LIFT BUTTON FOR OFF POSITION
OFF
TURN BOOST
PUMP ON
BEFORE SWITCHING
FUEL TANKS
RIGHT
40.5 U.S.
GALLONS
USABLE
LEFT
40.5 U.S.
GALLONS
USABLE
13614-001
FUEL
PUMP
PRIME
BOOST
P
O
W
E
R
IDLE CUTOFF
RICH
MAX
FLAPS
Figure 2-5
Placards (Sheet 3 of 7)
June 2007
2-24 Information Manual
Section 2 Cirrus Design
Limitations SR22
Figure 2-5
ALTITUDE GPH
16000 17
12000 18
8000 21
4000 24
SL 27
MAX POWER FUEL FLOWS
Instrument Panel Upper Right:
Instrument Panel Upper left:
INCLUDING APPROVED
NO
NORMAL CATEGORY AIRPLANE
SPINS,
ACROBATIC MANEUVERS,
133 KIAS SPEED: Vo
MANEUVERING
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
Cabin Door Window, lower edge, centered, applied upside down:
RESCUE: FRACTURE AND REMOVE WINDOW
Wing, flap aft edge and fuselage vortex generator:
NO STEP
SR22_FM02_1375C
Placards (Sheet 4 of 7)
June 2007
Information Manual 2-25
Cirrus Design Section 2
SR22 Limitations
SR22_FM02_1376C
Serials 0656 & subs.
GRAB HERE
Bolster Panel, both sides:
ELT LOCATED BEHIND BULKHEAD
REMOVE CARPET AND ACCESS PANEL
Baggage Compartment, aft edge:
DISTRIBUTED FLOOR LIMIT 130 LBS
BAGGAGE STRAP CAPACITY IS 35 LBS EACH MAXIMUM
SEE AIRPLANE FLIGHT MANUAL FOR BAGGAGE TIE-DOWN
AND WEIGHT AND BALANCE INFORMATION
Baggage Compartment Door, inside:
12378-001 REV A
Figure 2-5
Placards (Sheet 5 of 7)
June 2007
2-26 Information Manual
Section 2 Cirrus Design
Limitations SR22
Figure 2-5
SR22_FM02_1517C
Serials 0002 thru 0168.
EMERGENCY EXIT
REMOVE EGRESS HAMMER FROM ARMREST LID
STRIKE CORNER OF WINDOW,
KICK OR PUSH OUT AFTER FRACTURING
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AIRPLANE INFORMATION MANUAL for the CIRRUS DESIGN SR22(10)
