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the pilot must:
• Use an oxygen system approved by Cirrus Design and listed in
the Oxygen System AFM Supplement Part Number 13772-109.
• Secure the oxygen bottle in the right front seat as described in
the AFM Supplement noted above.
Inflatable Restraint System
Serials 0002 thru 1499, 1501 thru 1519 after SB 2X-25-14 and serials
1500, 1520 and subsequent; Use of a child safety seat with the
inflatable restraint system is prohibited.
Flap Limitations
Serials 0002 through 0227 before accomplishment of Service Bulletin
SB 22-27-02: Simultaneous Flap operation and COM transmission is
prohibited.
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.
Revision A8
P/N 13772-001 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 thru 2333, 2335 thru 2419, 2421 thru 2437.
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_1372C
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)
Revision A8
2-22 P/N 13772-001
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)
Revision A5
P/N 13772-001 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)
Revision A5
2-24 P/N 13772-001
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:
　
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