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ROCKET FOR PARACHUTE DEPLOYMENT INSIDE
Wing, adjacent to fuel filler caps:
SR22_FM02_2680
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
March 2010
Cirrus Design Section 2
SR22 Limitations
Information Manual 2-23
Figure 2-3
Placards (Sheet 2 of 6)
OPEN
TO
PUSH
L EU F O N
L EU F O N
L EU F ON
DE-ICING FLUIDS
REFER TO AFM FOR APPROVED
DE-ICING FLUID
EXTERNAL
POWER
28 V DC
NO PUSH
Wing, adjacent to fluid filler cap:
Left fuselage, on external power supply door:
Serials w/ Ice Protection.
Elevator and Rudder, both sides:
SR22_FM02_2681
Doors, above and below latch:
March 2010
2-24 Information Manual
Section 2 Cirrus Design
Limitations SR22
Figure 2-4
(Sheet 3 of 6)
CREW SEATS MUST BE LOCKED IN POSITION AND
CONTROL HANDLES FULLY DOWN BEFORE FLIGHT
RICH
OFF
LIFT BUTTON FOR OFF POSITION
P
O
W
E
R
OFF
TURN BOOST PUMP
ON DURING TAKE OFF,
CLIMB, LANDING AND
SWITCHING FUEL TANKS.
RIGHT
46 U.S.
GALLONS
USABLE
LEFT
46 U.S.
GALLONS
USABLE
CUTOFF
PUMP
FUEL
PRIME
BOOST
F
R
I
C
T
I
O
N
IDLE
M
I
X
T
U
R
E
MAX
ALTITUDE GPH
16000 ----- 17
12000 ----- 18
SL ----- 27
MAX POWER FUEL FLOWS
8000 ----- 21
4000 ----- 24
Engine control panel:
SR22_FM02_2682
March 2010
Cirrus Design Section 2
SR22 Limitations
Information Manual 2-25
Figure 2-5
(Sheet 4 of 6)
NO STEP
RESCUE: FRACTURE AND REMOVE WINDOW
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
MANEUVERING
SPEED: Vo 133 KIAS
NORMAL CATEGORY AIRPLANE
NO ACROBATIC MANEUVERS,
INCLUDING SPINS, APPROVED
Instrument Panel, left :
Bolster Switch Panel, left edge:
Cabin Door Window, lower edge, centered, applied upside down:
Wing, flap aft edge and fuselage vortex generator:
SR22_FM02_2683
March 2010
2-26 Information Manual
Section 2 Cirrus Design
Limitations SR22
Figure 2-6
(Sheet 5 of 6)
Instrument Panel, center:
DISPLAY
BACKUP
GRAB HERE
Bolster Panel, both sides:
ELT LOCATED BEHIND BULKHEAD
REMOVE CARPET AND ACCESS PANEL
Baggage Compartment, aft edge:
FIRE EXTINGUISHER FORWARD LEFT OF PILOT SEAT
FASTEN SEATBELTS • NO SMOKING
Instrument Panel:
EMERGENCY EXIT
REMOVE EGRESS HAMMER FROM WITHIN
CENTER ARMREST LID. STRIKE CORNER OF
WINDOW. KICK OR PUSH OUT AFTER FRACTURING
Cabin Window, above door latch:
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:
SR22_FM02_2684
March 2010
Cirrus Design Section 2
SR22 Limitations
Information Manual 2-27
Figure 2-7
(Sheet 6 of 6)
6. RESTRAINT SYSTEM............SECURE
5. MASTER SWITCH........................OFF
4. FUEL SELECTOR HANDLE........OFF
DO NOT JERK HANDLE
BOTH HANDS, MAXIMUM FORCE, STEADY PULL
3. ACTIVATION HANDLE.........PULL STRAIGHT DOWN
2. THIS COVER............................................REMOVE
1. FUEL MIXTURE.......................................CUT-OFF
ACTIVATION PROCEDURE
CIRRUS AIRFRAME PARACHUTE SYSTEM
133 KIAS
MAXIMUM DEMONSTRATED DEPLOYMENT SPEED
IN INJURY OR DEATH
USE OF THIS DEVICE COULD RESULT
MUST BE WORN AT ALL TIMES
SEAT BELT AND SHOULDER HARNESS
USE FOR EXTREME EMERGENCIES ONLY
WARNING
!
CAPS Deployment Handle Cover, above pilot's right shoulder:
SR22_FM02_2685
March 2010
2-28 Information Manual
Section 2 Cirrus Design
Limitations SR22
March 2010
Intentionally Left Blank
Information Manual 3-1
Cirrus Design Section 3
SR22 Emergency Procedures
Section 3
Emergency Procedures
Table of Contents
Introduction ........................................................................................ 3
Emergency Procedures Guidance ..................................................... 4
　
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