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RESCUE: FRACTURE AND REMOVE WINDOW
Wing, flap aft edge and fuselage vortex generator:
NO STEP
SR22_FM02_1375C
Placards (Sheet 4 of 7)
Revision A5
P/N 13772-001 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)
Revision A5
2-26 P/N 13772-001
Section 2 Cirrus Design
Limitations SR22
Figure 2-5
FASTEN SEAT BELT • NO SMOKING
FIRE EXTINGUISHER FORWARD LEFT OF PILOT SEAT
SR22_FM02_1517E
Serials 0002 thru 0168.
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:
FIRE EXTINGUISHER UNDER PILOT SEAT FRONT
FASTEN SEATBELTS
NO SMOKING
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:
Serials 0169 & subs.
Serials 1863 & subs.
Serials 0002 thru 1862.
Placards (Sheet 6 of 7)
Revision A9
P/N 13772-001 2-27
Cirrus Design Section 2
SR22 Limitations
FWD WITH BOTH HANDS
SEAT BELT AND SHOULDER HARNESS
MUST BE WORN AT ALL TIMES
CIRRUS AIRFRAME PARACHUTE SYSTEM
THIS AIRCRAFT IS EQUIPPED WITH A
6. RESTRAINT SYSTEM............SECURE
5. MASTER SWITCH........................OFF
4. FUEL SELECTOR HANDLE........OFF
3. ACTIVATION HANDLE................PULL DOWN AND
2. THIS COVER............................................REMOVE
1. FUEL MIXTURE.......................................CUT-OFF
ACTIVATION PROCEDURES
133 KIAS
MAXIMUM DEMONSTRATED DEPLOYMENT SPEED
USE OF THIS DEVICE COULD RESULT
IN INJURY OR DEATH
USE FOR EXTREME EMERGENCIES ONLY
WARNING
!
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
!
incorporating SB 22-95-03.
& 0002 thru 0209 after
Serials 0210 & subs
before SB 22-95-03.
Serials 0002 thru 0209
SR22_FM02_1437B
CAPS Deployment Handle Cover, above pilot's right shoulder:
Figure 2-5
Placards (Sheet 7 of 7)
Revision A5
2-28 P/N 13772-001
Section 2 Cirrus Design
Limitations SR22
Revision A5
Intentionally Left Blank
P/N 13772-001 3-1
Cirrus Design Section 3
SR22 Emergency Procedures
Section 3
Emergency Procedures
Table of Contents
Introduction .....................................................................................3-3
Airspeeds for Emergency Operations .............................................3-4
Emergency Procedures Guidance ..................................................3-5
Preflight Planning.........................................................................3-5
Preflight Inspections/Maintenance...............................................3-5
Methodology ................................................................................3-5
Memory Items ..............................................................................3-6
Ground Emergencies ......................................................................3-7
Engine Fire During Start ..............................................................3-7
Emergency Engine Shutdown On Ground...................................3-7
Emergency Ground Egress .........................................................3-8
In-Flight Emergencies .....................................................................3-9
Engine Failure On Takeoff (Low Altitude) ....................................3-9
Maximum Glide .............................................................................3-10
　
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