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illuminated.
AC
ON
SR22_FM09_2258A
AIRFLOW VENTS TEMPERATURE
Air Conditioner on.
Air Conditioning System Operation - Serials before G3 Wing
Revision 01: 03-27-07
P/N 13772-127 13 of 14
Cirrus Design Section 9
SR22 Supplements
1 2
3
OFF
COLD
HOT
NOTE: Illustration depicts settings for Emergency Procedures
Smoke and Fume Elimination.
Rotating the selector controls the volume of
airflow allowed into the cabin distribution
system through use of an electro-mechanical
linkage to a butterfly (hot air) valve in the
mixing chamber on the forward firewall.
When the airflow selector fan speed is
moved to the 1, 2, or 3 position the
electro-mechanical linkage actuates the
hot air valve to the full open position and
the 3-speed blower fan is turned on.
Shared airflow to the
defroster, cabin floor,
and panel outlets.
Maximum airflow to
the rear seat foot warmer
diffusers and the front
seat kickplate outlets.
Maximum airflow
to the panel and
armrest air gaspers.
Maximum airflow
to defroster.
Rotating the selector simultaneously
opens and closes the hot and fresh air
butterfly valves, permitting conditioned
(mixed) air to enter distribution system.
Air conditioning
mode.
AC ON illuminated.
Maximum air
conditioning
(recirculation)
mode. AC ON
illuminated.
AC
ON
SR22_FM09_2606
AIRFLOW VENTS TEMPERATURE
Air Conditioner on.
If source of smoke and fume is firewall forward, turn
Airflow Selector OFF.
Figure - 2 (Sheet 2 of 2)
Air Conditioning System Operation - Serials G3 and Subs
Revision 01: 03-27-07
14 of 14 P/N 13772-127
Section 9 Cirrus Design
Supplements SR22
Revision 01: 03-27-07
Intentionally Left Blank
13772-130 1 of 58
Cirrus Design Section 9
SR22 Supplements
Pilot’s Operating Handbook and
FAA Approved Airplane Flight Manual
Supplement
for
G3 Wing
When the G3 Wing is installed on the Cirrus Design SR22 serials
2334, 2420, 2438 and subsequent, this POH Supplement is applicable
and must be inserted in the Supplements Section (Section 9) of the
Cirrus Design SR22 Pilot’s Operating Handbook. This document must
be carried in the airplane at all times. Information in this supplement
adds to, supersedes, or deletes information in the basic SR22 Pilot’s
Operating Handbook.
Original: 03-27-07
2 of 58 13772-130
Section 9 Cirrus Design
Supplements SR22
Original: 03-27-07
Intentionally Left Blank
13772-130 3 of 58
Cirrus Design Section 9
SR22 Supplements
Section 1 - General
The G3 Wing is constructed in a conventional spar, rib, and shear
section arrangement. The upper and lower skins are bonded to the
spar, ribs, and aft shear web forming a torsion box that carries all of
the wing bending and torsion loads. The rear shear webs are similar in
construction but do not carry through the fuselage. The main spar is
laminated epoxy/carbon fiber in a C-section, and is continuous from
wing tip to wing tip. The wing spar passes under the fuselage below
the two front seats and is attached to the fuselage in two locations. Lift
and landing loads are carried by the single carry-through spar, plus a
pair of rear shear webs (one on each wing) attached to the fuselage.
G3 Wing geometry is slightly changed with an 1° increase in dihedral
which allows for the elimination of the aileron-rudder interconnect
system.
The CG Envelope (Center of Gravity Envelope) is expanded to allow
for slightly more forward loading at higher gross weights.
The main landing gear is moved slightly inboard and the strut angle
increased to achieve an increase in airplane height of 1.5 inches.
The ice protection system’s glycol tank is moved from the fuselage to
an integral tank on the left wing and the porous panels are lengthened
to cover the entire leading edge of the wing.
Other G3 Wing updates include:
• Increased fuel capacity,
• wing tip with integral, leading edge recognition lights.
• relocation of the fresh air inlets to the engine cowl and related
environmental system changes,
• improved trailing edge aerodynamics
• improved wing root fairings,
• relocation of the stall warning port.
Original: 03-27-07
4 of 58 13772-130
Section 9 Cirrus Design
Supplements SR22
Figure - 1
9.1 ft. (2.77 m)
0.5 ft. (0.15 m)
24.3 ft. (7.41 m)
RADIUS FOR NOSE GEAR 7.0 ft. (2.16 m)
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AIRPLANE INFORMATION MANUAL for the CIRRUS DESIGN SR22(138)
