CIRRUS DESIGN SR22 - Page 38

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:
I
N
C
L
U
D
I
N
G
A
P
P
R
O
V
E
D
N
O
N
O
R
M
A
L
C
A
TE
G
O
R
Y
A
I
R
P
LA
N
E
S
P
I
N
S
,
A
C
R
O
B
A
T
I
C
M
A
N
E
U
V
E
R
S
,
133
K
I
A
S
S
P
E
E
D
:
V
o
M
A
N
E
U
V
E
R
I
N
G
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)
March 2010