Cirrus DESIGN SR22T - Page 52

2-26 P/N 13772-003
Section 2 Cirrus Design
Limitations SR22T
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
ABOVE 17,500 V
NE
AND V
NO
MANEUVERING SPEED: Vo 133 KIAS
NORMAL CATEGORY AIRPLANE
NO ACROBATIC MANEUVERS,
INCLUDING SPINS, APPROVED
REDUCE LINEARLY WITH ALTITUDE:
V
NE
V
NO
17,500 200 177 KIAS
25,000 170 151 KIAS
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_3264
Revision 1