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Altitude Limits................................................................................... 17
Environmental Conditions ................................................................ 17
Maximum Occupancy ...................................................................... 17
Systems and Equipment Limits........................................................ 18
Cirrus Perspective Integrated Avionics System............................ 18
L-3 Skywatch Traffic Advisory System ......................................... 20
L-3 Stormscope Weather Information System.............................. 20
Inflatable Restraint System........................................................... 20
Flap Limitations............................................................................. 21
Paint.............................................................................................. 21
Cirrus Airframe Parachute System (CAPS) .................................. 21
Other Limitations.............................................................................. 21
Smoking........................................................................................ 21
Placards ........................................................................................... 22
March 2010
2-2 Information Manual
Section 2 Cirrus Design
Limitations SR22
March 2010
Intentionally Left Blank
Cirrus Design Section 2
SR22 Limitations
Information Manual 2-3
Introduction
The limitations included in this Section of the Pilot’s Operating
Handbook (POH) are approved by the Federal Aviation Administration.
This section provides operating limitations, instrument markings and
basic placards required by regulation and necessary for the safe
operation of the aircraft and its standard systems and equipment.
Refer to Section 9 of this handbook for amended operating limitations
for airplanes equipped with optional equipment. Compliance with the
operating limitations in this section and in Section 9 is required by
Federal Aviation Regulations.
• Note •
Limitations associated with optional equipment are not
described in this section. For optional equipment limitations,
refer to Section 9, Supplements
Certification Status
The aircraft is certificated under the requirements of Federal Aviation
Regulations (FAR) Part 23 as documented by FAA Type Certificate TC
A00009CH.
March 2010
2-4 Information Manual
Section 2 Cirrus Design
Limitations SR22
Airspeed Limitations
The indicated airspeeds in the following table are based upon Section
5 Airspeed Calibrations using the normal static source. When using
the alternate static source, allow for the airspeed calibration variations
between the normal and alternate static sources.
Speed KIAS KCAS Remarks
VNE 200 204 Never Exceed Speed is the speed limit that
may not be exceeded at any time.
VNO 177 180 Maximum Structural Cruising Speed is the
speed that should not be exceeded except in
smooth air, and then only with caution.
VO
3400 Lb 133 135
Operating Maneuvering Speed is the maximum
speed at which full control travel may be
used. Below this speed the airplane stalls
before limit loads are reached. Above this
speed, full control movements can damage
the airplane.
VFE
50% Flaps
100% Flaps
119
104
120
104
Maximum Flap Extended Speed is the highest
speed permissible with wing flaps extended.
VPD 133 135 Maximum Demonstrated Parachute Deployment
Speed is the maximum speed at which
parachute deployment has been demonstrated.
March 2010
Cirrus Design Section 2
SR22 Limitations
Information Manual 2-5
Airspeed Indicator Markings
The airspeed indicator markings are based upon Section 5 Airspeed
Calibrations using the normal static source. When using the alternate
static source, allow for the airspeed calibration variations between the
normal and alternate static sources.
Marking
Value
(KIAS)
Remarks
White Arc 62 - 104 Full Flap Operating Range. Lower limit is the most
adverse stall speed in the landing configuration. Upper
limit is the maximum speed permissible with flaps
extended.
Green Arc 73 - 177 Normal Operating Range. Lower limit is the maximum
weight stall at most forward CG with flaps retracted.
Upper limit is the maximum structural cruising speed.
Yellow Arc 177 - 200 Caution Range. Operations must be conducted with
caution and only in smooth air.
Red Line 200 Never exceed speed. Maximum speed for all operations.
March 2010
2-6 Information Manual
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西锐20飞机信息手册 SR22 AIRPLANE INFORMATION MANUAL 2979(5)
