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weight of the airplane and its contents as listed in the aircraft
specifications.
• Moment is the product of the weight of an item multiplied by
its arm.
• Useful Load is the basic empty weight subtracted from the
maximum weight of the aircraft. It is the maximum allowable
combined weight of pilot, passengers, fuel and baggage.
March 2010
1-12 Information Manual
Section 1 Cirrus Design
General SR20
• Station is a location along the airplane fuselage measured
in inches from the reference datum and expressed as a
number. For example: A point 123 inches aft of the reference
datum is Fuselage Station 123.0 (FS 123).
• Reference Datum is an imaginary vertical plane from which
all horizontal distances are measured for balance purposes.
• Tare is the weight of all items used to hold or position the
airplane on the scales for weighing. Tare includes blocks,
shims, and chocks. Tare weight must be subtracted from the
associated scale reading.
March 2010
Information Manual 2-1
Cirrus Design Section 2
SR20 Limitations
Section 2
Limitations
Table of Contents
Introduction .....................................................................................2-3
Certification Status..........................................................................2-3
Airspeed Limitations........................................................................2-4
Airspeed Indicator Markings ...........................................................2-5
Power Plant Limitations ..................................................................2-6
Engine..........................................................................................2-6
Propeller ......................................................................................2-7
Weight Limits ..................................................................................2-7
Instrument Markings .......................................................................2-8
Center of Gravity Limits ..................................................................2-9
Maneuver Limits............................................................................2-10
Flight Load Factor Limits...............................................................2-10
Minimum Flight Crew ....................................................................2-10
Kinds of Operation ........................................................................2-11
Kinds of Operation Equipment List ............................................2-11
Icing ...........................................................................................2-15
Runway Surface ........................................................................2-15
Instrument Procedures ..............................................................2-16
Taxi Power.................................................................................2-16
Fuel Limits.....................................................................................2-16
Altitude Limits................................................................................2-16
Environmental Conditions .............................................................2-16
Maximum Occupancy ...................................................................2-16
Systems and Equipment Limits.....................................................2-17
Cirrus Airframe Parachute System (CAPS) ...............................2-17
Primary Flight Display................................................................2-17
Multi-Function Display ...............................................................2-19
Oxygen System .........................................................................2-20
Inflatable Restraint System........................................................2-20
Flap Limitations..........................................................................2-20
Paint...........................................................................................2-20
Other Limitations...........................................................................2-20
Smoking.....................................................................................2-20
March 2010
2-2 Information Manual
Section 2 Cirrus Design
Limitations SR20
Placards ........................................................................................2-21
March 2010
Information Manual 2-3
Cirrus Design Section 2
SR20 Limitations
Introduction
• Note •
Limitations associated with optional equipment are not
described in this section. For optional equipment limitations,
refer to Section 9, Supplements
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西锐20飞机信息手册CIRRUS DESIGN SR20 AIRPLANE INFORMATION MA(4)
