Sharp R-360ES podręczniki

Sharp R-360ES Dokumentacja (392 strony)

Marka: Sharp | Kategoria: Kuchenki mikrofalowe | Rozmiar: 4.94 MB |

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CIRRUS DESIGN SR20

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Cirrus Design Corporation

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4515 Taylor Circle

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Duluth, MN 55811

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Section 1

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Figure 1-1

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Airplane Three View

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Figure 1-2

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Turning Radius

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The Airplane

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P/N 13999-002 Info Manual 1-7

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Cirrus Design Section 1

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SR20 General

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Meteorological Terminology

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Engine Power Terminology

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Section 1 Cirrus Design

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General SR20

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Section 2

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Limitations

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Certification Status

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Airspeed Limitations

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Airspeed Indicator Markings

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Power Plant Limitations

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Weight Limits

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Instrument Markings

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Center of Gravity Limits

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Maneuver Limits

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Flight Load Factor Limits

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Minimum Flight Crew

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Kinds of Operation

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Runway Surface

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Fuel Limits

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Altitude Limits

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Environmental Conditions

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Maximum Occupancy

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Systems and Equipment Limits

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Oxygen System

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Inflatable Restraint System

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Flap Limitations

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Other Limitations

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Placards

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EXTERNAL

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SR20_FM02_1222E

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SR20_FM02_1520B

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Figure 2-5

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Placards (Sheet 5 of 9)

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GRAB HERE

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Placards (Sheet 7 of 9)

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12390-001

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12390-002

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Placards (Sheet 9 of 9)

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Section 3

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Emergency Procedures

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3-2 P/N 13999-002 Info Manual

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Section 3 Cirrus Design

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Emergency Procedures SR20

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3-4 P/N 13999-002 Info Manual

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Emergency Procedures Guidance

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Memory Items

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Ground Emergencies

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Emergency Ground Egress

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In-Flight Emergencies

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Maximum Glide

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Engine Failure In Flight

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Engine Airstart

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Engine Partial Power Loss

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Low Oil Pressure

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Propeller Governor Failure

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Smoke and Fume Elimination

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Engine Fire In Flight

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Wing Fire In Flight

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Cabin Fire In Flight

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Emergency Descent

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Cirrus Design Section 3

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SR20 Emergency Procedures

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CAPS Deployment

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• WARNING •

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Landing Emergencies

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Ditching

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System Malfunctions

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Vacuum System Failure

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Section 3A

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Abnormal Procedures

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Abnormal Procedures Guidance

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Ground Procedures

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Landing Procedures

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Cirrus Design Section 3A

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SR20 Abnormal Procedures

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Communications Failure

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Pitot Static Malfunction

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Section 3A Cirrus Design

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Abnormal Procedures SR20

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Section 4

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Normal Procedures

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4-4 P/N 13999-002 Info Manual

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Preflight Walk-Around

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P/N 13999-002 Info Manual 4-7

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4-8 P/N 13999-002 Info Manual

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P/N 13999-002 Info Manual 4-9

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Before Starting Engine

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Starting Engine

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Before Taxiing

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Before Takeoff

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Normal Takeoff

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Short Field Takeoff

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Section 4 Cirrus Design

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Normal Procedures SR20

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September 2011

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Cirrus Design Section 4

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SR20 Normal Procedures

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Cruise Leaning

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Before Landing

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Balked Landing/Go-Around

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After Landing

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Shutdown

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Environmental Considerations

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Hot Weather Operation

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Fuel Conservation

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Section 5

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Performance Data

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5-2 P/N 13999-002 Info Manual

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Section 5 Cirrus Design

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Performance Data SR20

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Introduction

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Flight Planning

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Sample Problem

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P/N 13999-002 Info Manual 5-5

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Cirrus Design Section 5

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SR20 Performance Data

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5-6 P/N 13999-002 Info Manual

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P/N 13999-002 Info Manual 5-7

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Fuel Required

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P/N 13999-002 Info Manual 5-9

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Airspeed Calibration

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Altitude Correction

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Temperature Conversion

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Outside Air Temperature

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ISA Condition

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Stall Speeds

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Wind Components

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Takeoff Distance

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Takeoff Climb Gradient

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Takeoff Rate of Climb

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Enroute Climb Gradient

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Enroute Rate of Climb

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Figure 5-14

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Figure 5-15

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Factors:

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Cruise Performance

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Range / Endurance Profile

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Balked Landing Climb Gradient

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Balked Landing Rate of Climb

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Landing Distance

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Section 6

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Weight and Balance

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Intentionally Left Blank

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Figure 6-1

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Airplane Dimensional Data

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Figure 6-2

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Airplane Leveling

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Airplane Weighing Form

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Airplane Weighing Procedures

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6-8 P/N 13999-002 Info Manual

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Section 6 Cirrus Design

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Weight & Balance SR20

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P/N 13999-002 Info Manual 6-9

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Cirrus Design Section 6

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SR20 Weight & Balance

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Weight & Balance Record

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Figure 6-5

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Airplane Interior Dimensions

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Loading Instructions

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Figure 6-6

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Loading Data

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Moment Limits

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Equipment List

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Section 7

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7-2 P/N 13999-002 Info Manual

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Section 7 Cirrus Design

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Airplane Description SR20

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P/N 13999-002 Info Manual 7-3

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Airframe

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Empennage

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Flight Controls

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Figure 7-1

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Elevator Control System

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Aileron System

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Figure 7-2

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Aileron Control System

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Rudder System

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Figure 7-3

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Rudder Control System

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Trim Systems

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Yaw Trim System

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Flight Deck Arrangement

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Instrument Panel and Console

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Figure 7-4

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Flight Instruments

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Vertical Speed Indicator

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Altimeter

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Turn Coordinator

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Directional Gyro

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Course Deviation Indicator

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Magnetic Compass

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Wing Flaps

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Figure 7-5

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Flap Control System

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Landing Gear

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Airplane Cabin

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Figure 7-6

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Cabin General Arrangement

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Cirrus Design Section 7

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SR20 Airplane Description

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Windshield and Windows

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Cabin Safety Equipment

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Engine Oil System

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Engine Cooling

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Engine Fuel Injection

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Engine Air Induction System

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Engine Fuel Ignition

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Engine Exhaust

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Engine Controls

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Alternate Air Control

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Engine Indicating

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Figure 7-7

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Propeller

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Fuel System

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Figure 7-8

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Fuel Selector Valve

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Fuel Quantity Indicator

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Fuel Flow Indication

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Fuel Caution Light

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Boost Pump Switch

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Brake System

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Figure 7-9

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Electrical System

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Figure 7-10

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Power Distribution

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BAT & ALT Master Switches

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Avionics Power Switch

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Volt / Amp Meter

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Low Volts Warning Light

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Circuit Breakers and Fuses

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Ground Service Receptacle

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Convenience Outlet

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Exterior Lighting

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Interior Lighting

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Environmental System

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Figure 7-11

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Heating and Ventilation

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Cabin Heat Control

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Cabin Cooling Control

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Cabin Air Selector

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Figure 7-12

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Pitot-Static System

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Vacuum System

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Figure 7-13

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Suction Gauge

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Vacuum Warning Light

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Aux Vac Caution Light

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Stall Warning System

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Standard Avionics

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Multi-Function Display

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Autopilot

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GPS Navigation

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Navigation (Nav) Receiver

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Transponder

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Audio System

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Emergency Locator Transmitter

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Hour Meter

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Digital Clock

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System Description

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Activation Handle

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Deployment Characteristics

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Section 8

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Operator’s Publications

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Ordering Publications

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P/N 13999-002 Info Manual 8-5

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Cirrus Design Section 8

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Airworthiness Directives

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Airplane Inspection Periods

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100-Hour Inspection

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8-8 P/N 13999-002 Info Manual

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Section 8 Cirrus Design

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P/N 13999-002 Info Manual 8-9

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Ground Handling

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Leveling

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Servicing

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Tire Inflation

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Propeller Servicing

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Oil Servicing

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Figure 8-1

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Approved Oils

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Fuel System Servicing

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Draining Fuel System

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Battery Service

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Cleaning and Care

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Figure 8-2

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Cleaning Interior Surfaces

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Figure 8-3

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Section 9

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Supplements

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Log of Supplements

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Garmin GMA 340 Audio System

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Section 1 - General

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Audio/Transceiver Selection

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Speaker Output

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Public Address (PA) Function

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Personal Music Inputs

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Intercom

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P/N 11934-S01 7 of 10

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Cirrus Design Section 9

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SR20 Supplements

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Revision 02: 07-18-05

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Marker Beacon

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P/N 11934-S01 9 of 10

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10 of 10 P/N 11934-S01

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Section 9 Cirrus Design

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Supplements SR20

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Dual Alternator System

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Section 2 - Limitations

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Alternator Failure

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4 of 10 P/N 11934-S10

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Original: 09-28-99

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Section 5 - Performance

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Power Generation

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Low-Volts Warning Light

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ALT FAIL Lights

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10 of 10 P/N 11934-S10

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L-3 Avionics Systems WX500

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Stormscope Sensor

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Section 1 General

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Garmin GTX 327 Transponder

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Section 4 - Normal Procedures

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Mode Selector Keys

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Code Selector Keys

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Reply Light

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IDENT Key

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FUNC Key

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8 of 8 P/N 11934-S12

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Original: 12-26-00

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S-Tec System 55X Autopilot

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4 of 16 P/N 11934-S13

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Revision 04: 08-15-07

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Figure - 1

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Autopilot Malfunction

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P/N 11934-S13 7 of 16

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In-Flight Procedures

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10 of 16 P/N 11934-S13

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P/N 11934-S13 11 of 16

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12 of 16 P/N 11934-S13

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14 of 16 P/N 11934-S13

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P/N 11934-S13 15 of 16

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16 of 16 P/N 11934-S13

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Traffic Advisory System

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Respond to Traffic Advisories

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6 of 6 P/N 11934-S15

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Revision 01: 10-12-05

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Garmin GNS 430 GPS Navigator

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Section 2 – Limitations

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GNS 430 Integration

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6 of 10 P/N 11934-S22

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Revision 02: 08-15-07

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GPS Navigator

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TERRAIN Interface*

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Garmin GNC 420 GPS Navigator

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Honeywell KGP 560 Terrain/

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Awareness Warning System

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Activate TAWS

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6 of 12 P/N 11934-S30

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Revision 01: 12-15-07

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TAWS Annunciator Panel

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Alert Priority

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Advisory Callout

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Figure - 2

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10 of 12 P/N 11934-S30

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P/N 11934-S30 11 of 12

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Self Test

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Avidyne EMax™ Engine

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Instrumentation

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4 of 4 P/N 11934-S31

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Avidyne CMax™ Electronic

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Approach Charts

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4 of 4 P/N 11934-S32

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XM Satellite Weather System

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4 of 4 P/N 11934-S33

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Section 10

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Safety Information

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Deployment

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Cirrus Design Section 10

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SR20 Safety Information

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Landing Considerations

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Section 10 Cirrus Design

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Safety Information SR20

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Proper Operating Practices

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Brake Maintenance

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