西锐20飞机信息手册AIRPLANE INFORMATION MANUAL for the CIRRUS DESIGN SR20 1268－

航空发表于 2010-10-23 11:31:34

西锐20飞机信息手册AIRPLANE INFORMATION MANUAL for the CIRRUS DESIGN SR20 Aircraft Serials 1268 and Subsequent
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航空发表于 2010-10-23 11:40:01

AIRPLANE INFORMATION MANUAL for the CIRRUS DESIGN SR20 A l l - E l e c t r i c S R 2 0 A i r c r a f t S e r i a l s 1 2 6 8 a n d S u b s e q u e n t • NOTE • At the time of issuance, this Information Manual was harmonized with the SR20 Pilot's Operating Handbook Rev A9 (P/N 11934-003), and will not be kept current. Therefore, this Information Manual is for reference only and cannot be used as a substitute for the official Pilot's Operating Handbook and FAA Approved Airplane Flight Manual. Information Manual P/N 13999-003 March 2010 Copyright © 2001 - All Rights Reserved Cirrus Design Corporation 4515 Taylor Circle Duluth, MN 55811 Information Manual 1-1 Cirrus Design Section 1 SR20 General Section 1 General Table of Contents Introduction .....................................................................................1-3 The Airplane....................................................................................1-6 Engine..........................................................................................1-6 Propeller ......................................................................................1-6 Fuel..............................................................................................1-7 Oil ...............................................................................................1-7 Maximum Certificated Weights ....................................................1-7 Cabin and Entry Dimensions .......................................................1-7 Baggage Spaces and Entry Dimensions .....................................1-7 Specific Loadings.........................................................................1-7 Symbols, Abbreviations and Terminology.......................................1-8 General Airspeed Terminology and Symbols ..............................1-8 Meteorological Terminology.........................................................1-9 Engine Power Terminology........................................................1-10 Performance and Flight Planning Terminology..........................1-10 Weight and Balance Terminology..............................................1-11 March 2010 1-2 Information Manual Section 1 Cirrus Design General SR20 Intentionally Left Blank March 2010 Information Manual 1-3 Cirrus Design Section 1 SR20 General Introduction This section contains information of general interest to pilots and owners. You will find the information useful in acquainting yourself with the airplane, as well as in loading, fueling, sheltering, and handling the airplane during ground operations. Additionally, this section contains definitions or explanations of symbols, abbreviations, and terminology used throughout this handbook. • Note • For specific information regarding the organization of this Handbook, revisions, supplements, and procedures to be used to obtain revision service for this handbook, refer to the “Foreword” immediately following the title page March 2010 1-4 Information Manual Section 1 Cirrus Design General SR20 Figure 1-1 76" 2-BLADE 74" 3-BLADE 35.5' 11.0' 9.2' 7" 26.0' SR20_FM01_1004A NOTE: • Wing span includes position and strobe lights. • Prop ground clearance at 3000 lb - 7" (2 blade), 8" (3 blade). • Wing Area = 135.2 sq. ft. Airplane Three View March 2010 Information Manual 1-5 Cirrus Design Section 1 SR20 General 23' 11" 9' 11" SR20_FM01_1002 GROUND TURNING CLEARANCE TURNING RADII ARE CALCULATED USING ONE BRAKE AND PARTIAL POWER. ACTUAL TURNING RADIUS MAY VARY AS MUCH AS THREE FEET. -RADIUS FOR WING TIP -RADIUS FOR INSIDE GEAR 6" -RADIUS FOR OUTSIDE GEAR -RADIUS FOR NOSE GEAR 12' 2" Figure 1-2 Turning Radius March 2010 1-6 Information Manual Section 1 Cirrus Design General SR20 The Airplane Engine Number of Engines..............................................................................1 Number of Cylinders............................................................................6 Engine Manufacturer ........................................... Teledyne Continental Engine Model........................................................................IO-360-ES Fuel Metering.................................................................... Fuel Injected Engine Cooling .....................................................................Air Cooled Engine Type....................................Horizontally Opposed, Direct Drive Horsepower Rating................................................200 hp @ 2700 rpm Propeller Hartzell Propeller Type..............................................................Constant Speed Two-Blade Propeller: Model Number ...................................................BHC-J2YF-1BF/F7694 Diameter .............................................................76.0” (73.0” Minimum) Three-Blade Propeller: Model Number ...............................................PHC-J3YF-1MF/F7392-1 Diameter .............................................................74.0” (72.0” Minimum) Model Number ............................................... PHC-J3YF-1RF/F7392-1 Diameter .............................................................74.0” (72.0” Minimum) March 2010 Information Manual 1-7 Cirrus Design Section 1 SR20 General Fuel Total Capacity.............................................60.5 U.S. Gallons (229.0 L) Total Usable...................................................56 U.S. Gallons (212.0 L) Approved Fuel Grades: 100 LL Grade Aviation Fuel (Blue) 100 (Formerly 100/130) Grade Aviation Fuel (Green) Oil Oil Capacity (Sump) .............................................8 U.S. Quarts (7.6 L) Oil Grades: All Temperatures ............................................SAE 15W-50 or 20W-50 Below 40 F (4 C)................................................... SAE 30 or 10W-30 Above 40 F (4 C) ....................................................................SAE 50 Maximum Certificated Weights Maximum Gross for Takeoff...................................... 3000 lb (1361 Kg) Maximum Landing Weight ........................................ 2900 lb (1315 Kg) Maximum Baggage Compartment Loading.................... 130 lb (59 Kg) Standard Empty Weight ............................................. 2050 lb (930 Kg) Maximum Useful Load.................................................. 950 lb (431 Kg) Full Fuel Payload.......................................................... 622 lb (282 Kg) Cabin and Entry Dimensions Dimensions of the cabin interior and entry door openings are illustrated in detail in Section 6. Baggage Spaces and Entry Dimensions Dimensions of the baggage area and baggage door opening are illustrated in detail in Section 6. Specific Loadings Wing Loading .................................................... 22.2 lb per square foot Power Loading................................................................. 15.0 lb per hp March 2010 1-8 Information Manual Section 1 Cirrus Design General SR20 Symbols, Abbreviations and Terminology General Airspeed Terminology and Symbols KCAS Knots Calibrated Airspeed is the indicated airspeed corrected for position and instrument error. Calibrated airspeed is equal to true airspeed in standard atmosphere at sea level. KIAS Knots Indicated Airspeed is the speed shown on the airspeed indicator. The IAS values published in this handbook assume no instrument error. KTAS Knots True Airspeed is the airspeed expressed in knots relative to undisturbed air which is KCAS corrected for altitude and temperature. VG Best Glide Speed is the speed at which the greatest flight distance is attained per unit of altitude lost with power off. VO Operating Maneuvering Speed is the maximum speed at which application of full control movement will not overstress the airplane. VFE Maximum Flap Extended Speed is the highest speed permissible with wing flaps in a prescribed extended position. VNO Maximum Structural Cruising Speed is the speed that should not be exceeded except in smooth air, and then only with caution. VNE Never Exceed Speed is the speed that may not be exceeded at any time. VPD Maximum Demonstrated Parachute Deployment Speed is the maximum speed at which parachute deployment has been demonstrated. VS Stalling Speed is minimum steady flight speed at which the aircraft is controllable. VS 50% Stalling Speed is minimum steady flight speed at which the aircraft is controllable with 50% flaps. March 2010 Information Manual 1-9 Cirrus Design Section 1 SR20 General Meteorological Terminology VSO Stalling Speed is the minimum steady flight speed at which the aircraft is controllable in the landing configuration (100% flaps) at the most unfavorable weight and balance. VX Best Angle of Climb Speed is the speed at which the airplane will obtain the highest altitude in a given horizontal distance. The best angle-of-climb speed normally increases slightly with altitude. VY Best Rate of Climb Speed is the speed at which the airplane will obtain the maximum increase in altitude per unit of time. The best rate-of-climb speed decreases slightly with altitude. IMC Instrument Meteorological Conditions are meteorological conditions expressed in terms of visibility, distance from cloud, and ceiling less than the minima for visual flight defined in FAR 91.155. ISA International Standard Atmosphere (standard day) is an atmosphere where (1) the air is a dry perfect gas, (2) the temperature at sea level is 15 C, (3) the pressure at sea level is 29.92 in.Hg (1013.2 millibars), and (4) the temperature gradient from sea level to the altitude at which the temperature is -56.5 C is -0.00198 C per foot and zero above that altitude. MSL Mean Sea Level is the average height of the surface of the sea for all stages of tide. In this Handbook, altitude given as MSL is the altitude above the mean sea level. It is the altitude read from the altimeter when the altimeter’s barometric adjustment has been set to the altimeter setting obtained from ground meteorological sources. OAT Outside Air Temperature is the free air static temperature obtained from inflight temperature indications or from ground meteorological sources. It is expressed in either degrees Celsius or degrees Fahrenheit. March 2010 1-10 Information Manual Section 1 Cirrus Design General SR20 Engine Power Terminology Performance and Flight Planning Terminology • Pressure Altitude is the altitude read from the altimeter when the altimeter’s barometric adjustment has been set to 29.92 in.Hg (1013 mb) corrected for position and instrument error. In this Handbook, altimeter instrument errors are assumed to be zero. • Standard Temperature is the temperature that would be found at a given pressure altitude in the standard atmosphere. It is 15° C (59° F) at sea level pressure altitude and decreases approximately 2° C (3.6° F) for each 1000 feet of altitude increase. See ISA definition. HP Horsepower is the power developed by the engine. MCP Maximum Continuous Power is the maximum power that can be used continuously. MAP Manifold Pressure is the pressure measured in the engine’s induction system expressed as in. Hg. RPM Revolutions Per Minute is engine rotational speed. • Static RPM is RPM attained during a full-throttle engine runup when the airplane is on the ground and stationary. g One “g” is a quantity of acceleration equal to that of earth’s gravity. • Demonstrated Crosswind Velocity is the velocity of the crosswind component for which adequate control of the airplane during taxi, takeoff, and landing was actually demonstrated during certification testing. Demonstrated crosswind is not considered to be limiting. • Service Ceiling is the maximum altitude at which the aircraft at maximum weight has the capability of climbing at a rate of 100 feet per minute. GPH Gallons Per Hour is the amount of fuel (in gallons) consumed by the aircraft per hour. March 2010 Information Manual 1-11 Cirrus Design Section 1 SR20 General Weight and Balance Terminology NMPG Nautical Miles Per Gallon is the distance (in nautical miles) which can be expected per gallon of fuel consumed at a specific engine power setting and/or flight configuration. • Unusable Fuel is the quantity of fuel that cannot be safely used in flight. • Usable Fuel is the fuel available for flight planning. c.g. Center of Gravity is the point at which an airplane would balance if suspended. Its distance from the reference datum is found by dividing the total moment by the total weight of the airplane. • Arm is the horizontal distance from the reference datum to the center of gravity (c.g.) of an item. The airplane’s arm is obtained by adding the airplane’s individual moments and dividing the sum by the total weight. • Basic Empty Weight is the actual weight of the airplane including all operating equipment that has a fixed location in the airplane. The basic empty weight includes the weight of unusable fuel and full oil. MAC Mean Aerodynamic Chord is the chord drawn through the centroid of the wing plan area. LEMAC Leading Edge of Mean Aerodynamic Chord is the forward edge of MAC given in inches aft of the reference datum (fuselage station). • Maximum Gross Weight is the maximum permissible 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.
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
Section 3 Emergency Procedures Table of Contents Introduction .....................................................................................3-3 Airspeeds for Emergency Operations .............................................3-4 Emergency Procedures Guidance ..................................................3-5 Preflight Planning.........................................................................3-5 Preflight Inspections/Maintenance...............................................3-5 Methodology ................................................................................3-5 Memory Items ..............................................................................3-6 Ground Emergencies ......................................................................3-7 Engine Fire During Start ..............................................................3-7 Emergency Engine Shutdown On Ground...................................3-7 Emergency Ground Egress .........................................................3-8 In-Flight Emergencies .....................................................................3-9 Engine Failure On Takeoff (Low Altitude) ....................................3-9 Maximum Glide .............................................................................3-10 Engine Failure In Flight..............................................................3-11 Engine Airstart ...........................................................................3-12 Engine Partial Power Loss.........................................................3-13 Low Oil Pressure .......................................................................3-15 Propeller Governor Failure ........................................................3-15 Smoke and Fume Elimination....................................................3-16 Engine Fire In Flight...................................................................3-16 Wing Fire In Flight......................................................................3-16 Cabin Fire In Flight ....................................................................3-17 Emergency Descent ..................................................................3-18 Inadvertent Spiral Dive During IMC Flight .................................3-19 Spins..........................................................................................3-20 CAPS Deployment.....................................................................3-21 Landing Emergencies ...................................................................3-24 Emergency Landing Without Engine Power ..............................3-24 Ditching......................................................................................3-25 Landing Without Elevator Control ..............................................3-25 System Malfunctions.....................................................................3-26 Primary Flight Display System...................................................3-26 March 2010 3-2 Information Manual Section 3 Cirrus Design Emergency Procedures SR20 PFD - Loss of Air Data ...............................................................3-26 PFD - Loss of Attitude Data .......................................................3-26 Power Lever Linkage Failure .....................................................3-27
Section 4 Normal Procedures Table of Contents Introduction .....................................................................................4-3 Airspeeds for Normal Operation .....................................................4-4 Normal Procedures .........................................................................4-5 Preflight Inspection ......................................................................4-5 Preflight Walk-Around..................................................................4-6 Before Starting Engine...............................................................4-10 Starting Engine ..........................................................................4-11 Before Taxiing............................................................................4-13 Taxiing .......................................................................................4-13 Before Takeoff ...........................................................................4-14 Takeoff.......................................................................................4-16 Normal Takeoff ..........................................................................4-17 Short Field Takeoff ....................................................................4-17 Climb..........................................................................................4-18 Cruise ........................................................................................4-19 Cruise Leaning...........................................................................4-20 Descent......................................................................................4-21 Before Landing ..........................................................................4-21 Landing ......................................................................................4-21 Balked Landing/Go-Around .......................................................4-22 After Landing .............................................................................4-23 Shutdown...................................................................................4-23 Stalls ..........................................................................................4-24 Environmental Considerations ......................................................4-25 Cold Weather Operation ............................................................4-25 Hot Weather Operation..............................................................4-27 Noise Characteristics/Abatement..................................................4-28 Fuel Conservation.........................................................................4-29
Section 5 Performance Data Table of Contents Introduction .....................................................................................5-3 Associated Conditions Affecting Performance.............................5-3 Flight Planning ................................................................................5-4 Sample Problem .............................................................................5-4 Takeoff.........................................................................................5-5 Climb............................................................................................5-6 Cruise ..........................................................................................5-7 Fuel Required ..............................................................................5-8 Landing ........................................................................................5-9 Demonstrated Operating Temperature........................................5-9 Airspeed Calibration......................................................................5-10 Normal Static Source.................................................................5-10 Airspeed Calibration......................................................................5-11 Alternate Static Source ..............................................................5-11 Altitude Correction ........................................................................5-12 Normal Static Source.................................................................5-12 Altitude Correction ........................................................................5-13 Alternate Static Source ..............................................................5-13 Temperature Conversion ..............................................................5-14 Outside Air Temperature for ISA Condition ..................................5-15 Stall Speeds..................................................................................5-16 Wind Components ........................................................................5-17 Takeoff Distance ...........................................................................5-18 Takeoff Distance ...........................................................................5-19 Takeoff Distance ...........................................................................5-20 Takeoff Climb Gradient .................................................................5-21 Takeoff Rate of Climb ...................................................................5-22 Enroute Climb Gradient ................................................................5-23 Enroute Rate of Climb...................................................................5-24 Enroute Rate of Climb Vs Density Altitude ...................................5-25 Time, Fuel and Distance to Climb.................................................5-26 Cruise Performance ......................................................................5-27 Cruise Performance ......................................................................5-28 March 2010 5-2 Information Manual Section 5 Cirrus Design Performance Data SR20 Range / Endurance Profile ............................................................5-29 Range / Endurance Profile ............................................................5-30 Balked Landing Climb Gradient ....................................................5-31 Balked Landing Rate of Climb.......................................................5-32 Landing Distance ..........................................................................5-33 Landing Distance ..........................................................................5-34
Section 6 Weight and Balance Table of Contents Introduction .....................................................................................6-3 Airplane Weighing Form .................................................................6-6 Airplane Weighing Procedures .......................................................6-7 Weight & Balance Record .............................................................6-10 Loading Instructions......................................................................6-12 Center of Gravity Limits ................................................................6-14 Weight & Balance Loading Form ..................................................6-15 Loading Data.................................................................................6-16 Moment Limits...............................................................................6-17 Equipment List ..............................................................................6-18
Section 7 Airplane and Systems Description Table of Contents Introduction .....................................................................................7-5 Airframe ..........................................................................................7-6 Fuselage ......................................................................................7-6 Wings...........................................................................................7-6 Empennage .................................................................................7-7 Flight Controls .................................................................................7-8 Elevator System...........................................................................7-8 Aileron System...........................................................................7-10 Rudder System..........................................................................7-12 Trim Systems ................................................................................7-14 Pitch Trim Control System.........................................................7-14 Roll Trim Control System...........................................................7-14 Yaw Trim System.......................................................................7-15 Flight Deck Arrangement ..............................................................7-16 Instrument Panel........................................................................7-16 Center Console..........................................................................7-17 Flight Instruments .........................................................................7-21 Primary Flight Display................................................................7-21 Attitude Indicator........................................................................7-26 Airspeed Indicator......................................................................7-27 Vertical Speed Indicator.............................................................7-27 Altimeter.....................................................................................7-28 Turn Coordinator........................................................................7-28 Directional Gyro .........................................................................7-29 Course Deviation Indicator ........................................................7-30 Horizontal Situation Indicator.....................................................7-31 Magnetic Compass ....................................................................7-33 Wing Flaps ....................................................................................7-34 Flap Control Switch....................................................................7-34 Landing Gear ................................................................................7-36 Main Gear ..................................................................................7-36 Nose Gear .................................................................................7-36 Airplane Cabin ..............................................................................7-36 March 2010 7-2 Information Manual Section 7 Cirrus Design Airplane Description SR20 Cabin Doors ...............................................................................7-36 Baggage Compartment..............................................................7-38 Seats..........................................................................................7-38 Windshield and Windows...........................................................7-39 Cabin Safety Equipment ............................................................7-40 Engine ...........................................................................................7-43 Engine Oil System .....................................................................7-43 Engine Cooling...........................................................................7-43 Engine Fuel Injection .................................................................7-44 Engine Air Induction System......................................................7-44 Engine Fuel Ignition ...................................................................7-44 Engine Exhaust..........................................................................7-45 Engine Controls .........................................................................7-45 Alternate Air Control...................................................................7-46 Engine Indicating .......................................................................7-46 Propeller ........................................................................................7-55 Fuel System ..................................................................................7-56 Fuel Selector Valve....................................................................7-58 Fuel Quantity Indicator...............................................................7-59 Fuel Flow Indication ...................................................................7-62 Fuel Caution Light......................................................................7-62 Boost Pump Switch....................................................................7-63 Brake System.............................................................................7-64 Electrical System...........................................................................7-67 Power Generation ......................................................................7-67 Power Distribution......................................................................7-68 BAT & ALT Master Switches......................................................7-70 Avionics Power Switch...............................................................7-71 Volts and Ampere Meter/Indication............................................7-71 Ammeter Select Switch..............................................................7-73 Low-Volts Warning Light ............................................................7-73 ALT Fail Caution Lights..............................................................7-73 Circuit Breakers and Fuses........................................................7-74 Ground Service Receptacle .......................................................7-75 Convenience Outlet ...................................................................7-75 Exterior Lighting ............................................................................7-76 Navigation Lights .......................................................................7-76 Strobe Light................................................................................7-76 Landing Light .............................................................................7-76 March 2010 Interior Lighting .............................................................................7-76 Instrument Lights .......................................................................7-77 Panel Flood Lights .....................................................................7-77 Reading Lights...........................................................................7-77 Overhead Dome Light................................................................7-77 Environmental System..................................................................7-78 Description and Operation .........................................................7-82 Pitot-Static System........................................................................7-84 Pitot Heat Switch .......................................................................7-84 Pitot Heat Light ..........................................................................7-84 Alternate Static Source ..............................................................7-86 Stall Warning System....................................................................7-86 Standard Avionics .........................................................................7-87 Multi-Function Display ...............................................................7-89 Autopilot.....................................................................................7-90 GPS Navigation .........................................................................7-93 Communication (COM) Transceivers ........................................7-95 Navigation (Nav) Receiver.........................................................7-96 Transponder ..............................................................................7-98 Audio System.............................................................................7-98 Emergency Locator Transmitter ................................................7-99 Hour Meter(s)...........................................................................7-100 Digital Clock.............................................................................7-101 Cirrus Airplane Parachute System..............................................7-103 System Description..................................................................7-103 Activation Handle .....................................................................7-104 Deployment Characteristics .....................................................7-105
Section 8 Handling, Servicing, Maintenance Table of Contents Introduction .....................................................................................8-3 Operator’s Publications...................................................................8-3 Service Publications ....................................................................8-3 Ordering Publications ..................................................................8-4 Airplane Records and Certificates ..................................................8-5 Airworthiness Directives..................................................................8-6 Airplane Inspection Periods ............................................................8-6 Annual Inspection ........................................................................8-6 100-Hour Inspection ....................................................................8-7 Cirrus Design Progressive Inspection Program...........................8-7 Pilot Performed Preventative Maintenance .................................8-8 Ground Handling ...........................................................................8-10 Application of External Power ....................................................8-10 Towing .......................................................................................8-11 Taxiing .......................................................................................8-12 Parking.......................................................................................8-13 Tiedown .....................................................................................8-14 Leveling .....................................................................................8-14 Jacking.......................................................................................8-15 Servicing .......................................................................................8-16 Landing Gear Servicing .............................................................8-16 Brake Servicing..........................................................................8-16 Tire Inflation ...............................................................................8-18 Propeller Servicing.....................................................................8-18 Oil Servicing...............................................................................8-19 Fuel System Servicing ...............................................................8-22 Fuel Contamination and Sampling.............................................8-24 Draining Fuel System ................................................................8-25 Battery Service..............................................................................8-25 Cleaning and Care ........................................................................8-26 Cleaning Exterior Surfaces ........................................................8-26 Cleaning Interior Surfaces .........................................................8-30
Section 9 Log of Supplements Part Number Title Date ___ 11934-S01 R2 Garmin GMA 340 Audio System 07-18-05 ___ 11934-S05 Garmin GNC 250XL GPS Navigator w/ VHF COM 03-31-99 ___ 11934-S06 R1 S-Tec System Twenty Autopilot 12-07-04 ___ 11934-S09 R1 Approved Oxygen Systems 01-07-03 ___ 11934-S11 R1 L-3 Avionics Systems WX500 Stormscope Sensor 07-18-05 ___ 11934-S12 Garmin GTX 327 Transponder 12-26-00 ___ 11934-S15 R1 L-3 Avionics Systems SkyWatch Traffic Advisory System10-12-05 ___ 11934-S17 SR20 Airplanes Registered in Canada 10-10-01 ___ 11934-S19 R1 S-Tec System Thirty Autopilot with GPSS 12-07-04 ___ 11934-S20 R4 S-Tec System 55X Autopilot w/ Altitude Selector/Alerter 08-15-07 ___ 11934-S22 R2 Garmin GNS 430 GPS Navigator 08-15-07 ___ 11934-S23 R2 Garmin GNC 420 GPS Navigator 08-15-07 ___ 11934-S24 Sandel Avionics SN3308 Navigation Display 01-07-03 ___ 11934-S25 R1 Winterization Kit 12-07-04 ___ 11934-S27 R2 S-Tec System 55SR Autopilot 07-18-05 ___ 11934-S28 Garmin GTX 330 Mode S Transponder 07-03-04 ___ 11934-S29 SR20 Airplanes Registered in the European Union 05-27-04 ___ 11934-S30 R1 Honeywell KGP 560 Terrain/Awareness Warning System12-15-07 ___ 11934-S31 R1 Avidyne EMax™ Engine Instrumentation 12-15-07 ___ 11934-S32 R1 Avidyne CMax™ Electronic Approach Charts 12-15-07 ___ 11934-S33 R1 XM Satellite Weather System 12-15-07 ___ 11934-S34 R2 Avidyne Flight Director 12-15-07 ___ 11934-S36 R1 Artex ME406 406 MHz ELT System 12-18-08 ___ 11934-S37 R1 SR20 Airplanes Equipped with the “G3 Wing” 08-26-09 ___ 11934-S38 R1 Garmin 400W-Series GPS Navigator 11-11-07 ___ 11934-S44 Part 135 Operations: Electrical Loading Shedding 06-13-09 ___ 11934-S45 SR20 Airplanes Registered in Argentina 08-26-09

f214216709 发表于 2010-10-26 08:07:03

看看的哦谢谢

ditigo 发表于 2011-6-19 10:20:42

了解一下谢谢

wwwronin 发表于 2011-11-13 15:54:49

非常感谢，很需要呢

comicdna 发表于 2015-9-25 14:38:35

非常有用的资料！！！

buaawu 发表于 2016-3-10 19:08:59

谢啦感谢

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西锐20飞机信息手册AIRPLANE INFORMATION MANUAL for the CIRRUS DESIGN SR20 1268－