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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
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IP卡
狗仔卡
发表于 2010-10-23 11:31:34
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提升卡
置顶卡
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变色卡
显身卡
发表于 2010-10-26 08:07:03