Diamond DA20-C1

Diamond DA20-C1 - Advanced Aircraft Data

AirFrame
Fusulage Construction Semimonocoque
Airframe Material Carbon Fiber Composite
Number of Doors 1


Wing
Wing Location Bottom Wing
Wing Construction CFRP Spar
Wing Rib Material Semi-monocoque Sandwhich
Wing Skin Material Composite
--Aileron
Aileron Type Conventional
Aileron Trim None
Aileron Control System Push Rod
--Flap
Flap Type Plain
Wing Flap Actuation Electric


Empennage
Empennage Type T Tail
Empennage Rib Material Semi-Monocoque sandwich
Empennage Skin Material Composite
Rudder Trim Ground Adjustable Trim Tab
Yaw Trim Actuator None
Yaw Control System Cable and Pully
Pitch Trim Servo Tab
Pitch Control System Push Rod
Pitch Trim Actuator Electric


Landing Gear
Landing Gear Type Tricycle
Retractable No
Retraction System None
Emergency Extension None
Ground Steering Rudder Pedals
Shock Absorbtion Main Gear Aluminum Spring
Shock Absorbtion Other Gear Mechanical Spring
Brake Type Hydraulic Actuated Brake Disc
Brake Controls Toe Brakes


Cabin
Instrument Panel IFR non Glass
Flight Control Joystick
Number of Seats 2
Heating Engine Exhaust Shroud
Window Defrost Ducted Hot Air
Cooling Ducted Ram Air


Profiles
Normal Climb Profile Speed (KIAS) 75
Maximum Climb Profile Speed (KIAS) 75
Engine
Number of Engines 1
Engine Manufacturer Continental
Engine Model IO-240-B
Engine Type Normally Aspirated Piston
Geared Direct Drive
Cooled Air Cooled
Fuel/Air Mechanism Fuel Injected
Number of Cylinders 4
Max HP 125
Starter System Electric Starter


Propeller
Propeller Manufacturer Sensenich
Propeller Model W69EK7-63
Number of Blades 2
Minimum Diameter 5 ft 9 inch
Maximum Diameter 5 ft 9 inch
Propeller Type Fixed Pitch
Propeller Governor None


Fuel System
Fuel System Type Fuel Pump
Approved Fuel Type 1 100LL
Approved Fuel Type 2 100
Approved Fuel Type 3
Fuel Capacity (G) 24.5
Tank Type 1 Location Behind Passenger Compartment
Tank Type 1 Capacity (G) 24.5
Tank Type 2 Location
Tank Type 2 Capacity (G) 0
Usable Fuel (G) 24
Oil Capacity (Quarts) 6


Electrical System
Power Source Engine Driven Generator
Power Storage Battery
System Voltage 14
Alternator Amp 40
Battery Voltage 12
Battery Amp/Hour 20


Limitations
Maximum T/O Weight (lbs) 1653
Maximum LDG Weight (lbs) 1653
Standard Empty Weight (lbs) 1153
Useful Load (lbs) 500
Station 1 Baggage Location Aft Portion of Flight Deck
Max Weight Station 1 (lbs) 44
Station 2 Baggage Location
Max Weight Station 2(lbs) 0
Station 3 Baggage Location
Max Weight Station 3(lbs) 0
Wing Loading (lbs/sq.ft) 13.21
Vne (KCAS) 164
Vno (KCAS) 118
Va(Max Gross) (KCAS) 106