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attach to the trailing edge of the wing.
The horizontal stabilizer is a semi-monocoque structure. It has top and bottom shells made of GFRP.
The shells bond to GFRP spars and ribs. The trailing edge has a conventional elevator and a trim tab.
The one-piece canopy has a large quantity of wrap-around glazing. This gives a good all-round view
from the cockpit. A glazed rear passenger door gives access to the rear seats from the left side of the
airplane.
A polyurethane paint finish protects the outside skin from ultraviolet rays and humidity.
The fixed tricycle landing gear has fairings attached to each leg. The main legs attach to the fuselage
center-section. The nose leg attaches to the forward fuselage. Each main wheel has a disc brake on
the inside. Hydraulic pressure operates each disc brake.
The flight control system uses conventional ailerons, elevator and rudder. The DA 40 has 2 control
sticks and 2 rudder pedal assemblies to operate the primary flight-controls. Push-pull rods operate the
ailerons and elevator. Cables operate the rudder. An electric motor operates the wing flaps. A hand
wheel and Bowden cable operate the elevator trim.
The DA 40 is powered by one of the following engines:
) Lycoming IO360 - a four cylinder, direct drive, horizontally-opposed engine. The engine has a fuel
injection system and a conventional wet-sump oil system.
) Thielert Aircraft Engines TAE 125 - a four valve, four cylinder Diesel cycle engine with cylinders in
line. The engine has a turbo-charger and intercooler, a common rail high-pressure direct injection
system, and a wet oil system. It drives the propeller through a reduction gear.
The DA 40 has a hydraulic constant-speed propeller with 3 blades.
AIRCRAFT
DA 40 Series
AMM
General Description
Doc # 6.02.01
Rev. 5 03-00-00 Page 3
20 Sep 2007
The airplane has an aluminum fuel tank in each wing. Each tank consists of several chambers. The
fuel tanks are inboard between the spars. The tank assemblies have fuel fillers at or near the outboard
end. Flexible hoses connect the tanks to a fuel selector and shut-off valve under the cockpit floor. An
electrical boost pump (Lycoming version only) and an engine driven pump supply fuel to the engine.
The tanks have fuel quantity probes which operate the cockpit indicating systems.
The airplane has two sources of electrical power. A 28 Volt (Lycoming version) or 14 Volt (TAE
version) battery supplies power when the engine is not running. An alternator provides power when
the engine is running. Switches and circuit breakers control all electrical devices. A starter key controls
the engine starter motor. It also controls the magnetos (Lycoming version) or serves as electric master
switch (TAE version).
The DA 40 has a full range of flight instruments. These include Pitot/static instruments to show
airspeed and altitude, as well as electrically driven instruments and vacuum driven instruments (TAE
version only) to show attitude. The airplane has all the usual engine instruments, except that the TAE
version has a load indication instead of a manifold pressure indication.
The airplane also has radio and navigation aids installed.
AIRCRAFT
General Description
DA 40 Series
AMM
Page 4
20 Sep 2007 03-00-00 Doc # 6.02.01
Rev. 5
3. Equipment Data
The table below gives you the name and address of the manufacturers who supply systems and/or
equipment for the DA 40. This will help you get more data on a system and/or equipment.
Equipment/System Address
Lycoming IO-360-M1A Engine: Textron Lycoming
652 Oliver Street
Williamsport, PA 17701
USA
Homepage: www.lycoming.textron.com
TAE 125 Engine: Thielert Aircraft Engines
Platanenstr. 14
D-09350 Lichtenstein
Germany
Tel.: +49-37204/696-90
Fax: +49-37204/696-50
Homepage: www.tae-engines.com
E-mail: info@tae-engines.com
Propeller: MT-Propeller Entwicklung GmbH
Flugplatzstr. 1
D-94348 Atting
Germany
Tel.: +49-9429-94090
Fax: +49-9429-8432
Homepage: www.mt-propeller.de
MT-Propeller USA, Inc.
1180 Airport Terminal Drive
DeLand, FL 32724
Tel.: (386) 736-7762
Fax: (386) 736-7696
E-mail: mtprop@bellsouth.net
Main Wheels and Brakes: Cleveland: Parker Hannifin Corporation
Aircraft Wheel and Brake Division
P.O. Box 158
Avon, Ohio 44011
USA
Tel: (216) 934-5221
AIRCRAFT
DA 40 Series
AMM
General Description
Equipment/System Address
Doc # 6.02.01
Rev. 5 03-00-00 Page 5
20 Sep 2007
Navigation and Communication Equipment: Bendix/King
400 North Rogers Road
Olathe, Kansas 66062-1212
　
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