DA 40 F
Paragraph B is amended to read:
B. Engine Control Assembly
The engine control assembly in the center console has these controls: ) Throttle. %) Propeller (not for the DA 40 F variant). %) Carburetor Heat (DA 40 F variant only). ) Mixture. ) Parking brake. ) Cabin Heat control lever. ) Distribution control lever for Cabin Air. % The 3 power-plant control levers are on one pivot shaft at the rear of the assembly. A knob on the right side of the assembly adjusts throttle (mixture and propeller) friction. The parking brake and
cabin heat control levers are also on one shaft at the top front of the assembly. Friction discs,
stators and spring washers hold both groups of levers in position on the shafts.
The assembly has 2 aluminum-alloy side-plates. Four sheet-metal brackets hold the outer sheaths
of the control cables. A metal bracket at the front top attaches to the bottom of the instrument panel. A metal bracket at the back attaches to the elevator trim mounting. Rivets attach all of the metal brackets to the side plates.
Bolts hold 5 tubular spacers between the side plates. The spacers make fixed stops for the control
levers. Two of the spacers also hold one end of the friction stators for each group of levers. Two bolts attach the engine control assembly to the bottom of the instrument panel. Bolts attach the assembly to the side walls of the floor panel.
Doc # 6.02.01 Page 15a
31-10-00
DA 40 Series AMM
DA 40 F AIRCRAFT
Add the following figure for the DA 40 F variant:
Figure 25a: Engine Control Assembly in the Center Console for the DA 40 F variant
AIRCRAFT DA 40 F
Add the following paragraph:
C. Carbon Monoxide Detector (DA 40 F variant only):
The DA 40 F variant with fixed pitch propeller and the Lycoming O-360-A4M engine has an additional Carbon Monoxide (CO) detector installed.
The CO Detector consists of the CO-sensor, a test/ reset button and an amber alert annunciator light next to the test button. The CO-Detector is connected to the aircraft's electrical system via a circuit breaker. In case of a carbon monoxide alert, the pilot will receive an amber alert annunciator light. This visual alert will remain until the carbon monoxide level has dropped below the alert level. The indicator is automatically reset when the CO level drops below 50 ppm.
When power is applied to the CO Detector, a self test routine begins. The amber alert annunciator light flashes twice and remains OFF until a CO alert or a failure of the unit occurs.
When starting up the CO Detector, there is a delay of approximately three minutes until the indication is accurate.
Figure 1: Annunciator Panel with CO Detector installed (DA 40 F only)
Doc # 6.02.01 Page 5
31-20-00
DA 40 Series AMM
DA 40 F
Intentionally left blank
DA 40 F
Maintenance Practices
This section is amended to read:
1. General
% This Section tells you how to replace the digital chronometer and the CO Detector. Refer to the % equipment manufacturer's manuals for more data on this equipment. % 2. Remove/Install the Digital Chronometer or the CO Detector % A. Remove the Digital Chronometer or the CO Detector
Detail Steps/Work Items Key Items/References
(1) Open the OAT- circuit breaker. Open the CO DETECT - circuit breaker. Only for the Davtron M803. Only for the CO Detector.
(2) Remove the instrument panel cover. Refer to Section 25-10.
(3) Disconnect the electrical cable(s) from the instrument.
(4) Remove the screws which attach the instrument to the instrument panel. Hold the instrument.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：钻石40飞机维护手册 DA 40 SERIES AMM 6(36)
