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(1)  Taxi the airplane for 1500 ft with 1700 RPM.  Use the brakes to keep the speed at 5 to 10 mph (8 to 16 km/h). 
(2)  Let the brakes cool for 10 to 15 minutes. 
(3)  Apply the brakes. Do a high throttle run-up.  The brakes must hold with the usual pedal force. 
(4)  If the brakes do not hold the static run-up, do steps 1 to 3 again as necessary. 

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CHAPTER 33
 LIGHTS

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TABLE OF CONTENTS
CHAPTER 33
LIGHTS

1.
General ..............................................1

2.
Description............................................1

 

Section 33-10
Lights - Flight Compartment

1.
General ..............................................1

2.
Description............................................1

 

Trouble-Shooting
1. General ............................................101

Maintenance Practices
1.
General ............................................201

2.
Remove/Install a Cabin Light Assembly....................201

3.
Replace a Filament in a Reading Light Assembly.............202

4.
Remove/Install a Dimmer Switch.........................202

 

% Doc # 6.02.01 Page 1 % Rev. 4 09 Jan 2003
33-CONTENTS
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Section 33-40
Exterior Lights
1.
General ..............................................1

2.
Description............................................1

 

Trouble-Shooting
1. General ............................................101

Maintenance Practices
1.
General ............................................201

2.
Remove/Install the Taxi Light............................201

3.
Remove/Install the Landing Light.........................202

4.
Replace a Filament in the Wing-Tip Light Unit...............204

5.
Remove/Install the Light Unit in the Wing-Tip ...............205

6.
Remove/Install a Strobe Power Unit in the Wing-Tip ..........207

 

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33-CONTENTS
Lights
AMM

CHAPTER 33
LIGHTS

1. General
This Chapter tells you about the cockpit and the exterior lighting of the DA 40. Section 33-10 tells you about the flight compartment lighting and Section 33-40 tells you about the exterior lighting.
Note:  Equipment which is certified for installation in the DA 40 is listed in Section 6.5 of the Airplane Flight Manual. Such equipment may be installed in accordance with the Airplane Maintenance Manual.
Any equipment which is not listed in Section 6.5 of the Airplane Flight Manual is called "Additional Equipment". The installation of Additional Equipment is a modification which must be handled in accordance with national regulations or a Service Bulletin.
2. Description
Figure 1 shows you the location of the lights. The DA 40 has these flight compartment lights:
) Reading lights.
) Instrument lights.
) Instrument panel flood light.
Some avionics equipment has internal lighting. Refer to the related Section and the equipment manufacturers handbooks for the equipment in your airplane. Combined ON/OFF and dimmer switches for the instrument panel flood lights and the internal instrument lights are located in the instrument panel, top left.
The DA 40 has these exterior lights in one light unit at each wing-tip:
　
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