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A. Tools and consumable materials 402
B. Procedure 402
ADAA
Validity : S / N 1 - 9999 33 TC (EA) SEP 04
Page 2
SOCATA
TB 20 MODEL MAINTENANCE MANUAL
SUBJECT CHAPTER PAGE VALIDITY
ANTICOLLISION AND NAVIGATION LIGHTS 33-40-02 (BA) 501 Post-MOD. 151
ADJUSTMENT / TEST 501
1. OPERATIONAL TEST OF ANTICOLLISION AND
NAVIGATION LIGHTS 501
A. Tools and consumable materials 501
B. Procedure 501
EMERGENCY LIGHTING 33-50-00 (BA) 1 823 - 849, 888,
DESCRIPTION AND OPERATION 1 948 - 9999
1. GENERAL 1
2. LOCATION 1
3. DESCRIPTION 1
A. Emergency battery 1
B. Lighting spots 1
C. Control panel 1
4. OPERATION 2
A. Automatic operation 2
B. Manual operation 2
C. Test sequence 2
EMERGENCY LIGHTING 33-50-00 (BA) 401 823 - 849, 888,
REMOVAL / INSTALLATION 401 948 - 9999
1. REMOVAL OF THE EMERGENCY BATTERY 401
A. Tools and consumable materials 401
B. Procedure 401
2. INSTALLATION OF THE EMERGENCY BATTERY 401
A. Tools and consumable materials 401
B. Procedure 401
ADAA
Validity : S / N 1 - 9999 33 TC (E„ Page 3 SEP 04
PAGE INTENTIONALLY LEFT BLANK
ADAA
Validity : S / N 1 - 9999 33 TC (EA) Page 4 JUN 01
LIGHTS
DESCRIPTION AND OPERATION
1. GENERAL
The lighting system comprises the equipment and components ensuring aircraft lighting and external and internal indication.
This chapter is composed of the following sections :
- cockpit - refer to 33-10-00.
- external lighting - refer to 33-40-00.
28-volt aircraft
- emergency lighting (Option) - refer to 33-50-00.
ABM
Validity : S / N 1 - 9999 33-00 Page 1
00 (CA) JUN 01
PAGE INTENTIONALLY LEFT BLANK
ABAA
Validity : S / N 1 - 9999 33 00 00Page 2
(CA) JUN 01
COCKPIT
DESCRIPTION AND OPERATION
1. GENERAL
The cockpit lighting is located above the floor between the instrument panel and the rear cabin bulkhead and serves as lighting and indication.
2. DESCRIPTION (Figures 1, 2, 3 and 4)
Instrument panel and control panels lighting is provided by integral, flood, post lights and electroluminescent lighting. Three lighting control knobs are grouped together on the L.H. part of the L.H. instrument panel.
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