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1. GENERAL
The control and indicating panels contain essentially :
- instrument panel,
- central console,
- engine monitoring cluster.
2. LOCATION
COMPONENT QTY AREA ACCESS DOOR REFERENCE
Instrument panel 1 250 251L, 251R 31-10-01
Central console 1 250 251C 31-10-02
Engine monitoring cluster 1 250 251C 31-10-03
3. DESCRIPTION
A. Instrument panel (Figures 1 and 2)
1) L.H. instrument panel
The L.H. instrument panel is designed around the basic "T" configuration.
The gyros (if installed) are located in front of the pilot and arranged vertically.
The airspeed indicator or the true airspeed indicator and the altimeter are to the left and right of the
gyros, respectively. The rest of the flight instruments is located around the basic "T".
The upper edge of the instrument panel contains the advisory panel.
The left side of the panel contains lighting controls, emergency beacon switch (if installed) and
registration (for aircraft radio identification).
2) L.H. panel strip
The L.H. panel strip contains from left to right :
- L.H. vent,
- magneto / start selector,
- parking brake knob,
- landing gear configuration and control panel,
- propeller deicing box (if installed),
Option Pre-MOD. 151, Standard Post-MOD. 151
- alternate static source valve,
- vacuum system pressure gage.
AFAA
Validity : S / N 1 - 9999 31 10-00Page 1
(GA) SEP 02
Under the panel strip :
- emergency gear control (L.H. side),
- "Alternate Air" control (R.H. side).
3) R.H. instrument panel
The R.H. instrument panel contains : manifold pressure /flowmeter indicator and the tachometer. It also contains locations for additional equipment such as :
- 2nd altimeter,
- VOR / LOC indicator,
- outside air temperature,
- cylinder head temperature,
- exhaust gas temperature, etc...
4) R.H. panel strip
The R.H. panel strip contains :
- a location for radio equipment or any other one,
- air conditioning control,
- R.N. vent.
B. Central console (Figure 2)
The central console contains in the upper edge, the engine monitoring cluster then radio-navigation equipment vertically mounted to console lower edge.
• C. Engine monitoring cluster (Figures 2, 2A, 3, 3A, 3B, 3C and 3D)
NOTE : No repairs are allowed inside the engine monitoring cluster. In case of failure, carry out a standard replacement.
Pre-MOD. 182
The box, located in upper part of the central console, contains the following indicators, from left to right :
- oil temperature,
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本文链接地址：TB20 MAINTENANCE MANUAL 31 指示/记录系统 TB20飞机维护手册(4)
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