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MAINTENANCE PRACTICES 201
1. SERVICING - MANIFOLD PRESSURE FILTER 201
2. REMOVAL / INSTALLATION - MANIFOLD PRESSURE
FILTER 201
A. Tools and consumable materials 201
B. Removal of the manifold pressure filter 201
C. Installation of the manifold pressure filter 201
3. ADJUSTMENT / TEST - MANIFOLD PRESSURE FILTER 201
4. INSPECTION / CHECK - MANIFOLD PRESSURE FILTER 201
A. Tools and consumable materials 201
B. Inspection of the filter 201 1 - 9999
I TEMPERATURE 77-20-00 (DA) 1 OPT or STD
DESCRIPTION AND OPERATION 1 Post-MOD. 151
1. GENERAL 1
2. LOCATION 1
3. DESCRIPTION 1
A. Temperature dual indicator 1
B. Cylinder head temperature probe 1
C. Exhaust temperature probe 1
I TEMPERATURE 77-20-00 (BA) 201 OPT or STD
MAINTENANCE PRACTICES 201 Post-MOD. 151
1. SERVICING - TEMPERATURE 201
ADAA
Validity : S / N 1 - 9999 77 TC (EA) Page 2 JUN 01
ENGINE INDICATING
DESCRIPTION AND OPERATION
1. GENERAL
This chapter deals with the engine parameters required for correct flight progress. It includes two sections :
— the "power section, which informs the user about engine operation — refer to 77-10-00,
— the "temperature" section, which informs the user about engine temperature — refer to 77-20-00.
I AAAA
Validity : S / N 1 — 9999 77-00-00 (BA) Page 1
JUL 99
PAGE INTENTIONALLY LEFT BLANK
I AAAA
Validity : S / N 1 — 9999 77-00-00Page 2
(BA) JUL 99
POWER
DESCRIPTION AND OPERATION
1. GENERAL
I This section deals with the engine indicators which give indications, either directly or indirectly, on engine
operation.
The main elements are :
— tachometer indicator,
— manifold pressure indicator,
— tachometer control,
— manifold pressure filter.
2. LOCATION (Figure 1)
COMPONENT QTY AREA ACCESS DOOR REFERENCE
Tachometer indicator 1 200 / 77-10-00
Manifold pressure indicator 1 200 / 77-10-00
Tachometer control 1 100 121 77-10-00
Manifold pressure filter 1 100 121 77-10-02
I 3. DESCRIPTION
A. Tachometer indicator
Located on the instrument panel, this element receives information from the tachometer sensor and transmits information relative to the engine rotation speed to the pilot.
It is supplied by bus 1 bar.
B. Manifold pressure indicator
The dual indicator is located on the instrument panel. It is linked by a pipe to the pressure inlet which is connected to the R.H. rear cylinder and transmits all the changes of pressure to the pilot.
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