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B. Procedure 401
ENGINE MOUNT 71-20-00 (CA) 601 1 - 9999
INSPECTION / CHECK 601
1. CHECK OF ENGINE MOUNT 601
A. Tools and consumable materials 601
B. External check of engine mount 601
ENGINE MOUNT 71-20-00 (CA) 801 1 - 9999
REPAIR 801
1. REPAIRS AUTHORIZED ON ENGINE MOUNT 801
2. PERMISSIBLE DEFECTS 801
3. REPAIR 802
A. Tools and consumable materials 802
B. Repair procedure for a defect depth
less than 0.007 in (0.2 mm) 802
C. Repair procedure for a defect depth
within 0.007 in (0.2 mm) and 0.023 in (0.6 mm) 802
ADM
Validity : S / N 1 - 9999 71 -TC (EA) Page 2 JUN 02
SOCATA
TB 20 MODEL MAINTENANCE MANUAL
SUBJECT CHAPTER PAGE VALIDITY
AIR INLET 71-60-00 (EA) 1 1 - 9999
DESCRIPTION AND OPERATION 1
1. GENERAL 1
2. LOCATION 1
3. DESCRIPTION 1
A. Air intake box 1
B. Filter assy 1
C. Alternate Air 1
AIR INLET 71-60-00 (EA) 401 Without "Alternate
REMOVAL / INSTALLATION 401 Air" control
1. REMOVAL OF AIR INTAKE BOX 401
A. Tools and consumable materials 401
B. Procedure 401
2. INSTALLATION OF AIR INTAKE BOX 401
A. Tools and consumable materials 401
B. Procedure 401
AIR INLET 71-60-00 (FA) 401 With "Alternate
REMOVAL / INSTALLATION 401 Air" control
1. REMOVAL OF AIR INTAKE BOX 401
A. Tools and consumable materials 401
B. Procedure 401
2. INSTALLATION OF AIR INTAKE BOX 401
A. Tools and consumable materials 401
B. Procedure 401
PAGE INTENTIONALLY LEFT BLANK
ADAA
Validity : S / N 1 - 9999 71 -TC (EA) Page 4 JUN 02
POWER PLANT
DESCRIPTION AND OPERATION
1. GENERAL (Figure 1)
The powerplant of the TB 20 is installed in the aircraft front section, isolated from the airframe by a stainless
steel firewall.
The installation consists of :
- a LYCOMING injection engine, IO-540-C4D5D or IO-540-C4B5D (with starting vibrator) - refer
to 72-00-00,
- a propeller - refer to 61-00-00,
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