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TB20 MAINTENANCE MANUAL 72 发动机 TB20飞机维护手册

时间:2011-11-12 05:03来源:蓝天飞行翻译 作者:航空
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ENGINE
 
 
LIST OF EFFECTIVE PAGES
CHAPTER PAGE DATE CHAPTER PAGE DATE
I 72-LEP (EA) 1 SEP 04   
 2 SEP 02   
72-TC (EA) 1 SEP 02   
 2 SEP 02   
I 72-00-00 (EA) 1 SEP 04   
 2 SEP 02   
I 72-00-00 (EM) 1 SEP 04   
 2 SEP 02   
72-00-00 (BA) 301 SEP 02   
 302 SEP 02   

ADM
Validity : S / N 1 - 9999 72-LEP (EA) Page 1 SEP 04
 
PAGE INTENTIONALLY LEFT BLANK
ADAA
Validity : S / N 1 - 9999 72-LEP (EA) Page 2 SEP 02
 
TABLE OF CONTENTS
SUBJECT CHAPTER PAGE VALIDITY
PISTON ENGINE 72-00-00 (EA) 1 1 - 9999
DESCRIPTION AND OPERATION  1 
1. GENERAL  1 
PISTON ENGINE 72-00-00 (EM) 1 With starting vibrator
DESCRIPTION AND OPERATION  1 
1. GENERAL  1 
PISTON ENGINE 72-00-00 (BA) 301 1 - 9999
SERVICING  301 
1. NEW ENGINE SERVICING  301 
A. Tools and consumable materials  301 
B. Break-in and operation  301 
 
PAGE INTENTIONALLY LEFT BLANK
ADAA
Validity : S / N 1 - 9999 72 TC (EA) Page 2 SEP 02
 
PISTON ENGINE
DESCRIPTION AND OPERATION
1. GENERAL
The TB 20 is powered by a six-cylinder, horizontally opposed direct drive LYCOMING IO-540-C4D5D injection engine rated at 250 BHP at 2575 RPM, except for aircraft fitted with noise reduction option as green range of tachometer indicator is limited to 2500 RPM. It is equipped with a starter, an alternator, a shielded ignition harness, a dual magneto, vacuum pump and propeller governor drives, a fuel pump, an injection pump, a flow divider and an induction air filter located on an air inlet equipped with an alternate air system should the filter become obstructed.
The engine is controlled from the cockpit by the following manual controls located on the central pedestal :
- throttle control - refer to 76-10-01,
- Alternate Air control - refer to 76-10-05,
- mixture control - refer to 76-10-03.
For engine servicing, refer to AVCO LYCOMING Maintenance Manual.
ABAA
Validity : S / N 1 - 9999 72 00-00Page 1
(EA) SEP 04
 
PAGE INTENTIONALLY LEFT BLANK
ABAA
Validity : S / N 1 - 9999 72 00-00Page 2
(EA) SEP 02
 
PISTON ENGINE
DESCRIPTION AND OPERATION
1. GENERAL
The TB 20 is powered by a six-cylinder, horizontally opposed direct drive LYCOMING 10-540-C4B5D injection engine rated at 250 BHP at 2575 RPM, except for aircraft fitted with noise reduction option as green range of tachometer indicator is limited to 2500 RPM. It is equipped with a starter, an alternator, a shielded ignition harness, a dual magneto, vacuum pump and propeller governor drives, a fuel pump, an injection pump, a flow divider and an induction air filter located on an air inlet equipped with an alternate air system should the filter become obstructed.
 
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