SECTION 1
GENERAL
SOCATA
MODEL TB 20
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socata
. It is supplied in
confidence and commercial security of its contents must be maintained.
It must not be used for any purpose other than that for which it is supplied, nor
may information contained in it be disclosed to unauthorized persons. It must not
be reproduced nor transmitted in any form in whole or in part without permission
in writing from the owners of the Copyright.
Information in this document is subject to change without notice.
© 1988, 1991, 1992, 1994 to 1996, 1997, 2000 -
socata
- All rights reserved
June 30, 1988
Revision 8
1.3
GENERAL
This handbook contains 9 sections, and includes the material required by
FAR Part 23 to be furnished to the pilot for operation of SOCATA Model TB 20
airplane. It also contains supplemental data supplied by SOCATA.
This section provides basic data and information of general interest. It also
contains definitions or explanations of abbreviations and terminology
commonly used.
The general for optional systems are given in Section ”Supplements” of this
Manual.
DESCRIPTIVE DATA
ENGINE
Number of engines : 1
Engine Manufacturer : AVCO LYCOMING
Engine Model Number : IO–540–C4 D5D or IO–540–C4 B5D
Engine Type :
Six–cylinder, horizontally opposed, direct drive, air–cooled
Engine rated at 250 BHP at 2575 RPM.
PROPELLER
Number of propellers : 1
Propeller Manufacturer : HARTZELL
Propeller Model Number : HC–C2YK–1BF/F8477–4
Number of blades : 2
Propeller Diameter :
Maximum : 80 inches (2.03 m)
Minimum : 78 inches (1.98 m)
Propeller Type :
Constant–speed, hydraulically–actuated
Propeller Governor : WOODWARD M 210 681 or C210 761 or F210 761
