SECTION 2
LIMITATIONS
SOCATA
MODEL TB 20
The content of this document is the property of
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 2
2.3
GENERAL
The SOCATA Model TB 20 airplane is certified in Normal Category in
accordance with following basis.
–
Basic general technical conditions :
FAR 23 Regulations, amendments 1 to 16.
–
Complementary general technical conditions :
Paragraph 23–1581, amendment 21.
–
Special technical condition :
The landing gear being held in high position by hydraulic pressure alone,
the requirements of paragraphs 23–143 and 23–729 are modified as
follows :
(a) 1,6 V
S1
speed is replaced by V
NO
in 23–729 (a).
(b) Condition 23–143, as for landing gear extension must be checked up
to V
NO
.
This airplane must be flown in compliance with the limits specified by
placards or markings and with those given in this section and throughout this
Manual.
This section of the airplane Flight Manual presents the various operating
limitations, the significance of such limitations, instrument markings, color
coding, and basic placards necessary for the safe operation of the airplane,
its power plant and installed equipment.
The limitations for optional systems are given in Section ”Supplements” of
this Manual.
