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 7
2.11
PLACARDS
NOTE :
The placards described in the Section 9 ”Supplements” replace or
supplement those described in this paragraph.
(1) In full view of the pilot, forward of overhead lights
THIS AIRPLANE MUST BE OPERATED AS A NORMAL CATEGORY AIRPLANE IN
COMPLIANCE WITH THE OPERATING LIMITATIONS STATED IN FORM OF
PLACARDS, MARKINGS AND FLIGHT MANUAL.
INVERTED FLIGHT
. . . . . . . . . . . . . . . . . . . . . . . .
PROHIBITED
AEROBATIC MANEUVERS
. . . . . . . . . . . . . . . . . . . .
PROHIBITED
INTENTIONAL SPINS
. . . . . . . . . . . . . . . . . . . . . . .
PROHIBITED
ICING CONDITIONS
. . . . . . . . . . . . . . . . . . . . . . .
PROHIBITED
MAXIMUM TAKE–OFF AND LANDING WEIGHT
. . . . . . . .
3086 lbs
DESIGN MANEUVERING SPEED V
A
. . . . . . . . . . . . . .
129 KIAS
LIMIT SPEED V
NE
. . . . . . . . . . . . . . . . . . . . . . . .
187 KIAS
FLAPS EXTENDED MAXIMUM SPEED V
FE
. . . . . . . . . . .
FLAPS ”TAKE–OFF”
. . . . . . . . . . . . . . . . . . . .
129 KIAS
FLAPS ”LANDING”
. . . . . . . . . . . . . . . . . . . . .
103 KIAS
LANDING GEAR EXTENDED MAXIMUM SPEED V
LE
. . . . .
139 KIAS
LANDING GEAR OPERATING MAXIMUM SPEED V
LO
. . . . .
129 KIAS
POSITIVE FLIGHT LOAD FACTOR (MAXIMUM)
FLAPS UP
. . . . . . . . . . . . . . . . . . . . . . . . . . . .
+ 3.8
FLAPS DOWN
. . . . . . . . . . . . . . . . . . . . . . . . . .
+ 2
FLIGHT CONDITIONS : DAY VFR
ICING CONDITIONS NOT ALLOWED
