Flight and Operational Manual
TL- 96 STAR s/n 99 S 25
Notice! The information contained in this document is for reference and information only.
The pilot is the final and only responsible party for the safe operation of this aircraft.
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1.4.3. Measured values of the center of gravity for the airplane TL-96 Star before test flying
Serial number: 00S52
Measured value Unit Front center of gravity Back center of gravity
Gp
kg
295
368
Go
kg
73
82
Gvzl
kg
365
450
Lb
mm
1710
1710
Lt
mm
344
315
La
mm
670
670
Xt
mm
326
355
X%
%
23
25
Detected position of the point of balance is 23-25%SAT for the front center of gravity with the
pilot weighting 70kg, for the back center of gravity with the crew weighting 149kg.
2.Operating restrictions
2.1. Restriction of the speed of the flight and reparation of position fault of air-
speed recorder
Presented speeds of the flight applies to the maximum take off weight of 450kg and at the
conditions of the sea level by the MSA. The speed are presented in kilometers per hour.
Take off speed
75
Climb speed
130
Cruising speed
180-220
Accession landing speed
120
The speed of bearing the surface
62
Maximum speed of horizontal flight
230
Never never-exceed speed Vne
275
Maximum speed at turbulence
180
Stalling speed with no flaps
72
Stalling speed with flaps 35degrees / 2
nd
grade flap / 62
Maximum speed for extending the 1st grade flaps Vfe 140
Maximum speed for extending the 2nd grade flaps Vfe 120
Vne is the never-exceed speed which the airplane can not fly
Vfe is the maximum speed for extending the lifting flaps, there are the same speed restrictions
for the flight with extended flaps as for their extension.
