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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2.1.1. Airspeed indicator data reparation regarding the position fault of Pitot tube
Harming the by –passing in the area of placing the Pitot tube can run short that the speed data
indicated by the airspeed indicator do not correspond at all speed to the real aerial speed.
That´s why we do introduce the reparation of the indicated values for couple of the speed
ranges. The real speed is at about 6.3% - 8.2% lower than the speed indicated by the board
air-speed recorder. At low speed the relative mistake is lower and at higher speed the mistake
is increasing.
For security reasons / not extending the maximum allowed speeds /we choose the type of
lower real / calibrated / speed than the indicated speed.
All speed limits introduced in this guidebook as operating restrictions are initiated as the speeds
indicated by the air-speed recorder. There is no need for any recount in the way of functioning
of the airplane.
2.1.2. Reparation table of real and indicated air-velocity /km/h /
Indicated Actual Indicated Actual
I
ndicated Actual
60 58
110
103
160
148
70
67
120
112
170
157
80
76
130
121
180
167
90
85
140
130
190
176
100
94
150
139
2.2. .Weights and loads
2.2.1. Maximum and minimum weights
Maximum taking off weight 450kg
Maximum landing weight 450kg
Maximum weight of the fuel 49kg
Maximum load of one seat 90kg
Maximum weight of load behind the seats 4kg
Maximum weight of the crew 70kg
Empty airplane and detected position of the point of balance see point 1.4.3.
2.2.2.Sitting of the load
see point 2.10.
