MDM MDM-1 FOX, Руководство по эксплуатации самолета

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MDM-1 „FOX” FLIGHT MANUAL
Appr. 2.2
Issue III
2.1 Introduction.
Section 2 includes operating limitations, instrument markings and basic placards informing on
limitations necessary for safe operation of the glider, its systems and standard equipment.
The limitations contained in this Section and in Section 9 have been approved by Civil Aircraft
Inspection Board.
2.2 Airspeed.
Airspeed limitations and their operational significance, used in this Manual are shown below:
Speed (IAS) [km/h] [kt] Remarks
V
NE
Never exceed speed 282 152 Do not exceed this speed in any operation
and do not use more than 1/3 of control
deflection
V
RA
Rough air speed 225 122 Do not exceed this speed except in smooth
air and then only with caution. Examples
of rough air are: lee-wave rotor,
thunderclouds etc.
V
A
Manoeuvring speed 214 116 Do not make full or abrupt control
movements above this speed, because
under certain conditions the glider may be
overstressed by full control movement.
V
W
Maximum winch-
launching speed 150 81 Do not exceed this speed during winch-
launching.
V
T
Maximum aerotowing
speed 150 81 Do not exceed this speed during
aerotowing.
WARNING: In high altitude flight, the true airspeed (TAS) is higher than value indicated by
airspeed indicator (IAS). To maintain the safe margin against the flutter limit
related to true airspeed value, VNE must be reduced with altitude to values specified
in the following table.
Flight altitude Never exceed
speed V
NE
IAS
Flight altitude Never exceed
speed V
NE
IAS
[m] [km/h] [ft] [kt]
0-3000 282 0-10000 152
4000 267 13000 145
5000 253 16000 138
5500 246 18000 133
7
Rev. 7/ June 2019