Flugzeugbau Ventus-2C - 2.15 Limitation Placards

May 2006 LBA-app.
Revision 2 TN-No. 349-32 2.15
*) As the actual minimum or maximum
seat load of this aircraft (to which this
manual refers) may differ from these
typical weights, the placard in the cockpit
must always show the actual values,
which are also to be entered in the log
chart - see section 6.2.
For further placards refer to the Maintenance Manual.
2.15 Limitation placards
SCHEMPP-HIRTH FLUGZEUGBAU GmbH., KIRCHHEIM/TECK
Ventus-2c FLIGHT MANUAL
WEAK LINK FOR TOWING
Maximum 765 daN (1687 lb)
TIRE PRESSURE
Main wheel: 4.0 bar (58 psi)
Tail wheel : 2.5 bar (36 psi)
LOAD ON PILOT’S SEAT
(pilot and parachute)
Minimum load: kg/ lb
Maximum load: kg/ lb
154*
243*110*
For seat loads below placarded minimum
refer to Flight Manual, section 6.2
70*
Flap setting -1, -2, S, S1 285 154 177
Flap setting L, +2, +1, 0 200 108 124
Rough air speed 200 108 124
Maneuvering speed 200 108 124
Aerotowing speed 180 97 112
Winch launching speed 150 81 93
Landing gear operating speed 180 97 112
For 18 m span 1323 lb / 600 kg
For 15 m span 1157 lb / 525 kg
MAXIMUM PERMITTED SPEEDS (IAS): km/h kt mph
MAXIMUM PERMITTED ALL-UP MASS Max. permitted speed
0
1000
2000
3000
4000
5000
6000
7000
8000
9000
10000
Altitude
[m] [ft]
285
285
285
266
253
240
227
215
203
191
180
V
NE
(IAS)
km/h kt mph
154
154
154
143
136
129
122
115
109
102
97
177
177
177
166
157
149
141
134
126
119
112
0
3281
6562
9843
13123
16404
19685
22966
26247
29528
32808