Hoffman DIMONA H 36 Flight Manual page 12

Hoffmann
H 36 DIMONA
2.9 Cont.
To reduce the risk of encountering control flutter at Vne the following table should be used to determine
Vne at various altitudes.
ALTITUDE (m) 0 – 2000
(ft) 0 - 6500
Vne (km/h) 275
(kts)
Maneuvering speed (Va ) is the maximum speed at which application of full available aerodynamic
control will not overstress the airplane. Increasing altitude increases True Air Speed (TAS).
Indicated Airspeed Errors
The following table illustrates airspeed errors (IAS) due to positioning of the pitot pressure and pitot
static sources.
Pitot and Static Pressure source:
3000
10000
259
149 140
Leading edge Horizontal Stabilizer.
4000 5000
13000 16500
246 233
133 126
NOTE
11
2
Limitations
6000
20000
221
119
2—5