Aerospool WT-9 Dynamic - Balked Landing Climb; Demonstrated Crosswind Performance; Effect on Flight Performance and Characteristics; Noise Data

WT-9 Dynamic Club S FLIGHT MANUAL Section 5 Page 5-
4
5.3.2 Balked landing climb
The data is valid for maximum landing weight 472,5 kg , wing flaps position 38
o
.
Engine ROTAX 912 ULS, engine speed 5500 r.p.m, Propeller MTV-21-A
Flight altitude (m) Airspeed IAS km/h
Rate of climb m/s
0 115 4,2
1000 115 3,9
2000 115 3,1
5.3.3 Effect on flight performance and characteristics
No disturbing effects on flight performance and characteristic of the aeroplane WT-9
Dynamic Club S were recorded during the flight tests.
5.3.4 Demonstrated crosswind performance
The maximum demonstrated crosswind speed for take-off and landing is 6 m/s
according to the airworthiness requirements.
5.3.5 Noise data
The maximum noise data 56,7 dB (A) was measured during the flight tests according
to the German noise requirement LS – UL 96.
Date: 15.1.2007 / Rev.: 4 „Appr“