Aerospool DY043-04 Serie Manuel D'entretien Et De Réparation page 86

DYNAMIC WT9
5.1.4 Procès verbal du vol d'essai
Take-off weight:
Model:
DYNAMIC WT9
Engine: R 912 ULS
Propeller: SR 2000
Meteorological conditions
Engine check
Take-off and climbing to 1000 m ISA (
3300 ft )
IAS = 120 km/h ( 65 kts )
Stalling speed at idling
Steep turns
Never exceed speed
Cruising speed at engine speed:
Altitude 500 m ISA ( 1650 ft )
4800- km/h
5200- km/h
Maximum horizontal speed
Altitude 500 m ISA ( 1650 ft )
Landing
Date:
Report: Flight Test Results comply with Type Certificate.
Date: Novembre 2003
Flight Test Record
S/N:
S/N:
S/N:
RESULTS: ( Airspeed are IAS )
Regime
Full throttle
Idling
5000- km/h
5500- km/h
DYNAMIC WT9
MANUEL D'UTILISATION, D'ENTRETIEN ET DE REPARATION
Registration:
Hours flown:
No. of take-offs:
On ground pressure QNH
On groun temperature QMU
Wind direction / velocity
Engine speed 4900±200 rpm
Oil temperature 50
Oil pressure 1.5 – 5.0 bar
Ignition check 3850 rpm
Engine speed drop max 300 rpm
with either magneto switched off
1400 + 100 rpm
Engine speed max. 5500 rpm
Oil pressure 1.5 – 5.0 bar
Oil temperature 130
o
CHT 135 C
Time of climbing
300-1000 m ISA (1000-3300 ft)
Landing configuration
(flaps fully extended)
V = 50 km/h ( 27 kts )
SO
Cruise configuration
V = 60 km/h ( 33 kts )
S1
o
max. 45
V = 270 km/h IAS ( 262 CAS )
NE
Engine speed max. 5800 rpm
Airspeed at 5000 rpm
min. 160 km/h IAS ( 156 CAS )
86 kts IAS ( 84 CAS )
Oil temperature 90-110
o
CHT 60-135 C
Airspeed at 5750 rpm
min. 220 km/h IAS ( 215 CAS )
Oil temperature 90-130
o
CHT 60-135 C
Touch down speed
Pilot´s signature:
Test
o
o
C
L:
R:
o
C
o
C
o
C
Section 5
HPa
o
C
/ m/s
rpm
o
C
bar
rpm
rpm
bar
o
C
o
C
min
km/h
km/h
s
km/h
km/h
km/h
o
C
o
C
km/h
o
C
o
C
km/h
Page 5 - 5