Aerospool WT-9 Dynamic - Page 87

TECHNICAL DESCRIPTION, OPERATING, MAINTENANCE AND REPAIR MANUAL
5.1.4 Flight Test Record
Flight Test Record
Take-off weight:
Model: WT-9 Dynamic S/N: Registration:
Engine: R 912 S2 S/N: Hours flown:
Propeller: SR 2000 S/N: No. of take-offs:
RESULTS: ( Airspeed are IAS )
Regime Test
On ground pressure QNH
HPa
On groun temperature QMU
o
C
Meteorological conditions
Wind direction / velocity
o
/ m/s
Engine speed 4900±200 rpm
rpm
Oil temperature 50
o
C
o
C
Oil pressure 1.5 – 5.0 bar
bar
Full throttle
Ignition check 3850 rpm
Engine speed drop max 300 rpm
with either magneto switched off
L:
R:
Engine check
Idling
1400 + 100 rpm
rpm
Engine speed max. 5500 rpm
rpm
Oil pressure 1.5 – 5.0 bar
bar
Oil temperature 130
o
C
o
C
CHT 135
o
C
o
C
Take-off and climbing to 1000 m ISA (
3300 ft )
IAS = 120 km/h ( 65 kts )
Time of climbing
300-1000 m ISA (1000-3300 ft)
min
Landing configuration
(flaps fully extended)
V
SO
= 50 km/h ( 27 kts )
km/h
Stalling speed at idling
Cruise configuration
V
S1
= 60 km/h ( 33 kts )
km/h
Steep turns
max. 45
o
s
V
NE
= 270 km/h IAS ( 262 CAS )
km/h
Never exceed speed
Engine speed max. 5800 rpm
km/h
Airspeed at 5000 rpm
min. 160 km/h IAS ( 156 CAS )
86 kts IAS ( 84 CAS )
km/h
Oil temperature 90-110
o
C
o
C
Cruising speed at engine speed:
Altitude 500 m ISA ( 1650 ft )
4800- km/h 5000- km/h
5200- km/h 5500- km/h
CHT 60-135
o
C
o
C
Airspeed at 5750 rpm
min. 220 km/h IAS ( 215 CAS )
km/h
Oil temperature 90-130
o
C
o
C
Maximum horizontal speed
Altitude 500 m ISA ( 1650 ft )
CHT 60-135
o
C
o
C
Landing
Touch down speed
km/h
Date: Pilot´s signature:
Report: Flight Test Results comply with Type Certificate.
Date: 01.03.2002 WT-9 Dynamic Section 5 Page 5 - 6