Evector EV-97 EUROSTAR SL MICROLIGHT - Appendix 4 - Flight Test Record

EV-97 Eurostar SL Microlight Maintenance Manual GEN/EUR/04 Issue 4 45
Appendix 4 - Flight Test Record
Model Eurostar SL
Ser. No.:
Registration:G-
Engine Rotax 912UL
Ser. No.:
Take-off weight: Kg
Prop.: Woodcomp
Ser. No.:
Test flight take-off weight = 472.5KG +0, -10 KG
Regime: Limit
Result
Meteorological conditions
QNH
Temperature °C
Wind direction/speed
Pre-flight Engine
Checks
Full Throttle
Engine max. rpm static >4600 rpm
Oil temperature >50°C
Oil pressure 1.5 – 5 bar
Ignition
check
At 4000 rpm max. drop 300 rpm
max. difference 120 rpm
Idle
1400 - 1800 rpm
Take off & climb through 1000ft.
IAS 63kt
Engine speed max. 5500 rpm
Oil pressure 1.5 – 5 bar
Oil temp. max. 140°C
CHT max. 120°C
Time to climb 1000ft <1min:30sec
Fuel pressure 0.15 – 0.4 bar
Stall speed at idle (IAS)
Landing config. (flaps down)
<35kt(40mph)
Cruise config. (flaps up) <40kt(46mph)
Steep turns
Max. 60°
Never exceed speed
V
NE
= 127kt(146mph)
Engine speed <5800 rpm
Cruising speed at 2000 ft
At engine speed 4200
At engine speed 4600
At engine speed 4800 (max. continuous)
Oil temperature 50 – 120 °C
CHT 50 – 120 °C
Max. horizontal speed at 2000 ft.
At engine speed <5,800 rpm min.
110knots(127mph)
Oil temp. 50 – 120 °C
CHT 50 - 120°C
Date:
Location: Wycombe Air Park
Pilot’s Signature
Pilot’s Name: S. Pike
Transponder check at 3000 feet over Stokenchurch with Farnborough
satisfactory / not satisfactory