Tecnam P92 Eaglet - Page 60

P92 Eaglet
Flight Manual
Revision Date: 12-14-2007
Revision Number: 1.00
Doc n° 27-13-100-00
60
Carburetor Heat:........................................................................ CHECK
Throttle:..................................................................................... IDLE
Fuel quantity indicators:............................................................ CHECK
Fuel selector valves:.................................................................. BOTH ON
Flaps:......................................................................................... T/O (15°)
Flight controls: .......................................................................... CHECK
Trim:.......................................................................................... CENTER
Seat belts: .................................................................................. FASTENED
Doors:........................................................................................ CLOSED AND LOCKED
Transponder (if installed):......................................................... ALT
6.2.1.8 TAKEOFF AND CLIMB
Parking brake: ........................................................................... OFF
Carburetor heat:......................................................................... OFF
Taxi to line-up:
Magnetic compass and DG: ...................................................... CHECK, SET
Throttle:..................................................................................... FULL
NOTE
Static RPM is approximately 5100 ± 250 rpm
Engine instruments:................................................................... CHECK
Vr (Rotation speed):.................................................................. ~ 48 KIAS
NOTE
Rotate to takeoff attitude and accelerate to a climb speed of 60 knots with 15° Flaps
Above 300’ AGL:
Flaps:......................................................................................... RETRACT
Establish Vy clean:.................................................................... 68 KIAS
Trim:.......................................................................................... ADJUST
Cruise climb:............................................................................. 75 – 80 KNOTS
6.2.1.9 CRUISE
Reaching cruise altitude:
Throttle:..................................................................................... SET (5500 RPM Max)
Engine instruments:................................................................... CHECK
• Oil temperature: .........................90°-110 ° C
• Cylinder head temperature:.......90° - 135 °C
• Oil pressure:.....................................2 - 5 bar
• Fuel pressure:........................0.15 – 0.40 bar
CAUTION
Normal position of the fuel selectors is both on. Check fuel balance and fuel pressure. If necessary, shut off the higher
reading tank using the appropriate fuel shutoff valve. Check fuel pressure again. BE SURE THAT ONE TANK IS
FEEDING THE ENGINE AT ALL TIMES!
NOTE
Check fuel gauges frequently with one tank shut off to prevent fuel starvation.
6.2.1.10 BEFORE LANDING
Landing light (if installed):........................................................ ON
On downwind leg: Speed and flaps at your discretion based on traffic, etc.
Traffic:....................................................................................... CHECK
Flaps:......................................................................................... AS DESIRED
Optimal touchdown speed (full flaps):...................................... 40 KNOTS