TL Ultralight TL-2000 Sting S4, Руководство по эксплуатации для пилотов

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4-7
5.
VHF attitude reference.……………………..……………….…SET
6.
Transponder…………………………………...………....ON / ALT
7.
Trim…………………………………………………………….....AFT
11.
Controls………..........…….FREE and CORRECT MOVEMENT
12.
Doors…………………………….…….…CLOSED and LOCKED
13.
GRS safety pin………………………….…..CHECK REMOVED
14.
Aux fuel pump………………………...…………AS REQUIRED
Operation of both the engine driven and the auxiliary
fuel pump for take-off and landing is not recommended.
The combined pump output has been observed to
overcome the carburetor float valve fuel cutoff, flooding
the carburetor, preventing full power engine operation or
cause engine failure.
4.2.6 Takeoff
1. Flaps..................................................................CHECK (HALF)
2. Throttle...............................................................................FULL
3. Rotate..............................................................................45 KIAS
4. Throttle..................................MONITOR (5800 RPM maximum)
5.
Climb………………………...…...…………………..……..75 KIAS
6.
Flaps…………………………….……...…RETRACT AT 500 AGL
4.2.7 Climb
1.
Throttle…...........................SET TO 5500 RPM (or as required)
2. Climb...............................................................................75 KIAS
3. Trim..........................................................ADJUST AS NEEDED
4. EMS data.........................................................................CHECK
5.
Aux Fuel Pump………………......…….…………….OFF (if used)
4.2.7.1 Best angle of climb speed
Best angle of climb speed (V
x
) is 50 KTS
WARNING