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Eclipse Aviation Eclipse 500 - Page 44

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44
25. Ops Page……………………………………………………………..CHECK
a. Weights…….ENTER
Enter each pilot/passenger weight and any baggage.
b OAT…………ENTER
Use ATIS temperature, if available. If the OAT is not immediately accepted,
re-enter the OAT after taxi and prior to takeoff. Takeoff performance data is
NOT assured unless the OAT is properly entered.
c. Vr Speed………ENTER
Enter Vr speed computed from performance data.
26. Trims (3)……………………………………………………………….SET
Ensure all trims are in the green area. Failure to do so will result in “TO CONFIG
OK” not
being presented on CAS display. For most conditions, 10% nose down is
recommended for pitch trim.
27. Landing Altitude……………………………………………………..CHECK, SET
Set destination airfield elevation as printed in A/FD or approach plate.
28. AIR COND/FANS……………………………………………………..AS REQUIRED
Set air conditioner AUTO or OFF. Set desired temperature or “MAX
COOL/HEAT” and fan speed (AUTO, HIGH, MED, or OFF).
29. DC Voltage………………………………………………CHECK, 23 VDC MINIMUM
30. Chocks…………………………………………………………………REMOVED
ENGINE START
1. Throttles .....................................................IDLE
2. START BATT Switch ......................................ON
Ensure both engine selector switches are OFF
R AFT BUS Voltage: CHECK 23 VDC MINIMUM FOR BATTERY START; 25 VDC
MINIMUM FOR GPU START
3. R ENGINE Selector…………………………………………………..ON/START
The switch must be pushed in to move between OFF and ON/START.
The start cycle is complete when the red ITT limit line resets for normal operation.
CAUTION
Whenever the engine fails to light, a dry motoring cycle is required to clear out
trapped fuel or vapors. The high speed rotor (N
2
) should be allowed to
decelerate to zero RPM before attempting another start. Repeat complete
starting sequence, observing starter limits. (Refer to 2-8)

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