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5. Operating Engine N2 - - - -INCREASE to 55%
(for a cross-generator start)
6. Other Engine - - - - - - - - - - - - - - - - - START;
repeat steps 1 through 4
7. Ground Power Unit - - - - - - - -DISCONNECT
(if applicable)
8. L/R GEN Switches - - - - - - - - - - - - - - - GEN
9. AVN POWER Switch - - - - - - - - - - - - - - - ON
10. DC AMPS/VOLTS- - - - - - - - - - - - - -CHECK
BEFORE TAXI
1. COCKPIT/CABIN FAN Knobs -AS DESIRED
2. AIR COND Switch- - - - - - - - - -AS DESIRED
3. COCK/CABIN TEMP Knobs- - -AS DESIRED
4. WINDSHIELD ANTI-ICE Switches - - - - - AS
REQUIRED
5. Avionics Glareshield Cooling Fans (3)- - - - - -
CHECK FOR AIR FLOW
6. Air Source Select System - - - - - - - -CHECK
7. Flight Controls - - - - - -FREE and CORRECT
8. Flaps- - - - - - - - - - - - - - - - - - - - - - - - - -SET
9. Speed Brakes - - - - CHECK and RETRACT
10. Electric Elevator Trim - - - - CHECK and SET
11. Avionics Setup and Charts- - AS REQUIRED
12. Altimeters - - - - - - - - - -SET and COMPARE
13. Takeoff Data- - - - - - - - - - - SET and VERIFY
14. Destination Field Elevation - - - - - - - - - -SET
15. Radar - - - - - - - - - - - - - - - - - - - - STANDBY
16. CAS/PFD Messages- - - - - - - - - - - - CHECK
*** CLEARED / READY FOR TAXI ***
17. PAX SAFETY Switch - - - - - - - - SEAT BELT
18. EXTERNAL LIGHT Switches AS REQUIRED
19. Brakes- - - - - - - - - - - - - - APPLY and HOLD
20. PARKING BRAKE - - - - - - - - - - - RELEASE
TAKEOFF PERFORMANCE SIMPLIFIED
CRITERIA
1. No obstacle in flight path
2. Throttles - TAKEOFF Detent
3. Takeoff and approach flaps (15°)
4. Anti-Ice OFF or ON
5. Takeoff field length available = 5,000 feet or
longer
6. No tail wind
7. Runway Gradient - Takeoff = Zero to -2.0%
(downhill)
8. Dry paved runway
When conditions are other than those specified in the
simplified criteria, the appropriate tabulated data
must be referred to.
TAXI
1. Brakes- - - - - - - - - - - - - - - - - - - - - - CHECK
2. Nosewheel Steering - - - - - - - - - - - - CHECK
3. Flight Instruments (including standby)CHECK
BEFORE TAKEOFF
1. Anti-Ice/Deice systems (if required) - CHECK
2. STBY INST Switch - - - BATT TEST; GREEN
LIGHT; STBY INST (if not completed previously)
3. Passenger Seats - - - - - - - - FULL UPRIGHT
4. Flaps- - - - - - - - - - - - - -SET FOR TAKEOFF
5. Trims (3) - - - - - - - - - - -SET FOR TAKEOFF
6. Speed Brakes - - - - - - - - - - - -RETRACTED
7. Transponder - - - - - - - - - - - - - - - - - - - GND
8. Displays / Avionics / Navigation
Systems - - - - - - - - - - - - - - - - - - - - SETUP
9. Crew Briefing - - - - - - - - - - - - - -COMPLETE
*** CLEARED / READY FOR TAKEOFF ***
10. Pitot-Static Switch- - - - - - - - - PITOT STATIC
11. ENGINE ANTI-ICE Switches AS REQUIRED
12. WINDSHIELD ANTI-ICE Switches - - - - - AS
REQUIRED
13. PAX SAFETY Switch - - - - - - -PAX SAFETY
14. LANDING Light Switch - - - - - -AS DESIRED
15. ANTI-COLL Light Switch - - - - - - - - - - - - ON
16. Radar - - - - - - - - - - - - - - - - AS REQUIRED
17. EICAS- - - - - - - - - - - - - - - - - - - - - - CHECK
TAKEOFF
1. THROTTLES - - - - - - - - - - - - - - - TO Detent
2. Engine Instruments- - - - - CHECK NORMAL
3. Brakes- - - - - - - - - - - - - - - - - - - - RELEASE
4. Elevator Control - - - - - - - - - - - - ROTATE at
VR to +10° initial pitch attitude
AFTER TAKEOFF / CLIMB
1. LANDING GEAR Handle - - - - - - - - - - - - UP
2. FLAP Handle - - - - - - - - - - - - - - - - - - - - UP
(V2 + 12 and clear of obstacles)
3. THROTTLES - - - - - - - - - - - - - - CLB Detent
4. Yaw Damper - - - - - - - - - - - - -AS DESIRED
(ON Above FL300)
5. Anti-Ice/Deice Systems - - - - AS REQUIRED
6. PAX SAFETY Switch - - - - - AS REQUIRED
7. LANDING Light Switch - - - - AS REQUIRED
8. Pressurization - - - - - - - - - - - - - - - - CHECK
9. Altimeters (transition altitude)- -SET STD and
CROSSCHECK
510CLNP-07 AK 59.1
Configuration
QUICK REFERENCE CHECKLIST MODEL 510
60 AA 510CLNP-07
CRUISE
1. THROTTLES - -CRU Detent or AS DESIRED
2. Anti-Ice / Deice Systems - - - AS REQUIRED
3. Pressurization - - - - - - - - - - - - - - - -CHECK
4. In RVSM Airspace:
a. Autopilot - - - - -ALT Mode unless severe
turbulence is encountered.
b. Altimeters - - - CROSSCHECK pilot and
copilot altimeters at 1 hour intervals or
less. Maximum allowed difference is 200
feet.
DESCENT
1. Pressurization - - - - - - - - - - - - - - - -VERIFY
destination field elevation set
　
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