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of inflow to cockpit)
c. AIR SOURCE SELECT Knob - - - - - - - - - R (Check for sound
of inflow to cabin and cockpit)
d. AIR SOURCE SELECT Knob - - - - - - - - - - - - - - - - - - BOTH
7. Flight Controls- - - - - - - - - - - - - - - - - - - - - FREE and CORRECT
8. Flaps - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - SET
9. Speed Brakes - - - - - - - - - - - - - - - - - - - -CHECK and RETRACT
a. Extend Speed Brakes.
b. Advance throttles to the CRU Detent; verify speed brakes
retract and the SPD BRK EXTEND CAS message
extinguishes; throttles IDLE.
10. Electric Elevator Trim - - - - - - - - - - - - - - - - - - - CHECK and SET
(both pilot’s and copilot’s)
a. Push both sides of trim switch DOWN - - - - verify correct trim
wheel and pointer movement; press AP/TRIM DISC Switch - -
verify trim wheel stops moving.
b. Push both sides of trim switch UP - - - - - - - verify correct trim
wheel and pointer movement; press AP/TRIM DISC Switch - -
c. verify trim wheel stops moving.
Verify pilot’s trim switch command overrides copilot’s trim
switch command.
d. Set trim as required within TAKEOFF band.
11. Avionics Setup and Charts - - - - - - - - - - - - - - - - -AS REQUIRED
(Continued Next Page)
10 AA 510CLNP-07
Configuration
MODEL 510 NORMAL PROCEDURES
BEFORE TAXI (Continued)
12. Altimeters (pilot, standby and copilot) - - - - - -SET and COMPARE
Pilot and copilot altimeters must indicate departure field elevation
within +/-50 feet and within 75 feet of each other when set to local
altimeter setting.
13. Takeoff Data (V1, VR, V2, VENR, Takeoff Field Length, and Weight
Limits for appropriate takeoff flap setting) - - - - - 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
510CLNP-07 AA 11
Configuration
NORMAL PROCEDURES MODEL 510
TAXI
1. Brakes - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK
C A U T I O NCAUTION
IF DURING TAXI, A NO BRAKING CONDITION IS
ENCOUNTERED, OPERATE THE EMERGENCY BRAKE
SYSTEM. MAINTENANCE IS REQUIRED BEFORE FLIGHT.
2. Nosewheel Steering- - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK
3. Flight Instruments (including standby instruments) - - - - - CHECK
CROSSWIND COMPONENT
TEMPERATURE CONVERSION CHART
12 AA 510CLNP-05
Configuration
MODEL 510 NORMAL PROCEDURES
PILOT NOTES
510CLNP-05 AA 13
TAXI
Configuration
NORMAL PROCEDURES MODEL 510
STANDARD PERFORMANCE CONDITIONS
All takeoff and landing performance in this checklist is based on a paved,
dry runway.
TAKEOFF PERFORMANCE SIMPLIFIED CRITERIA
A simplified criteria is provided which is intended to cover the majority of
situations where runway length is appreciably longer than required for this
airplane. The other tabulated data gives more exact performance criteria
through a range of conditions which include all but the most extreme
cases.
The majority of takeoff situations result in field length margins that permit
using a single set of values for speeds and power settings for takeoff. If the
following conditions are met, the simplified procedures may be used.
1. No obstacle in flight path.
2. Throttles - - -TAKEOFF detent (Thrust mode indicator - green TO).
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
The values to be used are as follows:
When conditions are other than those specified in the simplified criteria,
the appropriate tabulated data must be referred to.
14 AA 510CLNP-05
Configuration
MODEL 510 NORMAL PROCEDURES
With a runway gradient, the zero runway gradient takeoff field length and V1
must be adjusted using the table below
510CLNP-06 AH 15
Configuration
NORMAL PROCEDURES MODEL 510
16 AH 510CLNP-06
Configuration
MODEL 510 NORMAL PROCEDURES
510CLNP-06 AH 17
Configuration
NORMAL PROCEDURES MODEL 510
　
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