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6. Circuit Breakers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IN
7. LANDING GEAR Handle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN
8. ANTISKID Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
9. All Other Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF or NORM
10. Elevator Trim. . . . . . . . . . . . . . . . . . . . . . CHECK/SET (trim indicator within TO trim range)
11. THROTTLES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CUTOFF
12. EMERGENCY GEAR RELEASE Handle . . . . . . . . . . STOWED and COVER INSTALLED
NOTE
Ground power must be disconnected to complete items 13, 14 and 15. The battery
disconnect switch does not disconnect ground power which will prevent a successful
test of the battery disconnect relay.
(Continued Next Page)
510FM-07 AA 3-137
SECTION III - OPERATING PROCEDURES MODEL 510
NORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
COCKPIT/CABIN INSPECTION (Continued)
13. BATTERY DISCONNECT Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DISCONNECT
14. BATT Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BATT (ALL DISPLAYS OFF)
15. BATTERY DISCONNECT Switch. . . . . . . . . . . . . . . . . . . . . . . . NORMAL/COVER DOWN
(PFD 1/2 and MFD powered)
16. Ground Power Unit (if desired) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CONNECTED
17. PARKING BRAKE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET
18. Pitot-Static Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PITOT STATIC (30 seconds); OFF
19. LANDING Light Switch . . . . . . . . . . . . . ON (Check illumination; OFF, if seen from cockpit)
20. Other EXTERNAL LIGHTING Switches ON (Check illumination; OFF, if seen from cockpit)
21. PAX SAFETY Switch . . . . . . . . . . . . . . . . . . . . . . PAX SAFETY (Check illumination); OFF
22. LANDING GEAR Position Lights . . . . . . . . . . . THREE GREEN LIGHTS / NO RED LIGHT
23. Database/Chart currency . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
24. Fuel Quantity and Balance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
25. FLAP Handle . . . . . . . . . . . . . . . . . . . . . . . AGREES WITH FLAP POSITION INDICATOR
26. AILERON and RUDDER TRIM. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK/SET
NOTE
• If a ground power unit is not used, expedite all checks with electrical power on and
make sure that the air conditioner switch is OFF.
• LANDING and NAV lights may be omitted if night flight is not anticipated.
3-138 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
NORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
EXTERIOR INSPECTION
During inspection, make a general check for security, condition, and cleanliness of the airplane and
components. Check particularly for damage; fuel, oil, and hydraulic fluid leakage; security of access
panels; and removal of keys from locks.
WARNING
Pitot tubes and Stall Warning Vane may still be hot.
1. Hot Items/Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
a. Left and Right Static Ports (4). . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR and WARM
b. Left and Right Pitot Tubes (2). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR and HOT
c. Stall Warning Vane . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CONDITION and HOT
d. LANDING Lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON (if not observed from cockpit)
e. BEACON Light . . . . . . . . . . . . . . . ON and FLASHING (if not observed from cockpit)
f. Right NAV and ANTI-COLLISION Lights . . . . . . . . . ON (if not observed from cockpit)
g. Left WING INSP, NAV and ANTI-COLLISION Lights ON (if not observed from cockpit)
2. EXTERNAL LIGHTING Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
3. BATT Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
4. Left Nose . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
a. Static Ports (2) and Surrounding Fuselage Skin. . . . . . . . . CLEAR and NO DAMAGE
b. OAT Probe Inlet and Sensors (2) . . . . . . . . . . . . . . . . . . . . CLEAR and NO DAMAGE
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Citation Mustang airplane flight manual 1(90)
