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b. VERIFY WING DE-ICE FAIL and TAIL DE-ICE FAIL messages display after 6
seconds.
c. WING/STAB Deice Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
d. Pitot-Static Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . RESET STALL WARN then OFF
DELAY BEFORE FLIGHT WITHOUT GPU
1. STBY INST Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
2. BATT Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
510FM-07 AJ 3-143
SECTION III - OPERATING PROCEDURES MODEL 510
NORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
BEFORE STARTING ENGINES
1. If delayed before flight without GPU:
a. STBY INST Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STBY INST
b. BATT Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BATT
2. Preflight Inspection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COMPLETE
3. Wheel Chocks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . REMOVED
4. Cabin Door . . . . . . . . . . . . . . . . . . CLOSED Check indicators for proper door pin position,
no CABIN DOOR message displayed, and handle latched
5. Passenger Briefing . . . . . . . . . . . . . . . . . . COMPLETE (Include seat/seat belt adjustment,
emergency exits, smoking, and emergency use of oxygen)
6. Seats and Seat Belts . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADJUST and SECURE
7. EXTERNAL LIGHTING Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED
8. AIR COND Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
9. COCKPIT/CABIN FAN Knobs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
10. EICAS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
11. BATTERY VOLTAGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
STARTING ENGINES
1. ENGINE START Button . . . . . . . . . . . . PRESS MOMENTARILY (Verify button illuminates)
2. THROTTLE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE
3. Engine Instruments. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MONITOR
a. N1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Abort start if no N1 indication by 40% N2
b. ITT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK FOR RISE
Abort start if ITT rapidly approaches 830°C or shows no rise within 10 seconds.
Do not exceed 830°C for more than 5 seconds, limit 862°C.
c. Oil Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STEADY INCREASE
d. Engine must reach stabilized idle within 45 seconds.
e. N2 display digits will change from WHITE to GREEN when FADEC start sequence is
completed.
4. Engine Instruments. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK NORMAL
(Battery Current less than 100 Amps)
NOTE
Following a battery start, the battery current should be allowed to decrease to 100
Amps or less prior to attempting a cross-generator start to make sure that sufficient
battery capacity exists for the engine start. To make sure that adequate generator
capacity exists, increase the operating engine N2 to 55% before a cross-generator
start.
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 (if ground power was used)
9. AVN PWR Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
10. DC AMPS/VOLTS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
a. L GEN Switch . . . OFF (L AMP decrease, R AMP increase, battery voltage 28 Volts.)
b. L GEN Switch . . . . . . . . . . . . . . . . GEN (L AMPS increase, battery voltage 28 Volts.)
c. R GEN Switch . . OFF (R AMP decrease, L AMP increase, battery voltage 28 Volts.)
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Citation Mustang airplane flight manual 1(95)
