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f. Aft Compartment Access Door . . . . . . . . . . . . . . . . . . . . . . . . SECURE and LOCKED
11. Left Wing. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
a. Flap, Speed Brakes, Aileron, and Trim Tab . . . . . . . . . . . . . . . . . . . . . . . CONDITION
(Make sure flap and trim tab positions match indicators.)
b. Static Wicks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
(3 installed. 1 may be missing. No more than 2 total missing on entire airplane.)
c. Fuel Tank Vent . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR
d. Fuel Filler Cap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SECURE
e. Wing Deice Boot. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CONDITION
f. Vortex Generators (8 per wing) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CONDITION
g. Stall Strip. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CONDITION
h. Main Gear Door, Wheel, Tire, and Strut . . . . . . . . . . . . . . . . . . . . . . . . . . CONDITION
i. Fuel Quick Drains (4) . . . . . . . . . . . . . . DRAIN and CHECK FOR CONTAMINATION
12. Fuselage Left Side . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
a. Wing Inspection Light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CONDITION
b. Landing Light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CONDITION
c. Cabin Door Seal . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK for RIPS and TEARS
510FM-07 AA 3-141
SECTION III - OPERATING PROCEDURES MODEL 510
NORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
COCKPIT PREPARATION
1. BATTERY DISCONNECT Switch. . . . . . . . . . . . . . . . . . . . . . . . . . NORM / COVER DOWN
2. INTERIOR DISCONNECT Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORM
3. Circuit Breakers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IN
4. STBY INST Switch . . . . . . . . . . . . . . . . . . . . BATT TEST (5 seconds); GREEN LIGHT ON
5. STBY INST Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STBY INST; AMBER LIGHT ON
NOTE
• With the STBY INST switch in the BATT TEST position, the green TEST light
illuminates after 5 seconds indicating the circuit for the standby system is
functional and that there is sufficient battery capacity. If the green light does not
illuminate, this check may be deferred to the BEFORE TAKEOFF checklist after
the battery has an opportunity to charge. A satisfactory test must be completed
prior to takeoff.
• With the STBY INST switch in the STBY INST position, the amber ON light
illuminates indicating the standby instrument system is operating from the standby
battery pack. Once the Battery Switch is turned to BATT the amber light should
extinguish.
6. If Ground Power Unit is connected (for battery power only, skip to Step 7):
a. BATT Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
b. AVN PWR Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
c. BATTERY VOLTAGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK 28V
d. COCKPIT/CABIN FAN Knobs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS DESIRED
e. AIR COND Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS DESIRED
7. Cockpit Switches and Controls. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET
a. OXYGEN CONTROL VALVE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORMAL
b. L/R GEN Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . GEN (for battery start)
OFF (for GPU start)
c. L/R IGNITION Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORM
d. L/R FUEL BOOST Switches. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORM
e. FUEL TRANSFER Knob . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
f. Pilot MIC Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . HEADSET
g. ICE PROTECTION Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
　
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本文鏈接地址：Citation Mustang airplane flight manual 1(93)