曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

a. AIR SOURCE SELECT Knob. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF (No Inflow)
b. AIR SOURCE SELECT Knob. . . . . . . . . . . . . L (Check for sound 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
NOTE
• With the Air Source Select knob in the R position, the bleed air inflow will primarily
be into the cabin with a small amount going to the cockpit.
• With the Air Source Select knob in the BOTH position and the aircraft on the
ground, there will be no bleed air inflow if the temperature is above 18°C (65°F)
until the throttles are advanced for takeoff. At temperatures of 18°C (65°F) or
colder, bleed air is available to assist in heating the cabin and cockpit.
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 - verify trim wheel stops moving.
c. 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
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
(Continued Next Page)
510FM-07 AA 3-145
SECTION III - OPERATING PROCEDURES MODEL 510
NORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
BEFORE TAXI (Continued)
*** 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
TAXI
1. Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
CAUTION
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
BEFORE TAKEOFF
1. Anti-Ice/Deice systems (if required) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
a. Engine Speed. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AT or ABOVE 70% N2
b. L/R ENGINE ANTI-ICE Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
c. L/R ENG A/I COLD CAS message. . . . . . . . . . . . . . . . . DISPLAY, then EXTINGUISH
(within one minute or less)
NOTE
At ambient temperatures above approximately 10°C (50°F), the white ENG A/I COLD
messages may not display. In this case, satisfactory operation of the engine anti-ice
　
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本文鏈接地址：Citation Mustang airplane flight manual 1(98)