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7. LANDING Light Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED
8. Pressurization. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
9. Altimeters (transition altitude) . . . . . . . . . . . . . . . . . . . . . . . . SET STD and CROSSCHECK
NOTE
Press the PFD BARO Knob to select standard pressure on the PFD altimeters. Set
29.92 IN HG (1013 MB) on Standby Altimeter.
CRUISE
1. THROTTLES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CRU DETENT or AS DESIRED
NOTE
The throttles should be reduced to the CRU detent or below within 10 minutes after
reaching an intermediate or final cruise altitude. The use of CLB during normal
operations beyond 10 minutes after reaching cruise altitude will significantly decrease
engine life and increase operator costs.
2. Anti-Ice/Deice Systems . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED
CAUTION
Do not operate Deice Boots when indicated RAT is below -30°C.
3. Pressurization. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
4. In RVSM Airspace:
a. Autopilot . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ALT Mode unless severe
turbulence is encountered
b. Altimeters . . . . . . . . . . . . . . . . . . . . . . . CROSSCHECK pilot and copilot altimeters at
1 hour intervals or less. Maximum allowed difference is 200 feet.
DESCENT
1. Pressurization. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . VERIFY destination field elevation set
2. Anti-Ice/Deice Systems . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED
3. THROTTLES . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED for anti-ice/deice systems
4. Altimeters (transition altitude) . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET and CROSSCHECK
5. Landing Data (VAPP, VREF, Landing Distance, Weight, and Factors). . . . . SET and VERIFY
6. LANDING Light Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED
3-148 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
NORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
APPROACH
1. Landing Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CONFIRM
2. Seats and Seat Belts . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADJUST and SECURE
3. Avionics and Flight Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
NOTE
TAWS terrain and obstacle alerts are possible during some instrument approaches
when the airplane is on a normal flight path. If an alert occurs during approach and the
aircraft is confirmed to be on an appropriate flight path, the TAWS INHIB function may
be used to silence the alert. If there is any uncertainty, climb until the TAWS alert
ceases and execute the missed approach as required.
4. Minimums . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET
5. PAX SAFETY Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PAX SAFETY
6. Passenger Seats . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK FULL UPRIGHT
7. FUEL TRANSFER Knob. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
8. Anti-Ice/Deice Systems. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED
9. LANDING Light Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
10. FLAP Handle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TO/APR
11. CAS Messages . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
12. Crew Briefing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COMPLETE
BEFORE LANDING
1. Landing Gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN and LOCKED
2. Speed Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRACTED
3. FLAP Handle . . . . . . . . . . . . . . . . . . . . . . . . . . . LAND (STALL WARNING-NORMAL only)
4. Pressurization . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK ZERO DIFFERENTIAL
5. Autopilot and Yaw Damper . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
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Citation Mustang airplane flight manual 1(100)
