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8. FUEL TRANSFER Knob. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
9. Anti-Ice/Deice Systems. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED
10. FLAP Handle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TO/APR (as required)
11. ANTISKID Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
12. LANDING Light Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
13. CAS Messages . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
14. Crew Briefing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COMPLETE (Include visibility call-outs,
GO-AROUND, and landing flap setting)
(Continued Next Page)
WEIGHT - POUNDS
6000 6500 7000 7500 8000 *8645
VREF LAND 82 85 88 91 94 98
VAPP 15° 87 91 95 98 101 105
* For use in an emergency which requires landing at weights in excess of 8000 lbs.
WEIGHT - POUNDS
6000 6500 7000 7500 8000 *8645
VREF 15° 98 102 105 109 112 117
VAPP 15° 98 102 105 109 112 117
* For use in an emergency which requires landing at weights in excess of 8000 lbs.
510FM-07 AA 3-125
SECTION III - OPERATING PROCEDURES MODEL 510
ABNORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
WINDSHIELD A/I INOPERATIVE APPROACH AND LANDING
(Continued)
BEFORE LANDING
15. LANDING GEAR Handle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOWN AND LOCKED
16. FLAP Handle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . TO/APR
17. Pressurization. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK ZERO DIFFERENTIAL
18. Autopilot/Yaw Damper . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF (50 feet above minimums)
19. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . VREF
20. Slip . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED to obtain and maintain runway visibility
21. Speed Brakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RETRACT PRIOR TO 50 FEET AGL
PROCEDURE COMPLETED
3-126 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
ABNORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
DOORS
AFT DOOR
Indicates that the tailcone baggage door is not locked.
• ON GROUND
1. Correct prior to flight. Secure baggage door if open, unlatched, or unlocked.
PROCEDURE COMPLETED
• IN FLIGHT
1. Land as soon as practical.
PROCEDURE COMPLETED
CABIN DOOR
Indicates the cabin door is not fully closed, latched and locked. Switches are located on the
inside handle, door pin mechanism, and the door frame.
• ON GROUND
1. Open the cabin door and close again.
2. Make sure inside handle is fully seated in the locked position.
3. Verify CAS message clears.
PROCEDURE COMPLETED
• IN FLIGHT
1. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . REDUCE
2. PAX SAFETY Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PAX SAFETY
3. Cabin Door . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . KEEP CLEAR
4. Altitude . . . . . . . . . . . . . . . . . . . . . . . . DESCEND (15,000 feet or lower recommended)
5. Land as soon as practical.
PROCEDURE COMPLETED
510FM-07 AA 3-127
SECTION III - OPERATING PROCEDURES MODEL 510
ABNORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
CHECK DOORS
Indicates that a nose baggage or cabin door monitor has not been properly tested or has failed.
This message is only displayed on the ground.
• IF A NOSE DOOR L-R OR CABIN DOOR MESSAGE ALSO
DISPLAYED
1. Open affected door.
2. Secure affected door making sure all latches and the key lock are properly secured.
3. Verify both CAS messages clear.
NOTE
This message can be caused by unlatching some of the nose baggage door latches
then re-latching them without fully unlatching and opening the door. Once a door is
partially unlatched, it must be fully opened and then latched and locked in order for
the door monitor to function properly.
PROCEDURE COMPLETED
IF MESSAGE DOES NOT CLEAR
4. Verify all doors are properly secured.
PROCEDURE COMPLETED
IF MESSAGE CLEARS
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Citation Mustang airplane flight manual 1(84)
