Garmin G5000 - Engine Failure During Final Approach

Model 560XL Section III – Operating Procedures
Emergency Procedures
Textron Aviation Citation 560XL 190-02313-03 Rev. 8
3-16 FAA Approved
 ENGINE FAILURE DURING FINAL APPROACH
Model Excel (Aircraft Serial Numbers 560 – 5001 through 560 – 5500)

IF FLAPS ARE 15° OR LESS (CONTINUE AND LAND AT 15° FLAPS)
1. Flaps – 15°.
2. TAWS Flap Override – ACTIVATE on GTC.
3. Landing Distance – MULTIPLY by 1.4.
4. Speedbrake – RETRACT.
5. Airspeed – V
APP
.
6. Rudder and Aileron Trim – TRIM toward operating engine as desired. Monitor slip/skid indicator
and mistrim indications.
Procedure completed
 IF FLAPS ARE 35° (CONTINUE AND LAND AT 35° FLAPS)
1. Continue and land at 35° Flaps.
Procedure completed
Model XLS (Aircraft Serial Numbers 560 – 5501 through 560 – 6000)
 IF FLAPS ARE 15° OR LESS (CONTINUE AND LAND AT 15° FLAPS)
1. Flaps – 15°.
2. TAWS Flap Override – ACTIVATE on GTC.
3. Landing Distance – MULTIPLY by 1.2.
4. Speedbrake – RETRACT.
5. Airspeed – V
APP
.
6. Rudder and Aileron Trim – TRIM toward operating engine as desired. Monitor slip/skid indicator
and mistrim indications.
Procedure completed
 IF FLAPS ARE 35° (CONTINUE AND LAND AT 35° FLAPS)
1. Continue and land at 35° Flaps.
Procedure completed