Specifications

SECTION VI
EMERGENCY PROCEDURES
MODEL 560
ENGINE FIRE (LH OR RH ENGINE FIRE WARNING LIGHT ON)
4. IGNITION Switch (affected engine) - NORM.
5. Throttle (affected engine) - OFF.
6. Electrical Load - REDUCE as required.
7. Affected ENGINE Anti-ice - CHECK OFF.
8. WING XFLOW Switch - ON as required.
IF FIRE WARNING LIGHT REMAINS ON AFTER 30 SECONDS
9. Remaining Illuminated BOTTLE ARMED Light - PUSH.
10. Land as soon as possible.
11. Refer to Abnormal Procedures, SINGLE-ENGINE APPROACH and LANDING.
IF LIGHT GOES OUT AND SECONDARY INDICATIONS ARE NOT PRESENT
2. Land as soon as practical.
3. Refer to Abnormal Procedures, SINGLE-ENGINE APPROACH and LANDING.
ENGINE FAILURE/FIRE DURING FINAL APPROACH
5. Rudder and Aileron Trim - TRIM toward operating engine as required.
6. Throttle (affected engine) - OFF.
7. Autopilot/Yaw Damper - ON as desired.
8. If engine fire, accomplish Emergency Procedures, ENGINE FIRE (LH OR RH ENGINE FIRE
WARNING LIGHT ON). Return to step 9 when complete.
9. Passenger Advisory Lights - PASS SAFETY.
10. Passenger Briefing - CHECK passenger seats full upright, outboard and positioned aft or forward
to clear all exit doors, seat belts and shoulder harnesses secure.
11. IGNITION Switch (operating engine) - ON.
12. Exterior Lights - AS REQUIRED.
13. Fuel CROSSFEED Switch - OFF.
14. ENGINE SYNC Knob - OFF.
15. Annunciators - CHECK.
16. GND IDLE Switch - NORM.
17. Pressurization - CHECK ZERO DIFFERENTIAL PRIOR TO LANDING.
18. Landing Gear - DOWN.
19. ANTI-SKID Switch - CHECK ON.
20. Landing Lights - AS DESIRED.
21. Flaps - LAND (35°).
22. Airspeed - V
REF
.
23. Autopilot and Yaw Damper - OFF (400 feet AGL and below).
24. Speed Brakes - RETRACT (50 feet AGL and below).
1. AP TRIM DISC Button - PRESS and RELEASE.
2. Thrust (operating engine) - INCREASE as required.
3. Airspeed - V
APP
.
4. Flaps - T.O. & APPR (15°).
1. Throttle (affected engine) - IDLE.
IF LIGHT REMAINS ON
2. ENGINE FIRE Switch (affected engine) - LIFT COVER and PUSH.
3. Either Illuminated BOTTLE ARMED Light - PUSH.
I 6-4 Configuration AA 56OMB-01