SECTION V
MODEL 560 ABNORMAL PROCEDURES
ABNORMAL PROCEDURES
ENGINE FAILURE/PRECAUTIONARY SHUTDOWN
1. AP TRIM DISC Button - PRESS and RELEASE.
2. Rudder and Aileron Trim - Trim toward operating engine as required.
3. Throttle (affected engine) - OFF.
4. Autopilot/Yaw Damper - ON as desired.
5. IGNITION Switch (affected engine) - NORM.
6. ENGINE SYNC Knob - OFF.
7. GEN Switch (affected engine) - OFF.
8. Electrical Load - REDUCE as required.
9. Fuel CROSSFEED Switch - AS REQUIRED (maximum imbalance 200 lbs.)
10. Affected ENGINE Anti-Ice - CHECK OFF.
11. WING XFLOW Switch - ON as required.
12. Refer to Abnormal Procedures, IN-FLIGHT RESTART - ONE ENGINE or Abnormal Procedures,
SINGLE-ENGINE APPROACH and LANDING.
IN-FLIGHT RESTART - ONE ENGINE (Refer to Figure 3-3 for Airstart Envelope)
FOLLOWING SHUTDOWN - WITH STARTER ASSIST
1. Throttle - OFF.
2. GEN Switch - ON.
3. ENGINE FIRE Switch (affected engine) - CHECK OPEN. (F/W SHUTOFF Caution Light L or R
extinguished).
4. IGNITION Switch - NORM.
5. ENGINE START L or R Button - PRESS momentarily.
6. Throttle - IDLE at 8% N
2
minimum.
7. Engine Instruments - MONITOR.
8. FUEL BOOST Pump - NORM.
IF START DOES NOT OCCUR
9. ENGINE START DISENGAGE Button - PRESS.
10. Accomplish Abnormal Procedures, ENGINE FAILURE/PRECAUTIONARY SHUTDOWN.
FOLLOWING SHUTDOWN - WINDMILLING WITH AIRSPEED ABOVE 200 KIAS AND N
2
ABOVE
8%. (Refer to Figure 3-3 for Airstart Envelope)
1. Throttle - OFF.
2. ENGINE FIRE Switch (affected engine) - CHECK OPEN. (F/W SHUTOFF Caution Light L or R
extinguished).
3. IGNITION Switch - ON.
4. FUEL BOOST Pump - ON.
5. Throttle - IDLE.
6. Engine Instruments - MONITOR.
7. FUEL BOOST Pump and IGNITION Switch - NORM (after engine stabilizes).
8. GEN Switch - ON.
I
56OMB-01 Configuration AL 5-5
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