Specifications

SECTION VI
MODEL 560 EMERGENCY PROCEDURES
EMERGENCY PROCEDURES
ENGINE FAILURE OR FIRE, OR MASTER WARNING DURING TAKEOFF
SPEED BELOW V
1
- TAKEOFF SHOULD BE ABORTED.
5. Thrust Reverser Indicator Lights - CHECK ILLUMINATION of ARM, UNLOCK AND DEPLOY
LIGHTS.
6. Thrust Reverser - REVERSE THRUST ON THE UNAFFECTED ENGINE.
7. Thrust Reverser - REVERSE LEVER TO IDLE REVERSE AT 60 KIAS.
NOTE
f To obtain maximum braking performance from the antiskid system, the pilot must
apply continuous maximum effort (no modulation) to the brake pedals.
f The Takeoff Field Lengths assume that the pilot has maximum effort applied to the
brakes at the scheduled V
1
speed during the aborted takeoff.
8. When airplane comes to a stop - Refer to Emergency Procedures, EMERGENCY EVACUATION
(if appropriate).
SPEED ABOVE V
1
- TAKEOFF SHOULD NORMALLY BE CONTINUED.
IF ENGINE FIRE
4. At or above 400 feet AGL, or Minimum Obstacle Clearance Altitude, accomplish Emergency
Procedures, ENGINE FIRE (continue with step 5 after complete).
5. Flaps - RETRACT (at Level Off Altitude and V
2
+ 10 KIAS, accelerate to V
ENR
).
6. Throttle (operating engine) - SET Maximum Continuous N
1
.
IF ENGINE FAILURE
4. At or above 400 feet AGL, or Minimum Obstacle Clearance Altitude, accomplish Abnormal
Procedures, IN-FLIGHT RESTART - ONE ENGINE or Abnormal Procedures, ENGINE
FAILURE/PRECAUTIONARY SHUTDOWN (continue with step 5 after complete).
5. Flaps - RETRACT (at Level Off Altitude and V
2
+ 10 KIAS, accelerate to V
ENR
).
6. Throttle (operating engine) - SET Maximum Continuous N
1
.
1. Rotate - V
R.
2. Landing Gear - UP (after positive rate-of-climb).
3. Climb - V
2
until Level Off Altitude.
1. Brakes - AS REQUIRED.
2. Throttles - IDLE.
3. Speed Brakes - EXTEND.
4. Thrust Reverser - DEPLOY ON UNAFFECTED ENGINE.
I 56OMB-01 Configuration AA 6-3