Specifications

SECTION IV
OPERATING INFORMATION
MODEL 560
LANDING
1. Throttles - IDLE.
NOTE
Eight seconds after touchdown, engines will spool down from flight idle to ground
idle if the GND IDLE switch is in NORM.
2. Brakes - APPLY (after touchdown).
CAUTION
f IF, DURING LANDING, A NORMAL BRAKE PEDAL - NO BRAKING CONDITION
IS ENCOUNTERED, OPERATE THE EMERGENCY BRAKE SYSTEM. CORRECT
PRIOR TO NEXT FLIGHT.
f ANTISKID SYSTEM DOES NOT FUNCTION DURING EMERGENCY BRAKING.
EXCESSIVE PRESSURE ON EMERGENCY BRAKE HANDLE CAN CAUSE BOTH
WHEEL BRAKES TO LOCK, RESULTING IN BLOWOUT OF BOTH TIRES.
NOTE
To obtain maximum braking performance from the antiskid system, the pilot must
apply continuous maximum effort (no modulation) to the brake pedals.
3. Control Wheel - APPLY FORWARD PRESSURE.
CAUTION
THE NOSEWHEEL MUST BE IN FIRM CONTACT WITH THE GROUND PRIOR TO
EXTENDING SPEEDBRAKES AND/OR DEPLOYING THRUST REVERSERS.
4. Speed Brake - EXTEND (after nosewheel firm ground contact).
5. Thrust Reversers - DEPLOY (after nosewheel firm ground contact).
WARNING
DO NOT ATTEMPT TO RESTOW REVERSERS AND TAKE OFF ONCE
REVERSERS HAVE STARTED TO DEPLOY.
NOTE
f To prevent any possible nose up pitch during thrust reverser deployment, maintain
forward pressure on the control column after the nosewheel is on the ground.
f To avoid possible jamming of the throttle lockout cams, do not exceed
approximately 15 pounds force on the thrust reverser levers until thrust reversers are
fully deployed.
6. Thrust Reverser Indicator Lights - CHECK ILLUMINATION OF ARM, UNLOCK AND DEPLOY
LIGHTS.
7. Reverse Thrust - AS REQUIRED. (Do not exceed 71.4% N
1
when OAT is at or above -18° C
or 68.3% N
1
when OAT is below -18° C).
8. Thrust Reversers - REVERSER LEVERS TO IDLE REVERSE AT 60 KIAS.
I 4-16 Configuration AA 56OMB-01