Specifications

SECTION V
ABNORMAL PROCEDURES
MODEL 560
AUTOPILOT OUT OF TRIM (AP ROLL MISTRIM OR AP PITCH MISTRIM CAUTION LIGHT ON)
(Continued)
NOTE
Be prepared for minor control wheel force required to maintain desired flight path
3. Elevator, Rudder or Aileron Trim - CHECK, ADJUST as required.
4. Thrust - CHECK balanced.
5. Fuel Quantity - CHECK balanced.
6. Autopilot Button - ENGAGE as desired.
LANDING WITH FAILED PRIMARY FLIGHT CONTROL CABLE
RUDDER
1. Utilize rudder trim.
2. Yaw Damper - OFF.
3. If possible, choose a runway with least possible crosswind.
4. After touchdown, lower the nose and extend speed brakes as soon as possible.
CAUTION
• AVOID THE USE OF ASYMMETRIC THRUST REVERSERS DURING LANDING
ROLLOUT.
• NOSE WHEEL STEERING MAY NOT BE AVAILABLE, USE DIFFERENTIAL
BRAKING.
AILERON
1. Yaw Damper - OFF.
2. Use rudder for directional control limiting bank angle to 15 degrees maximum. Do not use
aileron trim except for gross adjustments.
3. If possible, choose a runway with least possible crosswind.
4. Land with flaps 15 degrees, V
APP
.
5. Flap Override Switch - GPWS FLAP OVRD ON (amber).
6. After touchdown, lower the nose and extend speed brakes as soon as possible.
7. Thrust Reversers - AS DESIRED.
NOTE
Multiply landing distance by 1.4 for flaps 15°.
ELEVATOR
1. Use manual elevator trim wheel for primary pitch control. Do not use electric trim.
2. Make small pitch and power changes and set up landing configuration early.
3. After touchdown and nose wheel on ground, extend speed brakes and apply wheel brakes as
soon as possible.
4. Land with flaps 15 degrees, V
APP
.
5. Flap Override Switch - GPWS FLAP OVRD ON (amber).
WARNING
DO NOT DEPLOY THRUST REVERSERS DURING LANDING ROLLOUT WITH
FAILED ELEVATOR CONTROL.
NOTE
Multiply landing distance by 1.4 for flaps 15°.
I 5-16 Configuration AA 56OMB-01