Specifications

SECTION IV
MODEL 560 OPERATING INFORMATION
AFTER TAKEOFF - CLIMB
1. Landing Gear - UP.
2. Flaps - UP.
3. Throttles - SET CLIMB N
1
.
4. ENGINE SYNC Knob - ON.
5. Yaw Damper - ENGAGE.
6. IGNITION Switch - NORMAL. (ON when flying in heavy rain).
7. Passenger Advisory Lights - AS REQUIRED.
8. Pressurization - CHECK.
9. Altimeters- SET and CROSS CHECK (transition altitude).
10. REC/TAXI Lights - OFF (transition altitude).
11. A/C COMPRESSOR - OFF or FAN (above 18,000 feet).
12. Anti-Ice/Deice - AS REQUIRED.
CRUISE
1. Throttles - SET CRUISE N
1
.
2. Pressurization - CHECK.
3. Anti-Ice/Deice - AS REQUIRED.
CAUTION
DO NOT OPERATE DEICE BOOTS UNDER ANY OF THE FOLLOWING CONDI-
TIONS BECAUSE BOOT CRACKING MAY RESULT:
AIRSPEEDS AT OR ABOVE 150 KIAS AND THE RAT IS LESS THAN OR
EQUAL TO -35
°C (-31°F).
AIRSPEEDS BELOW 150 KIAS AND THE RAT IS LESS THAN OR EQUAL TO
-40
°C (-40°F).
NOTE
f Ignition switches should be selected to ON when flying through heavy rain.
f Check deice systems for proper operation prior to entering areas in which icing
might be encountered.
f The pilot’s and copilot’s footwarmers should be opened for a short period during
cruise to purge the side windows of moist air.
4. Fuel CROSSFEED - AS REQUIRED (maximum imbalance 200 lbs.)
I 56OMB-01 Configuration AA 4-13