Specifications

SECTION IV
OPERATING INFORMATION
MODEL 560
COCKPIT PREPARATION (Continued)
13. Warning Systems - TEST/OFF.
NOTE
The W/S TEMP annunciator may not test after cold soak at extremely cold
temperatures. If this occurs, repeat the test after the cabin has warmed up. The test
must be completed prior to each flight.
14. AVIONIC POWER Switch - OFF.
15. Windshield Ice Detection Lights - CHECK FOR ILLUMINATION.
DELAY BEFORE FLIGHT W/O GPU
1. STBY GYRO - OFF.
2. Battery Switch - OFF.
BEFORE STARTING ENGINES
1. Passenger Briefing - COMPLETED.
a. Emergency exit location and operation.
b. Use of emergency oxygen.
c. Smoking.
d. Seat adjustment - CHECK passenger seats are full upright, outboard and positioned aft or
forward to clear all exit doors, seat belts and shoulder harnesses secure.
2. Battery Switch - BATT.
3. PARK BRAKE - SET.
4. Wheel Chocks - REMOVED.
5. Pilot's Cockpit Side Window - CLOSED/LATCHED.
6. Exterior Lights - AS REQUIRED.
a. BEACON - ON.
b. NAV Lights - ON (during night operations).
7. Annunciators - CHECKED.
STARTING ENGINES
NOTE
f Either engine may be started first.
f If the aircraft has been cold soaked at temperatures below -10°C (+14°F), the use
of external power or warming the battery to -10°C (+14°F) or warmer is
recommended. This temperature may be checked with the battery temperature
gauge. Proper battery warmup may require extended application of heat to the
battery. Refer to Normal Procedures, Cold Weather Operations.
1. Engine - START.
a. ENGINE START Button - PUSH L or R; Button Light illuminates.
b. At 8% N
2
- THROTTLE TO IDLE.
c. Abort start if no ITT rise within 10 seconds.
d. Abort start if ITT rapidly approaches 700°C.
e. Abort start if no indication of N
1
rotation by 25% N
2.
f.Engine instruments - CHECK NORMAL.
(Continued Next Page)
I 4-8 Configuration AB 56OMB-01