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operation and no crew action is required.
(5) APU, START/STOP switch/light........................Press in and check the following:
• START light on.
• 60% rpm – START light out.
NOTE
Greater than 30% rpm
within 60 seconds.
• 95% rpm + 4 seconds
(approx) – AVAIL light on.
• 100% rpm + 15 seconds
(approx) – APU GEN OFF
caution message on.
On airplanes 5301 to 5630 NOT incorporating Service Bulletin 604–49–006 or
604–49–009:
(5) APU, START/STOP switch/light........................Press in and check the following:
• START light on.
• 60% rpm – START light out.
NOTE
Maximum 60 seconds
below 60% rpm.
• 95% rpm + 4 seconds
(approx) – AVAIL light on.
• 100% rpm + 15 seconds
(approx) – APU GEN OFF
caution message on.
NORMAL PROCEDURES
Auxiliary Power Unit
04−04−3
REV 66, Feb 01/07
▼
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. AUXILIARY POWER UNIT (CONT'D)
C. Starting the APU on Ground or in Flight – Subsequent Starts (Cont’d)
After APU RPM and EGT have stabilized:
(6) AC POWER, APU GEN switch................................. Set as required (Refer to Chapter
2: LIMITATIONS – POWER
PLANT).
(7) BLEED AIR, APU LCV switch/light........................... Set as required.
D. Stopping the APU
(1) AC POWER, APU GEN switch.............................Select to OFF/RESET.
Check APU GEN OFF caution
message on.
(2) APU, START/STOP switch/light......................Press out to shutdown the APU.
Check AVAIL light out.
If on ground:
(3) L and R PACK switch/lights.............................Press out
(4) BLEED AIR, APU LCV switch/light..................Press out to close load control valve.
Check APU LCV OPEN light
out.
When rpm decreases to below 50% and EGT to below 350°C (662°F):
(5) APU, PWR FUEL switch/light..........................Press out and check the following:
• APU GEN OFF caution
message out.
• STAT page – APU gauges
out (after approx 60 sec).
NORMAL PROCEDURES
Auxiliary Power Unit
04−04−4
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. AUTOMATIC FLIGHT CONTROL SYSTEM
NOTE
1. During a descent, when autopilot is in flight level change or
vertical speed mode with the flight director engaged, the flight
director may command excursions beyond VMO /MMO . Care
should be taken not to exceed VMO /MMO .
2. After generator transfers, if AFCS 2 is selected, the following
must be manually re-engaged:
• Yaw damper 2, and
• Autopilot (if it was coupled before power interruption).
A. Yaw Dampers – Before Take-Off
(1) YD 1 and YD 2 switch/lights ..............................Press in to engage both.
Check the following:
• YAW DAMPER caution
message out,
• YD 1 INOP status message
out, and
• YD 2 INOP status message
out.
B. Autopilot − After Take-Off
At an altitude not less than 320 feet AGL:
(1) AP switch/light ...................................................Press in to engage.
C. Autopilot − During Flight
(1) Autopilot operation .............................................Monitor Check for significant
discrepancy between L and R
elevator position.
D. AFCS − Before Landing
CAUTION
To avoid possible false localizer captures, do not arm approach until
airplane is close to, or established on, an inbound localizer course.
(1) Autopilot ........................................................Disengage at an altitude not less than
320 feet AGL.
If performing an autopilot-coupled ILS approach:
(1) Autopilot ........................................................Disengage at an altitude not less than
80 feet AGL.
(2) Flight Directors ................................................... Ensure both displayed.
NORMAL PROCEDURES
Automatic Flight Control System
04−05−1
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
NORMAL PROCEDURES
Automatic Flight Control System
04−05−2
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
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1. DOORS
NOTE
The main passenger door can be opened, closed, or used for static
open operation up to 60 knots windspeed.
A. Passenger Door
　
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