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31.7 − 32.6 4.0
32.7 − 33.7 3.8
33.8 − 34.7 3.6
34.8 − 36.5 3.4
36.6 − 38.0 3.2
NOTE
Trim data from the FMS should be rounded down to the
next lowest multiple of 0.2 trim units.
On airplanes NOT incorporating Service Bulletin 604–34–035:
NOTE
Usage of trim data from the FMS is prohibited.
NORMAL PROCEDURES
Flight Controls
04−10−4
REV 74, Nov 07/08
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. FLIGHT CONTROLS (CONT'D)
D. During Flight
When operating flight spoilers, do not release FLIGHT SPOILER lever until normal extension
or retraction of spoilers is ascertained.
NORMAL PROCEDURES
Flight Controls
04−10−5
REV 74, Nov 07/08
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
NORMAL PROCEDURES
Flight Controls
04−10−6
REV 74, Nov 07/08
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
THIS PAGE INTENTIONALLY LEFT BLANK
1. FLIGHT MANAGEMENT SYSTEM (FMS)
A. Prior to FMS Use
(1) FMS position information......................................Check for accuracy.
On airplanes 5500 and subsequent and airplanes incorporating Service Bulletin
604–34–031:
NOTE
1. The input parameters on the THRUST LIMIT, TAKEOFF REF and
APPROACH REF CDU pages must be re-confirmed by the pilot
following an FMS SYNC command, an FMS 3 reversion (if
installed) or an FMS cold start.
2. The engine bleed selection used for the FMS thrust setting
computations is based upon the sensed setting of the airplane
engine bleed cockpit switches, unless manually overridden by the
flight crew on the THRUST LIMIT CDU page.
The engine bleed selection used for the FMS V speed
computations is based upon the default setting (as selected on the
DEFAULTS 4/4 CDU page) or upon manual selection, by the flight
crew, for the anticipated take-off or approach configuration.
The engine bleed setting on the TAKEOFF REF and APPROACH
REF CDU pages represents the planned setting and not the
actual/sensed airplane setting.
3. In case of multiple obstacles, each obstacle clearance calculation
is done separately. For each obstacle, obstacle height and
obstacle distance from reference zero should be entered in the
FMS. The FMS computes and displays the geometric gross
level-off height and the required climb gradient for obstacle
clearance. The highest gross level-off height and the greatest
required climb gradient of all obstacles should be retained. Note
that an obstacle may be the most limiting for the required climb
gradient while another is the most limiting for the gross level-off
height.
The most limiting gross level-off height and required climb gradient
should be entered in the FMS. The FMS computes and displays
the take-off weight limited by obstacle clearance, which is used to
calculate the maximum take-off weight, to ensure all obstacles will
be cleared.
B. Prior to Overwater Operation
On airplanes 5301 to 5386 NOT incorporating Service Bulletin 604–24–002:
(1) Reversionary panel, FMS 3 switch
(if installed) ...........................................................Select to 1 for the duration of the
flight. FMS 3 is the preferred
nav source during overwater
operations.
NORMAL PROCEDURES
Navigation Systems
04−11−1
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. FLIGHT MANAGEMENT SYSTEM (FMS) (CONT'D)
C. After Periods of Dead Reckoning (DR) Navigation
(1) FMS position information......................................Check for accuracy.
2. INERTIAL REFERENCE SYSTEM (IRS)
A. Before Starting Engines
NOTE
Normal IRS alignment time is approximately 7 minutes.
When ambient temperatures are below –15°C (5°F), the IRS will
require a prolonged period of alignment.
(1) IRS selectors ............................................................ Set to NAV.
(2) FMS....................................................................... Enter present airplane position.
B. Subsequent Flights
NOTE
Rapid IRS alignment time is approximately 40 seconds.
(1) IRS selectors ............................................................ Set to OFF (for not more than 5
seconds), and then to NAV.
(2) FMS....................................................................... Enter present airplane position.
3. GLOBAL POSITIONING SYSTEM (GPS) (IF INSTALLED)
A. Before Starting Engines
　
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