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amount of braking necessary, to prevent heat build-up in the affected gear. Sharp turns should be
avoided.
Taxiing completely clear of the runway is acceptable, provided only one tire per gear is flat. In
cases where both tires of a gear are flat, taxiing is not recommended except in the interests of
safety, because the airplane will then be rolling on the wheel rims.
NOTE
The duration of taxiing with a flat or blown-out tire should be kept to a
minimum, since the remaining tire could also blow out.
2. TOWING WITH FLAT TIRE(S)
Normal towing procedures are acceptable when only one tire per gear is flat, and the airplane
weight is not greater than the maximum landing weight. When both tires of a gear are flat, special
maintenance handling/towing procedures will need to be employed, so as not to exceed the
capacity of the nose gear for towing.
SUPPLEMENTARY PROCEDURES
Landing Gear
Vol. 1 06−07−1
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
SUPPLEMENTARY PROCEDURES
Landing Gear
Vol. 1 06−07−2
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
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1. FLIGHT MANAGEMENT SYSTEM
NOTE
FMS normal procedures are contained in the FMS–6000 Pilot’s Guide.
A. Prior to FMS Use
(1) FMS position information......................................Check for accuracy.
On airplanes 5500 and subsequent and airplanes incorporating Canadair 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 one 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.
SUPPLEMENTARY PROCEDURES
Navigation Systems
Vol. 1 06−08−1
REV 77, Oct 20/09
CL−604 Operating Manual
PSP 604−6
1. FLIGHT MANAGEMENT SYSTEM (CONT'D)
B. Prior to Overwater Operations
On airplanes 5301 to 5386 not incorporating Canadair 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.
C. After Periods of Dead Reckoning (DR) Navigation
(1) FMS position information......................................Check for accuracy.
2. INERTIAL REFERENCE SYSTEM
For the system description and operation of the inertial reference system, refer to the Operating
Manual, Volume 2 – FLIGHT INSTRUMENTS.
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.
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庞巴迪挑战者604操作手册 Operating Manual 2(47)
