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The maximum demonstrated crosswind component approved for use of reverse thrust is 24 knots
[at 33 feet (10 meters) tower height]. This value was demonstrated on a dry runway, and is
considered limiting.
8. TAXI LIGHTS
The taxi lights must be selected off whenever the airplane is stationary in excess of 10 minutes.
9. WHEEL BRAKE COOLING LIMITATIONS
Brake cooling times (established in accordance with the procedures in Chapter 6;
PERFORMANCE – TURN-AROUND TIME) must be observed between a landing or a low-energy
rejected take-off (RTO) and a subsequent take-off, to ensure that sufficient brake energy is
available to bring the airplane to a complete stop, if the subsequent take-off is rejected.
If a fusible plug releases, the wheels, brakes and tires and the anti-skid speed sensors must be
inspected in accordance with the procedure in the time limits/maintenance checks, provided in
the CL–604 Airplane Maintenance Manual, and any damage rectified before the next take-off.
LIMITATIONS
Systems Limitations
02−08−2
REV 68, Apr 16/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
10. TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS)
The TCAS installation is in accordance with JAA TGL No. 8.
On airplanes NOT incorporating Service Bulletin 604–34–001 Rev 1, 604–34–017 Rev 1 or
604–34–027:
The TCAS installation is NOT in accordance with JAA TGL No. 8.
Pilots are authorized to deviate from their Air Traffic Control (ATC) clearance in order to comply
with a TCAS resolution advisory (RA) command.
AR Certified Airplanes
Pilots are authorized to deviate from their Air Traffic Control (ATC) clearance in order to comply
with a TCAS resolution advisory (RA) command. The pilots shall inform ATC of the deviation
from the ATC clearance following the response to the RA.
Maneuvers must not be based solely on information presented on the traffic display.
The transponder has been demonstrated only for the purposes of surveillance modes A (Identity),
C (Altitude) and TCAS functions.
11. CONFIGURATION DEVIATION LIST
If the aircraft is to be operated with certain secondary airframe and/or any nacelle parts missing,
operation must be in accordance with the limitations specified in the basic Airplane Flight Manual,
and as amended by the Configuration Deviation List (Appendix 1).
12. ELECTRICAL/AVIONICS EQUIPMENT
During ground operation at ambient temperatures above 40°C (104°F), operation of
electrical/avionics equipment must be limited to 30 minutes, unless at least one air conditioning
pack is operating and the passenger door is closed.
LIMITATIONS
Systems Limitations
02−08−3
REV 68, Apr 16/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
LIMITATIONS
Systems Limitations
02−08−4
REV 68, Apr 16/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
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1. FLIGHT MANAGEMENT SYSTEM
The flight management system (FMS) must be operated in accordance with the latest edition of
the following:
• Airplane Flight Manual, and
• Flight Management System FMS–6000 Pilot’s Guide, part number 523–0808879–001117, or
later applicable revision.
On airplanes 5301 to 5665 NOT incorporating Service Bulletin 604–34–050 and on
airplanes 5301 to 5499 incorporating Service Bulletin 604–34–031:
• Flight Management System FMS–6000 Pilot’s Guide, part number 523–0780609–001117,
dated 04–01–01 or later applicable revision.
On airplanes 5301 to 5499 NOT incorporating Service Bulletin 604–34–031:
• Flight Management System FMS–6000 Pilot’s Guide, part number 523–0777833–004117,
dated 08–14–95 or later applicable revision.
The FMS is approved for use only with the following software program version or later applicable
revision:
WITHOUT SB 604–34–034 WITH SB 604–34–034
WITH SB 604–34–050 SCID 832–4117–094 SCID 832–4117–095
WITH SB 604–34–042 SCID 832–4117–074 SCID 832–4117–075
WITHOUT SB 604–34–042 SCID 832–4117–033 SCID 832–4117–034
On airplanes 5301 to 5499 NOT incorporating Service Bulletin 604–34–031:
The FMS is approved for use only with software program version SCID 829–7739–008 or later
applicable revision.
FMS database information must be verified as being current. Waypoints must be checked for
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庞巴迪挑战者604飞机飞行手册CL604 Airplane Flight Manual 1(55)
