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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
PSP 604–5, and any damage rectified before the next take-off.
15/05/95
CL-604 Airplane Flight Manual
PSP 604–1
DOT Approved
REV 46, Mar 28/02
LIMITATIONS
Systems Limitations
02–08–4
10. TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS)
On airplanes incorporating Canadair Service Bulletin 604–34–001 or 604–34–017:

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.

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.
On airplanes incorporating Canadair Service Bulletin 604–34–001 Rev 1,
604–34–017 Rev 1 or 604–34–027:

The TCAS installation is 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.

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.
15/05/95
CL-604 Airplane Flight Manual
PSP 604–1
DOT Approved
REV 46, Mar 28/02
LIMITATIONS
Systems Limitations
02–08–4
10. TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS)
On airplanes incorporating Canadair Service Bulletin 604–34–001 or 604–34–017:

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. 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.
On airplanes incorporating Canadair Service Bulletin 604–34–001 Rev 1,
604–34–017 Rev 1 or 604–34–027:

The TCAS installation is 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. 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.
15/05/95
CL-604 Airplane Flight Manual
PSP 604–1
DOT Approved AR
REV 53, Jun 04/04
LIMITATIONS
Navigation Systems Limitations
02−09−1
1. FLIGHT MANAGEMENT SYSTEM

The flight management system (FMS) must be operated in accordance with the latest
　
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