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To ensure adequate maneuver margins, flight spoilers must not be extended in flight at
airspeeds below the recommended approach speed plus 10 KIAS (refer to Chapter 6;
PERFORMANCE – LANDING PERFORMANCE of the Airplane Flight Manual).
LIMITATIONS
Systems Limitations
Vol. 1 02−08−1
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
6. STALL PROTECTION SYSTEM
Both stall protection system pusher switches must remain on for all phases of flight.
The stall protection test indicator must only be used for stall protection system functional test
purposes.
The PFD normalized AOA indicator is advisory only, it does not replace the airspeed indicator as
primary speed instrument, and it does not replace the stick shaker as primary stall warning.
The PFD normalized AOA indicator shall not be used during take-off.
7. THRUST REVERSERS
Thrust reversers are approved for ground use only.
The thrust reversers are intended for use during full stop landings. Do not attempt a go-around
maneuver after deployment of the thrust reversers.
Backing the airplane with the use of reverse thrust is prohibited.
Take-off with any of the following thrust reverser icons or EICAS messages displayed is
prohibited:
• REV icon on N1 gauge,
• L (R) REV UNLOCKED caution message, and
• L (R) REV UNSAFE caution message.
During landing, application of maximum reverse thrust is not permitted at airspeeds below
60 KIAS. Below 60 KIAS, reverse thrust must be reduced to 60% N1 or less.
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 of the Airplane Flight Manual) 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–605 Airplane Maintenance Manual, and any damage rectified before the next take-off.
LIMITATIONS
Systems Limitations
Vol. 1 02−08−2
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
10. TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS)
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.
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.
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.
AR Certified Airplanes
13. AIRSPACE OPERATIONAL LIMITATIONS
The airplane can fly in the former USSR airspace only on routes covered by ATC ground
facilities using RBS mode. If the airplane is to fly in areas that are not completely covered by
VHF stations and if the interruptions between VHF covered zones exceeds one flight hour, two
HF radios must be installed on the airplane.
AR Certified Airplanes
14. LONG RANGE NAVIGATION ACCURACY
When airplanes, not equipped with GPS, operate on routes, having a width of ±5 kilometers,
not covered by VOR/DME, it is recommended that the airplane position be confirmed by ATC
after 1 hour 30 minutes.
When airplanes, not equipped with GPS, operate on routes, having a width of ±10 kilometers,
　
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