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Automatic Performance Reserve (APR) 02−05−3
Starter Cranking Limits (Ground and Air) 02−05−4
Engine Start 02−05−4
Associated Conditions 02−05−4
Dry Motoring Cycle 02−05−4
15/05/95
CL-604 Airplane Flight Manual
PSP 604−1
DOT Approved
REV 61, Jun 29/06
AR
LIMITATIONS
Table of Contents
02−00−2
Page
POWER PLANT (CONT’D)
Engine Relight 02−05−4
Fuel 02−05−6
Fuel Temperature 02−05−8
Fuel Grades 02−05−8
Fuel Additives 02−05−9
Fuel Transfer 02−05−10
Fuel Jettison 02−05−11
Oil Grades 02−05−11
Oil Consumption 02−05−11
Oil Replenishment System 02−05−11
Auxiliary Power Unit 02−05−11
Type 02−05−11
Maximum RPM 02−05−11
Maximum EGT 02−05−11
Starting 02−05−12
APU Bleed Air 02−05−13
APU Generator 02−05−13
APU Indications 02−05−13
OPERATING SPEEDS
Maximum Operating Speed and Mach Number 02−06−1
RVSM Maximum Operating Speed 02−06−1
Design Maneuvering Speed 02−06−1
Flaps Extended Speed 02−06−1
Maximum Landing Gear Operating Speed 02−06−1
Maximum Landing Gear Extended Speed 02−06−1
Tire Limit Speed 02−06−4
Maximum Airspeed for ADG Operation 02−06−4
Turbulence Penetration Speed 02−06−4
Minimum Operating Limit Speed 02−06−4
15/05/95
CL-604 Airplane Flight Manual
PSP 604−1
DOT Approved
REV 57, Jul 19/05
LIMITATIONS
Table of Contents
02−00−3
Page
MANEUVERING LOADS
Maneuvering Limit Load Factors 02−07−1
Side Slip Maneuvers 02−07−1
SYSTEMS LIMITATIONS
Air-Conditioning and Pressurization 02−08−1
Automatic Flight Control System 02−08−1
Bleed Air Systems 02−08−1
Electrical Systems 02−08−2
A/C Generators 02−08−2
Permissible Loads on AC System 02−08−2
Permissible Loads on DC Systems 02−08−2
Flight Controls - Lift/Drag Devices 02−08−2
Flaps 02−08−2
Flight Spoilers 02−08−2
Stall Protection System 02−08−2
Thrust Reversers 02−08−3
Taxi Lights 02−08−3
Wheel Brake Cooling Limitations 02−08−3
Traffic Alert and Collision Avoidance System (TCAS) 02−08−4
Configuration Deviation List 02−08−4
Electrical / Avionics Equipment 02−08−4
NAVIGATION SYSTEMS LIMITATIONS
Flight Management System 02−09−1
Navigation Operational Approvals 02−09−5
Enhanced Ground Proximity Warning System (GPWS) 02−09−7
Airborne Flight Information System (AFIS) 02−09−7


CL-604 Airplane Flight Manual
PSP 604−1
DOT Approved
REV 58, Dec 05/05
LIMITATIONS
Table of Contents
02−00−4
LIST OF ILLUSTRATIONS
Page
Figure 02−03−1 Centre of Gravity Limits (MTOW 48,200 lb) 02−03−1
Figure 02−03−2 Centre of Gravity Limits (MTOW 48,200 lb)
Airplanes 5301 to 5547, 5549 and 5550 NOT incorporating
SB 604−28−007 and airplanes 5301 to 5571 NOT
incorporating SB 604−27−009 or 604−27−012 02−03−2
Figure 02−03−3 Centre of Gravity Limits (MTOW 47,600 lb) 02−03−3
Figure 02−03−4 Centre of Gravity Limits (MTOW 47,600 lb)
Airplanes 5301 to 5547, 5549 and 5550 NOT incorporating
SB 604−28−007 and airplanes 5301 to 5571 NOT
incorporating SB 604−27−009 or 604−27−012 02−03−4
Figure 02−04−1 Altitude and Temperature Operating Limits 02−04−1
Figure 02−05−1 Engine Air Start Envelope (In Flight) 02−05−5
Figure 02−05−2 Auxiliary Tank Quantity / Tail Tank Quantity −
Relation Versus Centre of Gravity 02−05−7
Figure 02−05−3 Manual Fuel Transfer -
Auxiliary Tank Quantity vs Tail Tank Quantity 02−05−10
Figure 02−05−4 APU In-Flight Envelope 02−05−14
Figure 02−05−5 APU In-Flight Envelope
Airplanes 5301 to 5630 NOT incorporating
SB 604−49−006 or 604−49−009 02−05−15
　
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