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Fuel Additives 02−05−13
Anti-icing 02−05−13
Biocide 02−05−13
Anti-static 02−05−13
Corrosion inhibitor 02−05−13
Fuel Transfer 02−05−14
Fuel Jettison 02−05−15
Oil Grades 02−05−15
Oil Consumption 02−05−15
Oil Replenishment System 02−05−15
Auxiliary Power Unit 02−05−15
Type 02−05−15
Maximum RPM 02−05−15
Maximum EGT 02−05−15
Starting 02−05−16
APU Bleed Air 02−05−17
APU Generator 02−05−17
APU Indications 02−05−18
LIMITATIONS
Table of Contents
02−00−2
REV 77, Oct 20/09
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
Page
OPERATING SPEEDS
Maximum Operating Speed and Mach Number 02−06−1
RVSM Maximum Operating Speed 02−06−1
Design Maneuvering Speed 02−06−2
Flaps Extended Speed 02−06−3
Maximum Landing Gear Operating Speed 02−06−3
Maximum Landing Gear Extended Speed 02−06−3
Tire Limit Speed 02−06−3
Maximum Airspeed for ADG Operation 02−06−3
Turbulence Penetration Speed 02−06−3
Minimum Operating Limit Speed 02−06−3
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 02−08−1
Permissible Loads on AC System 02−08−1
Permissible Loads on DC Systems 02−08−1
Circuit Breaker Reset (In Flight) 02−08−1
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 02−08−2
Taxi Lights 02−08−2
Wheel Brake Cooling Limitations 02−08−2
Traffic Alert And Collision Avoidance System (TCAS) 02−08−3
Configuration Deviation List 02−08−3
Electrical/Avionics Equipment 02−08−3
LIMITATIONS
Table of Contents
02−00−3
REV 77, Oct 20/09
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
Page
NAVIGATION SYSTEMS LIMITATIONS
Flight Management System 02−09−1
Navigation Operational Approvals 02−09−5
Enhanced Ground Proximity Warning System (GPWS) 02−09−8
Airborne Flight Information System (AFIS) 02−09−8
LIST OF ILLUSTRATIONS
CENTRE OF GRAVITY
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 Service Bulletin
604−28−007 and airplanes 5301 to 5571 NOT
incorporating Service Bulletin 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 Service Bulletin
604−28−007 and airplanes 5301 to 5571 NOT
incorporating Service Bulletin 604−27−009 or
604−27−012 02−03−4
OPERATING LIMITATIONS
Figure 02−04−1 Altitude and Temperature Operating Limits 02−04−1
POWER PLANT
Figure 02−05−1 Engine Air Start Envelope (In Flight) 02−05−4
Figure 02−05−2 Auxiliary Tank Quantity/Tail Tank Quantity − Relation
Verses Centre of Gravity 02−05−6
Figure 02−05−3 Minimum Wing Tank Fuel Quantity for Take-Off 02−05−9
Figure 02−05−4 Minimum Wing Tank Fuel Quantity for Take-Off
(Airplanes 5301,
5303 to 5639 NOT incorporating Service Bulletin
604–11–001) 02−05−10
Figure 02−05−5 Manual Fuel Transfer − Auxiliary Tank Quantity vs Tail
Tank Quantity 02−05−14
Figure 02−05−6 APU In-Flight Envelope 02−05−19
Figure 02−05−7 APU In−Flight Envelope
(Airplanes 5301 to 5630 NOT incorporating
SB 604−49−006 or 604−49−009) 02−05−20
　
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