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SB 604–33–001 Wing Landing/Taxi Light System, Installation of Pulsating Light System
SB 604–33–002 Standby Instrument Integral Lighting, Power Source Change
SB 604–34–001 Traffic Alert and Collision Avoidance System, Installation
SB 604–34–003 Ground Proximity Warning System, Installation
SB 604–34–007 Dual Global Positioning System, Installation
SB 604–34–012 Reduced Vertical Separation Minimum (RVSM), 1000 Ft. Aircraft
Qualification Requirements
SB 604–34–016 Ground Proximity Warning System, Installation on Aircraft with Provisions
SB 604–34–017 Traffic Alert and Collision Avoidance System, Installation on Aircraft with
Provisions
SB 604–34–018 Dual Global Positioning System, Installation on Aircraft with Provisions for
Dual GPS
SB 604–34–020 Ground Proximity Warning System, Introduction of Enhanced GPWS
SB 604–34–025 Enhanced Ground Proximity Warning System, Installation of EGPWS for
Aircraft with Full Provisions
SB 604–34–027 Traffic Alert and Collision Avoidance System, Change 7.0 Upgrade
SB 604–34–031 Engine Indicating and Crew Alerting System and Flight Management
System, Introduction of Basic PrecisionPlus Avionics Upgrade
SB 604–34–034 Flight Management System, Installation of Search Patterns
SB 604–34–035 Flight Management System, Introduction of New Vspeed Data Bases
SB 604–34–042 Flight Management Computing, Introduction of FMS Software Version 3.0.3
SB 604–34–050 Flight Management Computing, Introduction of FMS Software Version 3.3.1
INTRODUCTION
General
01−01−19
REV 77, Oct 20/09
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
7. SERVICE BULLETINS (CONT'D)
Service Bulletin Title
SB 604–34–055 Enhanced Ground Proximity Warning System, Introduction of Steep
Approach Push Button Annunciator
SB 604–49–006 Auxiliary Power Unit, Introduction of 36–150(CL) APU
SB 604–49–009 Auxiliary Power Unit, Activation of 36–150(CL) APU
SB 604–73–003 Fuel System, Russian Fuel Sampling Program
SB 604–76–001 Throttle Quadrant Assembly, Throttle Levers can Possibly Lock in the Idle
Position
INTRODUCTION
General
01−01−20
REV 77, Oct 20/09
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
INTRODUCTION
General 02−01−1
Kinds of Airplane Operation 02−01−1
STRUCTURAL WEIGHT
Structural Weight Limitation 02−02−1
CENTRE OF GRAVITY
Centre of Gravity Limits (MTOW 48,200 LB) 02−03−1
Centre of Gravity Limits (MTOW 47,600 LB) 02−03−3
OPERATING LIMITATIONS
Altitude and Temperature Operating Limit 02−04−1
Take-Off 02−04−2
Rotation Rate and Pitch Attitude 02−04−2
Pitch Trim 02−04−2
Take-Off Pitch Target 02−04−2
Cold Weather Operations 02−04−3
Operation in Icing Conditions 02−04−4
Cowl Anti-ice System 02−04−4
Wing Anti-ice System 02−04−5
Super-Cooled Large Droplet Icing 02−04−6
Enhanced Take-Off Procedures and Winter Operations Training 02−04−7
Runway Slopes 02−04−7
Tailwind Conditions 02−04−7
Approaches 02−04−7
Minimum Flight Crew 02−04−7
Maximum Occupants 02−04−7
Maximum Crosswind Component 02−04−8
POWER PLANT
Engines 02−05−1
LIMITATIONS
Table of Contents
02−00−1
REV 77, Oct 20/09
CHAPTER 2 - LIMITATIONS
02−00−1
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
TABLE OF CONTENTS
Page
TABLE OF CONTENTS
POWER PLANT
Engine Indications 02−05−1
Engine Operating Limits 02−05−2
Engine Operating Limits Table 02−05−2
Airplane Cold Soak 02−05−2
Oil Temperature 02−05−2
Oil Pressure 02−05−2
Continuous Engine Ignition 02−05−3
Automatic Performance Reserve (APR) 02−05−3
Starter Cranking Limits (Ground and Air) 02−05−3
Engine Start 02−05−3
Associated Conditions 02−05−3
Dry Motoring Cycle 02−05−3
Engine Relight 02−05−3
Fuel 02−05−5
Fuel Temperature 02−05−11
Fuel Grades 02−05−12
　
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