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SUPPLEMENT 11 − APPROACHES BELOW 4.5 DEGREES 07−11−01−1
SUPPLEMENTS
List of Supplements
07−00−01−1
REV 70, Jun 08/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
TABLE OF CONTENTS
PAGE
SUPPLEMENT 12 − STEEP APPROACHES UP TO 5.5 DEGREES 07−12−01−1
SUPPLEMENTS
List of Supplements
07−00−01−2
REV 70, Jun 08/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
INTRODUCTION 07−01−01−1
Introduction 07−01−01−1
Limitations 07−01−01−1
Emergency Procedures 07−01−01−1
Normal Procedures 07−01−01−1
Abnormal Procedures 07−01−01−1
Performance 07−01−01−1
CERTIFICATE AIRPLANE CONFIGURATION 07−01−01−1
Take-Off and Sideline Noise Levels 07−01−01−1
Approach Noise Levels 07−01−01−2
CERTIFICATE NOISE LEVELS 07−01−01−2
SUPPLEMENT 1
Noise Characteristics
07−01−00−1
REV 66, Feb 01/07
07−01−00−1
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
TABLE OF CONTENTS
Page
TABLE OF CONTENTS
SUPPLEMENT 1
Noise Characteristics
07−01−00−2
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
THIS PAGE INTENTIONALLY LEFT BLANK
1. INTRODUCTION
This supplement contains the noise characteristics data for the CL 600–2B16 airplane, which are
required to comply with the following:
• CAM Chapter 516,
• FAR 36 Amendment 36-20, and
• ICAO Annex 16, Chapter 3.
The effect of this Supplement on the basic Airplane Flight Manual is given below:
A. Introduction
The general information in Chapter 1 is applicable.
B. Limitations
The limitations in Chapter 2 are applicable.
C. Emergency Procedures
The emergency procedures in Chapter 3 are applicable.
D. Normal Procedures
The normal procedures in Chapter 4 are applicable.
E. Abnormal Procedures
The abnormal procedures in Chapter 5 are applicable.
F. Performance
The performance data in Chapter 6 are applicable.
2. CERTIFICATE AIRPLANE CONFIGURATION
Compliance has been demonstrated in the following configuration:
A. Take-Off and Sideline Noise Levels
Take-off and sideline noise levels were obtained in the following configuration:
• Maximum take-off weight 21,591 kg/47,600 lb, or
21,863 kg/48,200 lb.
• Climb speed V2 + 10 KIAS
• Flaps setting 20 degrees
• APU Off
• Air-Conditioning packs Off
• Wing and cowl anti-ice Off
• Normal take-off thrust (both engines
operating)
SUPPLEMENT 1
Noise Characteristics
07−01−01−1
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
2. CERTIFICATE AIRPLANE CONFIGURATION (CONT'D)
B. Approach Noise Levels
Landing approach noise levels were established as per the following configuration:
• Glideslope 3 degrees
• Landing gear Down
• Landing weight 17,237 kg/38,000 lb
• Approach speed VREF + 10 KIAS
• Flaps setting 45 degrees
• APU On
• Air-Conditioning packs Off
• Wing and cowl anti-icing Off
3. CERTIFICATE NOISE LEVELS
The demonstrated effective perceived noise levels (EPNdB), noise limits and margins of
compliance are as listed below:
21,591 KG/47,600 LB MTOW
Phase of Flight Actual Noise Level
in EPNdB
Maximum Allowable
Requirement (dB) Margin (dB)
Take-Off Flyover 80.9 89.0 –8.1
Sideline/Lateral 86.2 94.0 –7.8
Approach 90.3 98.0 –7.7
21,863 KG/48,200 LB MTOW
Phase of Flight Actual Noise Level
in EPNdB
Maximum Allowable
Requirement (dB) Margin (dB)
Take-Off Flyover 81.2 89.0 –7.8
Sideline/Lateral 86.2 94.0 –7.8
Approach 90.3 98.0 –7.7
No determination has been made such that the noise levels of this airplane are, or should be,
acceptable or unacceptable for operation at, into, or out of, any airport.
These noise level values are stated for reference conditions of standard atmospheric pressure at
sea level, 25°C (77°F) ambient temperature, 70% relative humidity, and zero wind.
SUPPLEMENT 1
Noise Characteristics
07−01−01−2
REV 66, Feb 01/07
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