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REV 66, Feb 01/07
Final Take-Off/Enroute Gross Rate of Climb − Flaps 0°, Landing Gear Up
Figure 07−05A−10
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
6. ABNORMAL PROCEDURES
The abnormal procedures in Chapter 5 are applicable.
7. PERFORMANCE
The performance data in Chapter 6 is applicable.
SUPPLEMENT 5A
Airworthiness Flight Test/Crew Training
07−05A−01−16
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
GENERAL 07−06−01−1
INTRODUCTION 07−06−01−1
LIMITATIONS 07−06−01−1
EMERGENCY PROCEDURES 07−06−01−1
NORMAL PROCEDURES 07−06−01−1
ABNORMAL PROCEDURES 07−06−01−1
PERFORMANCE 07−06−01−2
Take-Off Performance 07−06−01−2
Weight Altitude Temperature Limits 07−06−01−2
Climb Gradients and Climb Speeds 07−06−01−2
SUPPLEMENT 6
Flight With Landing Gear Down
07−06−00−1
REV 66, Feb 01/07
07−06−00−1
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
TABLE OF CONTENTS
Page
TABLE OF CONTENTS
SUPPLEMENT 6
Flight With Landing Gear Down
07−06−00−2
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
THIS PAGE INTENTIONALLY LEFT BLANK
1. GENERAL
The data in this Supplement must be used when operating the airplane with fixed landing gear
down.
These data complement or supersede data contained in the basic Airplane Flight Manual. This
Supplement must therefore be used in conjunction with the basic Airplane Flight Manual.
The effect of this Supplement on the basic Airplane Flight Manual is given in paragraphs
(2) to (7).
This supplement is applicable only when used in conjunction with a Minimum Equipment List
approved by the appropriate authority.
2. INTRODUCTION
The general information in Chapter 1 is applicable.
3. LIMITATIONS
The limitations in Chapter 2 are applicable, except as modified by the following:
• Airspeed must not exceed VLE (250 KIAS).
• Flight altitude above 20,000 ft is prohibited.
• Flight in known or anticipated icing conditions is not permitted.
4. EMERGENCY PROCEDURES
The emergency procedures in Chapter 3 are applicable.
5. NORMAL PROCEDURES
The normal procedures in Chapter 4 are applicable.
6. ABNORMAL PROCEDURES
The abnormal procedures in Chapter 5 are applicable.
SUPPLEMENT 6
Flight With Landing Gear Down
07−06−01−1
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
7. PERFORMANCE
The performance data in Chapter 6 are applicable, except as modified by the following:
A. Take-Off Performance
The take-off speeds (V1, VR, and V2) must be increased by 2 knots. The field length limited
take-off weight must be reduced by 2%. For a given take-off weight, the take-off field length
must be increased by 4%. The take-off weight limited by tire speed must be reduced by 4%.
The take-off weight limited by maximum brake energy must be reduced by 2%.
B. Weight Altitude Temperature Limits
The following penalty must be applied to the performance data as a weight decrement:
FLIGHT SEGMENT WEIGHT DECREMENT (%)
Take-off – Flaps 20° 16%
Landing – Approach Flaps 20°
– Landing Flaps 45° 13%
The take-off weight is limited by the second segment climb gradient requirement (2.4% gross
gradient – one engine inoperative). In landing, the limiting requirement is the approach climb
gradient (2.1% gross gradient, one engine inoperative).
C. Climb Gradients and Climb Speeds
The following gradient penalty must be subtracted from the climb gradient data:
CLIMB GRADIENT GRADIENT PENALTY (%)
Obstacle Clearance Reference Climb Gradient (Flaps 20°) 2.4%
Final Segment / Enroute (Flaps 0°) 3.3%
Approach (Flaps 20°) 2.4%
Landing (Flaps 45°) Not applicable
The approach climb speed in the flaps 20° configuration must be increased by 2 knots.
SUPPLEMENT 6
Flight With Landing Gear Down
07−06−01−2
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
INTRODUCTION 07−07−01−1
GENERAL 07−07−01−1
LIMITATIONS 07−07−01−1
Navigation Procedures 07−07−01−1
　
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