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NOTE
If ice accumulation is suspected on unprotected surfaces, subtract
0.9 percent from the gradient derived from Figure 06−05−3.
Example:
Associated Conditions:
Temperature = –8°C
Cowl anti-icing = On
Pressure altitude = 5,000 ft
Gross weight = 15,000 kg (33,069 lb)
The example on Figure 06−05−3 shows that for the above associated conditions, the
following climb gradients are obtained:
• Gross final segment and
gross enroute climb gradients = 10.2%
• Net final segment climb gradient = 9.4%
• Net enroute climb gradient = 9.1%
PERFORMANCE
Enroute Performance
06−05−6
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
3. FINAL SEGMENT AND ENROUTE CLIMB GRADIENT (CONT'D)
DFM0605_003 enr_anti_ice_405.uni
PERFORMANCE
Enroute Performance
06−05−7
REV 66, Feb 01/07
Final Segment and Enroute Climb Gradient, Flaps 0° − Anti-Icing On
Figure 06−05−3
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
PERFORMANCE
Enroute Performance
06−05−8
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
THIS PAGE INTENTIONALLY LEFT BLANK
1. INTRODUCTION
The Approach and Landing Climb section contains the charts used to obtain the approach and
landing climb gradients and speed schedules for varying conditions of temperature, airport
pressure altitude, and airplane weight for the specified approach and landing configurations.
PERFORMANCE
Approach and Landing Climb
06−06−1
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
2. APPROACH CLIMB SPEED
A. Approach Climb Speed, Flaps 20°
The approach climb speed for varying conditions of airplane weight and airport pressure
altitude, for an approach with flaps at 20°, is provided by Figure 06−06−1.
Example:
Associated Conditions:
Airplane weight = 18,000 kg (39,683 lb)
Airport pressure altitude = 4,000 feet
The example in Figure 06−06−1 shows that for the above associated conditions, the
approach climb speed for an approach with flaps at 20° is 138.8 KIAS.
PERFORMANCE
Approach and Landing Climb
06−06−2
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
2. APPROACH CLIMB SPEED (CONT'D)
DFM0606_001 appr_speed_ha.uni
PERFORMANCE
Approach and Landing Climb
06−06−3
REV 66, Feb 01/07
Approach Climb Speed, Flaps 20°
Figure 06−06−1
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
3. APPROACH CLIMB GRADIENT
A. Approach Climb Gradient, Flaps 20° – Anti-Icing Off
The approach climb gradient for varying conditions, for an approach with flaps at 20° with the
anti-icing off, is provided by Figure 06−06−2.
NOTE
If ice accumulation is suspected on unprotected surfaces, then reduce the
approach climb gradient values derived from Figure 06−06−2 by 0.8%.
Example:
Associated Conditions:
Airport pressure altitude = 4,000 feet
Temperature = 27°C
Wing & Cowl Anti-Icing = Off
10th Stage Bleeds = Closed
Airplane weight = 15,000 kg (33,069 lb)
The example in Figure 06−06−2 shows that for the above associated conditions, the
approach climb gradient for an approach with flaps at 20° is 10%.
PERFORMANCE
Approach and Landing Climb
06−06−4
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
3. APPROACH CLIMB GRADIENT (CONT'D)
DFM0606_002 appr_acu_and_off_405_ha.u
PERFORMANCE
Approach and Landing Climb
06−06−5
REV 66, Feb 01/07
Approach Climb Gradient, Flaps 20° − Anti-Icing Off
Figure 06−06−2
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
3. APPROACH CLIMB GRADIENT (CONT'D)
FAA Certified Airplanes
The approach climb gradient for varying conditions, for an approach with flaps at 20° with
the anti-icing off, is provided by Figure 06−06−2.
NOTE
If ice accumulation is suspected on unprotected surfaces, then reduce
the approach climb gradient values derived from Figure 06−06−2
by 0.8%.
Example:
Associated Conditions:
Airport pressure altitude = 4,000 feet
Temperature = 27°C
　
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