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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 8.8 %.
PERFORMANCE
Approach and Landing Climb
06−06−6
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
3. APPROACH CLIMB GRADIENT (CONT'D)
FAA Certified Airplanes
DFM0606_003 appr_acu_and_off_faa_ha.u
Approach Climb Gradient, Flaps 20° − Anti-Icing Off
Figure 06−06−2
PERFORMANCE
Approach and Landing Climb
06−06−7
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
3. APPROACH CLIMB GRADIENT (CONT'D)
B. Approach Climb Gradient, Flaps 20° – Anti-Icing On
The approach climb gradient for varying conditions, for an approach with flaps at 20° with the
wing and/or cowl anti-icing on, is provided by Figure 06−06−3.
NOTE
If ice accumulation is suspected on unprotected surfaces, then reduce the
approach climb gradient values derived from Figure 06−06−3 by 0.8%.
Example:
Associated Conditions:
Airport pressure altitude = 4,000 feet
Temperature = –8°C
Cowl Anti-Icing = On
10th Stage Bleeds = Closed
Airplane weight = 15,000 kg (33,069 lb)
The example in Figure 06−06−3 shows that for the above associated conditions, the
approach climb gradient for an approach with flaps at 20° is 10.3%.
PERFORMANCE
Approach and Landing Climb
06−06−8
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
3. APPROACH CLIMB GRADIENT (CONT'D)
DFM0606_004 app_anti_ice_405_ha.uni
PERFORMANCE
Approach and Landing Climb
06−06−9
REV 66, Feb 01/07
Approach Climb Gradient, Flaps 20° − Anti-Icing On
Figure 06−06−3
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 wing and/or cowl anti-icing on, is provided by Figure 06−06−3.
NOTE
If ice accumulation is suspected on unprotected surfaces, then reduce
the approach climb gradient values derived from Figure 06−06−3
by 0.8%.
Example:
Associated Conditions:
Airport pressure altitude = 4,000 feet
Temperature = –8°C
Cowl Anti-Icing = On
10th Stage Bleeds = Closed
Airplane weight = 15,000 kg (33,069 lb)
The example in Figure 06−06−3 shows that for the above associated conditions, the
approach climb gradient for an approach with flaps at 20° is 9.2 %.
PERFORMANCE
Approach and Landing Climb
06−06−10
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
3. APPROACH CLIMB GRADIENT (CONT'D)
FAA Certified Airplanes
DFM0606_005 appr_anti_ice_faa_ha.uni
Approach Climb Gradient, Flaps 20° − Anti-Icing On
Figure 06−06−3
PERFORMANCE
Approach and Landing Climb
06−06−11
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
4. LANDING CLIMB SPEED
A. Landing Climb Speed, Flaps 45°
The landing climb speed for varying conditions of airplane weight and airport pressure
altitude, for a landing with flaps at 45°, is provided by Figure 06−06−4.
Example:
Associated Conditions:
Airplane weight = 18,000 kg (39,683 lb)
Airport pressure altitude = 4,000 feet
The example in Figure 06−06−4 shows that for the above associated conditions, the landing
climb speed for a landing with flaps at 45° is 138.5 KIAS.
PERFORMANCE
Approach and Landing Climb
06−06−12
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
4. LANDING CLIMB SPEED (CONT'D)
DFM0606_006 ldg_speed_ha.uni
PERFORMANCE
Approach and Landing Climb
06−06−13
REV 66, Feb 01/07
Landing Climb Speed, Flaps 45°
Figure 06−06−4
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
5. LANDING CLIMB GRADIENT
A. Landing Climb Gradient, Flaps 45° – Anti-Icing Off
The landing climb gradient for varying conditions, for a landing with flaps at 45° with the
　
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