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DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
5. NORMAL PROCEDURES (CONT'D)
SUPPLEMENT 5A
Airworthiness Flight Test/Crew Training
07−05A−01−6
REV 66, Feb 01/07
Stick Shaker Speed (KIAS) − Flaps 30°, Landing Gear Up
Figure 07−05A−3
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
5. NORMAL PROCEDURES (CONT'D)
SUPPLEMENT 5A
Airworthiness Flight Test/Crew Training
07−05A−01−7
REV 66, Feb 01/07
Stick Shaker Speed (KIAS) − Flaps 45°, Landing Gear Down
Figure 07−05A−4
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
5. NORMAL PROCEDURES (CONT'D)
SUPPLEMENT 5A
Airworthiness Flight Test/Crew Training
07−05A−01−8
REV 66, Feb 01/07
Stick Pusher Speed (KIAS) − Flaps 0°, Landing Gear Up
Figure 07−05A−5
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
5. NORMAL PROCEDURES (CONT'D)
SUPPLEMENT 5A
Airworthiness Flight Test/Crew Training
07−05A−01−9
REV 66, Feb 01/07
Stick Pusher Speed (KIAS) − Flaps 20°, Landing Gear Up
Figure 07−05A−6
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
5. NORMAL PROCEDURES (CONT'D)
SUPPLEMENT 5A
Airworthiness Flight Test/Crew Training
07−05A−01−10
REV 66, Feb 01/07
Stick Pusher Speed (KIAS) − Flaps 30°, Landing Gear Up
Figure 07−05A−7
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
5. NORMAL PROCEDURES (CONT'D)
SUPPLEMENT 5A
Airworthiness Flight Test/Crew Training
07−05A−01−11
REV 66, Feb 01/07
Stick Pusher Speed (KIAS) − Flaps 45°, Landing Gear Down
Figure 07−05A−8
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
5. NORMAL PROCEDURES (CONT'D)
C. Gross Climb Performance
The gross climb performance data are presented in the following charts:
Figure 07−05A−9 provides the gross climb performance in the take-off configuration;
Figure 07−05A−10 provides the gross climb performance in the final take-off/enroute
configuration.
(1) GROSS CLIMB PERFORMANCE IN TAKE-OFF CONFIGURATION
The gross climb performance in the take-off configuration presented in Figure 07−05A−9
is based on the following:
• Flaps = 20°
• Landing gear = Up
• Climb airspeed = V2
• Engines = One engine at normal take-off thrust (zero bleed) and
other engine at IDLE
Example:
Associated Conditions:
Airplane weight = 41,888 lb (19,000 kg)
Altitude = Sea Level
Temperature = 10°C
The gross rate of climb during the second segment, for the above associated conditions
as shown in Figure 07−05A−9 is 1,040 feet per minute.
SUPPLEMENT 5A
Airworthiness Flight Test/Crew Training
07−05A−01−12
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
5. NORMAL PROCEDURES (CONT'D)
DFM0705_001
SUPPLEMENT 5A
Airworthiness Flight Test/Crew Training
07−05A−01−13
REV 66, Feb 01/07
Take-Off Gross Rate of Climb − Flaps 20°, Landing Gear Up
Figure 07−05A−9
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
5. NORMAL PROCEDURES (CONT'D)
(2) GROSS CLIMB PERFORMANCE IN FINAL TAKE-OFF/ENROUTE CONFIGURATION
The gross climb performance in the final take-off/enroute configuration presented in
Figure 07−05A−10 is based on the following:
• Flaps = 0°
• Landing gear = Up
• Climb airspeed = Final take-off/enroute
• Engines = One engine at MCT (ACU on) and other engine
inoperative
Example:
Associated Conditions:
Airplane weight = 41,888 lb (19,000 kg)
Altitude = 5,000 feet
Temperature = 10°C
The gross rate of climb during the final take−off segment, for the above associated
conditions as shown in Figure 07−05A−10 is 1,180 feet per minute.
SUPPLEMENT 5A
Airworthiness Flight Test/Crew Training
07−05A−01−14
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
5. NORMAL PROCEDURES (CONT'D)
DFM0705_002
SUPPLEMENT 5A
Airworthiness Flight Test/Crew Training
07−05A−01−15
　
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