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Airworthiness Flight Test/Crew Training
Vol. 1 06−20A−6
REV 66, Feb 01/07
Stick Shaker Speed (KIAS) − Flaps 30°, Landing Gear Up
Figure 06−20A−3
CL−604 Operating Manual
PSP 604−6
5. NORMAL PROCEDURES (CONT'D)
SUPPLEMENTARY PROCEDURES
Airworthiness Flight Test/Crew Training
Vol. 1 06−20A−7
REV 66, Feb 01/07
Stick Shaker Speed (KIAS) − Flaps 45°, Landing Gear Down
Figure 06−20A−4
CL−604 Operating Manual
PSP 604−6
5. NORMAL PROCEDURES (CONT'D)
SUPPLEMENTARY PROCEDURES
Airworthiness Flight Test/Crew Training
Vol. 1 06−20A−8
REV 66, Feb 01/07
Stick Pusher Speed (KIAS) − Flaps 0°, Landing Gear Up
Figure 06−20A−5
CL−604 Operating Manual
PSP 604−6
5. NORMAL PROCEDURES (CONT'D)
SUPPLEMENTARY PROCEDURES
Airworthiness Flight Test/Crew Training
Vol. 1 06−20A−9
REV 66, Feb 01/07
Stick Pusher Speed (KIAS) − Flaps 20°, Landing Gear Up
Figure 06−20A−6
CL−604 Operating Manual
PSP 604−6
5. NORMAL PROCEDURES (CONT'D)
SUPPLEMENTARY PROCEDURES
Airworthiness Flight Test/Crew Training
Vol. 1 06−20A−10
REV 66, Feb 01/07
Stick Pusher Speed (KIAS) − Flaps 30°, Landing Gear Up
Figure 06−20A−7
CL−604 Operating Manual
PSP 604−6
5. NORMAL PROCEDURES (CONT'D)
SUPPLEMENTARY PROCEDURES
Airworthiness Flight Test/Crew Training
Vol. 1 06−20A−11
REV 66, Feb 01/07
Stick Pusher Speed (KIAS) − Flaps 45°, Landing Gear Down
Figure 06−20A−8
CL−604 Operating Manual
PSP 604−6
5. NORMAL PROCEDURES (CONT'D)
C. Gross Climb Performance
The gross climb performance data are presented in the take-off configuration, and in the final
take-off/enroute configuration.
GROSS CLIMB PERFORMANCE IN TAKE-OFF CONFIGURATION
The gross climb performance in the take-off configuration presented 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 06−20A−9, is 1,040 feet per minute.
SUPPLEMENTARY PROCEDURES
Airworthiness Flight Test/Crew Training
Vol. 1 06−20A−12
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
5. NORMAL PROCEDURES (CONT'D)
DFM0705_001
SUPPLEMENTARY PROCEDURES
Airworthiness Flight Test/Crew Training
Vol. 1 06−20A−13
REV 66, Feb 01/07
Take-Off Gross Rate of Climb − Flaps 20°, Landing Gear Up
Figure 06−20A−9
CL−604 Operating Manual
PSP 604−6
5. NORMAL PROCEDURES (CONT'D)
GROSS CLIMB PERFORMANCE IN FINAL TAKE-OFF/ENROUTE CONFIGURATION
The gross climb performance in the final take-off/enroute configuration presented 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 06−20A−10, is 1,180 feet per minute.
SUPPLEMENTARY PROCEDURES
Airworthiness Flight Test/Crew Training
Vol. 1 06−20A−14
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
5. NORMAL PROCEDURES (CONT'D)
DFM0705_002
SUPPLEMENTARY PROCEDURES
Airworthiness Flight Test/Crew Training
Vol. 1 06−20A−15
REV 66, Feb 01/07
Final Take-Off/Enroute Gross Rate of Climb − Flaps 0°, Landing Gear Up
Figure 06−20A−10
CL−604 Operating Manual
PSP 604−6
6. ABNORMAL PROCEDURES
The abnormal procedures in Chapter 5 are applicable.
7. PERFORMANCE
The performance in Chapter 6 of the Airplane Flight Manual is applicable.
SUPPLEMENTARY PROCEDURES
Airworthiness Flight Test/Crew Training
Vol. 1 06−20A−16
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
　
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