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PSP 604−6
5. NORMAL PROCEDURES (CONT'D)
Figure 06−20−7 provides the stick pusher speeds for flaps 30° and gear up; and
Figure 06−20−8 provides the stick pusher speeds for flaps 45° and gear down.
The stick shaker and stick pusher speeds were calculated based on a reference centre of
gravity (CG) position of 20% MAC. To estimate stick shaker and stick pusher speeds at a
different CG position, reduce the speeds derived from the following tables by 0.1% for every
1.0% MAC aft of the reference CG position.
Example:
Airplane weight = 38,000 lb
Altitude = 14,000 feet
Flaps = 20°
Landing gear = Up
CG = 21% MAC
Using Figure 06−20−2, the estimated stick shaker speed for the above conditions is
calculated as follows:
134.5 – (134.5 × .001) = 134.4 KIAS
Using Figure 06−20−6, the estimated stick pusher speed for the above conditions is
calculated as follows:
126.0 – (126.0 × .001) = 125.9 KIAS
SUPPLEMENTARY PROCEDURES
Airworthiness Flight Test/Crew Training
Vol. 1 06−20−3
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
5. NORMAL PROCEDURES (CONT'D)
SUPPLEMENTARY PROCEDURES
Airworthiness Flight Test/Crew Training
Vol. 1 06−20−4
REV 66, Feb 01/07
Stick Shaker Speed (KIAS) − Flaps 0°, Landing Gear Up
Figure 06−20−1
CL−604 Operating Manual
PSP 604−6
5. NORMAL PROCEDURES (CONT'D)
SUPPLEMENTARY PROCEDURES
Airworthiness Flight Test/Crew Training
Vol. 1 06−20−5
REV 66, Feb 01/07
Stick Shaker Speed (KIAS) − Flaps 20°, Landing Gear Up
Figure 06−20−2
CL−604 Operating Manual
PSP 604−6
5. NORMAL PROCEDURES (CONT'D)
SUPPLEMENTARY PROCEDURES
Airworthiness Flight Test/Crew Training
Vol. 1 06−20−6
REV 66, Feb 01/07
Stick Shaker Speed (KIAS) − Flaps 30°, Landing Gear Up
Figure 06−20−3
CL−604 Operating Manual
PSP 604−6
5. NORMAL PROCEDURES (CONT'D)
SUPPLEMENTARY PROCEDURES
Airworthiness Flight Test/Crew Training
Vol. 1 06−20−7
REV 66, Feb 01/07
Stick Shaker Speed (KIAS) − Flaps 45°, Landing Gear Down
Figure 06−20−4
CL−604 Operating Manual
PSP 604−6
5. NORMAL PROCEDURES (CONT'D)
SUPPLEMENTARY PROCEDURES
Airworthiness Flight Test/Crew Training
Vol. 1 06−20−8
REV 66, Feb 01/07
Stick Pusher Speed (KIAS) − Flaps 0°, Landing Gear Up
Figure 06−20−5
CL−604 Operating Manual
PSP 604−6
5. NORMAL PROCEDURES (CONT'D)
SUPPLEMENTARY PROCEDURES
Airworthiness Flight Test/Crew Training
Vol. 1 06−20−9
REV 66, Feb 01/07
Stick Pusher Speed (KIAS) − Flaps 20°, Landing Gear Up
Figure 06−20−6
CL−604 Operating Manual
PSP 604−6
5. NORMAL PROCEDURES (CONT'D)
SUPPLEMENTARY PROCEDURES
Airworthiness Flight Test/Crew Training
Vol. 1 06−20−10
REV 66, Feb 01/07
Stick Pusher Speed (KIAS) − Flaps 30°, Landing Gear Up
Figure 06−20−7
CL−604 Operating Manual
PSP 604−6
5. NORMAL PROCEDURES (CONT'D)
SUPPLEMENTARY PROCEDURES
Airworthiness Flight Test/Crew Training
Vol. 1 06−20−11
REV 66, Feb 01/07
Stick Pusher Speed (KIAS) − Flaps 45°, Landing Gear Down
Figure 06−20−8
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 06−20−9, is 1,040 feet per minute.
SUPPLEMENTARY PROCEDURES
Airworthiness Flight Test/Crew Training
Vol. 1 06−20−12
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
　
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