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4. FLIGHT CAPABILITIES (CONT'D)
DFM0601_009 vsr_afm_0_cas.uni
PERFORMANCE
General
06−01−19
REV 66, Feb 01/07
Reference Stall Speed − Flaps 0°/Landing Gear Up
Figure 06−01−9
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
4. FLIGHT CAPABILITIES (CONT'D)
B. Reference Stall Speed – Flaps 20°/Landing Gear Up
The reference stall speeds for a flaps 20° and landing gear up configuration at varying gross
weights and pressure altitude, are provided in Figure 06−01−10. This chart is based upon the
most forward take-off centre of gravity limit at flaps 20°. The speeds shown are valid only for
pressure altitudes at and below 15,000 feet.
Example:
Gross weight = 19,500 kg (42,990 lb)
Flaps setting = 20°
Landing gear = Up
Pressure altitude = 6,000 feet
Reference stall speed = 126.6 KCAS
PERFORMANCE
General
06−01−20
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
4. FLIGHT CAPABILITIES (CONT'D)
DFM0601_010 vsr_afm_20_cas.uni
PERFORMANCE
General
06−01−21
REV 66, Feb 01/07
Reference Stall Speed − Flaps 20°/Landing Gear Up
Figure 06−01−10
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
4. FLIGHT CAPABILITIES (CONT'D)
C. Reference Stall Speed – Flaps 30°/Landing Gear Up
The reference stall speeds for a flaps 30° and landing gear up configuration at varying gross
weights and pressure altitude, are provided in Figure 06−01−11. This chart is based upon the
most forward centre of gravity limit at flaps 30°. The speeds shown are valid only for pressure
altitudes at and below 15,000 feet.
Example:
Gross weight = 19,500 kg (42,990 lb)
Flaps setting = 30°
Landing gear = Up
Pressure altitude = 6,000 feet
Reference stall speed = 121.4 KCAS
PERFORMANCE
General
06−01−22
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
4. FLIGHT CAPABILITIES (CONT'D)
DFM0601_011 vsr_afm_00_cas.uni
PERFORMANCE
General
06−01−23
REV 66, Feb 01/07
Reference Stall Speed − Flaps 30°/Landing Gear Up
Figure 06−01−11
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
4. FLIGHT CAPABILITIES (CONT'D)
D. Reference Stall Speed – Flaps 45°/Landing Gear Down
The reference stall speeds for a flaps 45° and landing gear down configuration at varying
gross weights and pressure altitude, are provided in Figure 06−01−12. This chart is based
upon the most forward centre of gravity limit at flaps 45°. The speeds shown are valid only for
pressure altitudes at and below 15,000 feet.
Example:
Gross weight = 19,500 kg (42,990 lb)
Flaps setting = 45°
Landing gear = Down
Pressure altitude = 6,000 feet
Reference stall speed = 116.9 KCAS
PERFORMANCE
General
06−01−24
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
4. FLIGHT CAPABILITIES (CONT'D)
DFM0601_012 vsr_afm_45_cas.uni
PERFORMANCE
General
06−01−25
REV 66, Feb 01/07
Reference Stall Speed − Flaps 45°/Landing Gear Down
Figure 06−01−12
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
4. FLIGHT CAPABILITIES (CONT'D)
E. Maneuvering Capabilities
The maneuvering capabilities are shown in Figure 06−01−13. The chart shows the maneuver
margin (bank angle and/or g-load factor) for a given weight, C.G., altitude and speed
combination. Alternatively, for a 1.0 g load factor, the chart shows the altitude and speed
margins for a given weight, C.G., and speed combination.
Maneuvering capability is defined relative to buffet onset or stick shaker activation, whichever
occurs first.
Example:
Associated conditions:
Airplane gross weight = 20,412 kg (45,000 lb)
Centre of Gravity (C.G.) = 30% MAC
Indicated Mach No. = 0.74
Pressure altitude = 39,000 feet
Example A in Figure 06−01−13, for the associated conditions mentioned above (enter the
chart from the indicated mach number scale), shows that the maneuvering capability is
equal to 1.3 g or a bank angle of 40°.
Example B in Figure 06−01−13, for the associated conditions mentioned above (enter the
chart from the gross weight scale), shows the altitude and speed margins before buffet or
　
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