View source for CL650/Airplane Flight Manual Limitations

== V-Speeds ==
{| class="wikitable"
| rowspan="2" |V<sub>MO</sub>
|< 8,000 ft
|300 kias
|-
|8,000–22,150 ft
|348 kias
|-
|M<sub>MO</sub>
| colspan="2" |Mach 0.85 (0.83 in RVSM airspace)
|-
|V<sub>LE</sub> (gear extended)
| colspan="2" |250 kias 
|-
|V<sub>LO</sub> (gear operation)
| colspan="2" |197 kias
|-
| rowspan="3" |V<sub>FE</sub> (flaps extended)
|Flaps 20°
|231 kias
|-
|Flaps 30°
|197 kias
|-
|Flaps 45°
|189 kias
|}

== Approach, Take-off, and Landing ==
{| class="wikitable"
| rowspan="3" |Glidepath Angle Limit

''See “Special Approach Supplement”''
|Normal
|3.5°
|-
|Special Performance
|4.5°
|-
|Steep
|5.5°
|-
|Demonstrated Crosswind Component
| colspan="2" |24 kts
|-
|Maximum Tailwind Component
| colspan="2" |10 kts
|-
|Maximum Normal Runway Altitude
| colspan="2" |10,000 ft pressure altitude
|-
|Maximum Reduced Weight Runway Altitude
| colspan="2" |14,000 ft pressure altitude
|-
|Maximum Air Temperature for Take-off and Landing
| colspan="2" |ISA+35 °C
|-
|Minimum Air Temperature for Take-off
| colspan="2" |−40 °C / −40 °F
|-
|Maximum Runway Slope
| colspan="2" |2% uphill / 2% downhill
|-
|Minimum Autopilot Disconnect Height 
| colspan="2" |80 ft
|}

== Flight in Icing Conditions ==
{| class="wikitable"
|Engine Cowl Anti-Ice
| colspan="2" |In icing conditions (visible moisture, SAT ≥ −40 °C, TAT ≤ 10 °C)
|-
| rowspan="2" |Wing Anti-Ice

''See “Operations in Icing Conditions”''
|> 22,000 ft
|Ice detection indicated
|-
|< 22,000 ft
|Ice detection indicated

''OR''

In icing conditions

''OR''

TAT ≤ 10 °C & approach flaps extended
|}