CL650/Operations Reference/Limitations: Difference between revisions
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== Speeds == | == V-Speeds == | ||
{| class="wikitable" | {| class="wikitable" | ||
| rowspan="2" |V<sub>MO</sub> | | rowspan="2" |V<sub>MO</sub> | ||
| Line 9: | Line 9: | ||
|- | |- | ||
|M<sub>MO</sub> | |M<sub>MO</sub> | ||
| colspan="2" |Mach 0.85 (0.83 in RVSM airspace) | | colspan="2" |Mach 0.85 (0.83 in [[wikipedia:Reduced_vertical_separation_minima|RVSM]] airspace) | ||
|- | |- | ||
|V<sub>LE</sub> (gear extended) | |V<sub>LE</sub> (gear extended) | ||
| Line 32: | Line 32: | ||
| rowspan="3" |Glidepath Angle Limit | | rowspan="3" |Glidepath Angle Limit | ||
''See | ''See [[CL650/Operations Reference/Special Approach|Special Approach]]'' | ||
|Normal | |Normal | ||
|3.5° | |3.5° | ||
| Line 74: | Line 74: | ||
| rowspan="2" |Wing Anti-Ice | | rowspan="2" |Wing Anti-Ice | ||
''See | ''See [[CL650/Operations Reference/Operations in Icing Conditions|Operations in Icing Conditions]]'' | ||
|> 22,000 ft | |> 22,000 ft | ||
|Ice detection indicated | |Ice detection indicated | ||
| Line 87: | Line 87: | ||
''OR'' | ''OR'' | ||
TAT ≤ 10 °C & | TAT ≤ 10 °C & approach flaps extended | ||
approach flaps extended | |||
|} | |} | ||
Latest revision as of 12:17, 17 May 2025
V-Speeds
| VMO | < 8,000 ft | 300 kias |
| 8,000–22,150 ft | 348 kias | |
| MMO | Mach 0.85 (0.83 in RVSM airspace) | |
| VLE (gear extended) | 250 kias | |
| VLO (gear operation) | 197 kias | |
| VFE (flaps extended) | Flaps 20° | 231 kias |
| Flaps 30° | 197 kias | |
| Flaps 45° | 189 kias | |
Approach, Take-off, and Landing
| Glidepath Angle Limit
See Special Approach |
Normal | 3.5° |
| Special Performance | 4.5° | |
| Steep | 5.5° | |
| Demonstrated Crosswind Component | 24 kts | |
| Maximum Tailwind Component | 10 kts | |
| Maximum Normal Runway Altitude | 10,000 ft pressure altitude | |
| Maximum Reduced Weight Runway Altitude | 14,000 ft pressure altitude | |
| Maximum Air Temperature for Take-off and Landing | ISA+35 °C | |
| Minimum Air Temperature for Take-off | −40 °C / −40 °F | |
| Maximum Runway Slope | 2% uphill / 2% downhill | |
| Minimum Autopilot Disconnect Height | 80 ft | |
Flight in Icing Conditions
| Engine Cowl Anti-Ice | In icing conditions (visible moisture, SAT ≥ −40 °C, TAT ≤ 10 °C) | |
| Wing Anti-Ice | > 22,000 ft | Ice detection indicated |
| < 22,000 ft | Ice detection indicated
OR In icing conditions OR TAT ≤ 10 °C & approach flaps extended | |