CL650/Operations Reference: Difference between revisions
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== Preflight Inspection == | |||
[[File:Preflight Inspection.png|border]] | |||
Revision as of 16:21, 6 March 2024
Airspeeds and Power Settings
The following guidance for airspeed, pitch, and N1 values is indexed to a 38,000 lb plane, in ISA conditions, calm winds, and 30% Mean Aerodynamic Chord (MAC).
| Flight Phase | Airspeed (kts) | Pitch (degrees) | N1 % |
| Climb | |||
| < 10,000 ft | 250 | 12° | Thrust Limit |
| 10,000–25,000 ft | 250 | 7.5° | Thrust Limit |
| > 25,000 ft | 250 / M0.72 | 5° | Thrust Limit |
| Descent | |||
| All altitudes | 250 | 0° | Idle |
| Initial approach (level flight) | |||
| Flaps 0° / Gear up | 250 | 2.5° | 60 |
| Flaps 0° / Gear up | 200 | 4° | 55 |
| Flaps 20° / Gear up | 180 | 2° | 60 |
| Flaps 30° / Gear down | 160 | 2° | 68 |
| Final approach (3° slope) | |||
| Flaps 45° / Gear down | VRef +5 | −2° | 60 |
| Flaps 20° / Gear down / Single engine | VRef +14 +5 | 1° | 63 |
| Min maneuvering | |||
| Flaps 0° / Gear up | 170 | 7° | 53 |
| Flaps 20° / Gear up | 160 | 3° | 55 |
| Flaps 30° / Gear up | 150 | 2° | 60 |
| Flaps 30° / Gear down | 150 | 2° | 67 |
| Flaps 45° / Gear down | 145 | 0° | 73 |
| Correction guidance on power settings | |||
| Weight | ±1% N1 per ±4,000 lbs (2,000 kg) | ||
| Single engine | +15% N1 | ||
| Altitude | +0.8% N1 per 1,000 ft | ||
| Wind (on approach) | +3% per 10 kt headwind | ||
Climb Data
| Climb Profile (500 fpm ceiling) | Max Weight | Altitude | |
| 250 kts / 250 kts / M0.72 / ISA | LBS | KG | Flight Level |
| 48,000 | 21,800 | 350 | |
| 47,750 | 21,700 | 360 | |
| 47,250 | 21,500 | 360 | |
| 37,000 | 16,800 | 410 | |
| 250 kts / 300 kts / M0.78 / ISA | LBS | KG | Flight Level |
| 48,000 | 21,800 | 350 | |
| 46,500 | 21,100 | 360 | |
| 45,750 | 20,800 | 360 | |
| 35,750 | 16,200 | 410 | |
Cruise Altitudes
Mach 0.72
| M0.72 CRUISE ISA | |||||||||||
| LBS | 28,000 | 30,000 | 32,000 | 34,000 | 36,000 | 38,000 | 40,000 | 42,000 | 44,000 | 46,000 | 48,000 |
| KG | 12,700 | 13,600 | 14,500 | 15,500 | 16,400 | 17,300 | 18,200 | 19,100 | 20,000 | 20,900 | 21,800 |
| Flight
Level |
410 | 390 | 370 | 350 | |||||||
| M0.72 CRUISE ISA+10 | |||||||||||
| LBS | 28,000 | 30,000 | 32,000 | 34,000 | 36,000 | 38,000 | 40,000 | 42,000 | 44,000 | 46,000 | 48,000 |
| KG | 12,700 | 13,600 | 14,500 | 15,500 | 16,400 | 17,300 | 18,200 | 19,100 | 20,000 | 20,900 | 21,800 |
| Flight
Level |
410 | 390 | 370 | 350 | |||||||
Mach 0.80
| M0.80 CRUISE ISA | |||||||||||
| LBS | 28,000 | 30,000 | 32,000 | 34,000 | 36,000 | 38,000 | 40,000 | 42,000 | 44,000 | 46,000 | 48,000 |
| KG | 12,700 | 13,600 | 14,500 | 15,500 | 16,400 | 17,300 | 18,200 | 19,100 | 20,000 | 20,900 | 21,800 |
| Flight
Level |
410 | 390 | 370 | 350 | |||||||
| M0.80 CRUISE ISA+10 | |||||||||||
| LBS | 28,000 | 30,000 | 32,000 | 34,000 | 36,000 | 38,000 | 40,000 | 42,000 | 44,000 | 46,000 | 48,000 |
| KG | 12,700 | 13,600 | 14,500 | 15,500 | 16,400 | 17,300 | 18,200 | 19,100 | 20,000 | 20,900 | 21,800 |
| Flight
Level |
410 | 390 | 370 | 350 | 330 | ||||||
Preflight Inspection
