CL650/Operations Reference: Difference between revisions

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== Airspeeds and Power Settings ==
== Airspeeds and Power Settings ==
The following guidance for airspeed, pitch, and N<sub>1</sub> values is indexed to a 38,000 lb plane, in ISA conditions, calm winds, and 30% Mean Aerodynamic Chord (MAC).
{| class="wikitable"
|'''Flight Phase'''
|'''Airspeed (kts)'''
|'''Pitch (degrees)'''
|'''N<sub>1</sub> %'''
|-
| colspan="4" |'''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
|-
| colspan="4" |'''Descent'''
|-
|All altitudes
|250
|0°
|Idle
|-
| colspan="4" |'''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
|-
| colspan="4" |'''Final approach (3° slope)'''
|-
|Flaps 45° / Gear down
|V<sub>Ref</sub> +5
|−2°
|60
|-
|Flaps 20° / Gear down / Single engine
|V<sub>Ref</sub> +14 +5
|1°
|63
|-
| colspan="4" |'''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
|-
| colspan="4" |'''Correction guidance on power settings'''
|-
|Weight
| colspan="3" |±1% N<sub>1</sub> per ±4,000 lbs (2,000 kg)
|-
|Single engine
| colspan="3" |+15% N<sub>1</sub>
|-
|Altitude
| colspan="3" |+0.8% N<sub>1</sub> per 1,000 ft
|-
|Wind (on approach)
| colspan="3" |+3% per 10 kt headwind
|}


== Climb Data ==
== Climb Data ==
{| class="wikitable"
|'''Climb Profile (500 fpm ceiling)'''
| colspan="2" |'''Max Weight'''
|'''Altitude'''
|-
| rowspan="5" |'''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
|-
| rowspan="5" |'''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 ==
== Cruise Altitudes ==
=== Mach 0.72 ===
{| class="wikitable"
| colspan="12" |'''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
| colspan="6" |410
|390
| colspan="2" |370
| colspan="2" |350
|}
{| class="wikitable"
| colspan="12" |'''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
| colspan="5" |410
| colspan="2" |390
| colspan="2" |370
| colspan="2" |350
|}
=== Mach 0.80 ===
{| class="wikitable"
| colspan="12" |'''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
| colspan="5" |410
| colspan="2" |390
| colspan="2" |370
| colspan="2" |350
|}
{| class="wikitable"
| colspan="12" |'''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
| colspan="3" |410
| colspan="2" |390
| colspan="3" |370
| colspan="2" |350
|330
|}

Revision as of 21:33, 5 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
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