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2 Engines (each) 5.5 5.2 11.19 5.09
Total 11.0 10.4 22.38 10.18
Airspeed Limits (IAS) * Knots Mach VMO and MMO (Maximum Operating) Below 8000 feet 330* * *See Flight Manual for variations of VMO and MMO at or above 8000 ft
VFE (Flaps extended) 8° 20° 30° 45° 230 230 196 191 Or for Airplanes 7904 and subsequent; and Airplanes incorporating Canadair Service Bulletin: SB601R-11-080, Flight Compartment, Placards and markings – Installation of the New Airspeed Limitation Placard and Removal of Flap Inspection Placard: VFE (Flaps extended) 8° 20° 30° 45° 230 230 185 170
VA (Manoeuvring) (Refer to Flight Manual for variations of VA with altitude and aircraft weight)
VLO (Landing Gear Operating) Extending Retracting 250 200
VLE (Landing Gear Extended) 250
Max. tyre ground speeds: m.p.h. knots
Nose Gear Tyre 210 182
Main Gear Tyre 210 182
6. Centre of Gravity Range
Centre of Gravity Range: See AFM, CSP A-012
Datum: FS 0.0 located at 100 in. Fwd of the aircraft nose
Mean Aerodynamic Cord (MAC): 2.53 m (99.43 in.) (MAC leading edge at fuselage station 493.793.1 in.)
Leveling Means: A leveling targets are installed in the aft equipment bay, for use with a plumb bob to level the aircraft in the lateral and longitudinal planes.
7. Maximum Certified Weights kg (lbs)
Max. Taxi and ramp 23,247 kg (51,250 lb.)
Max. Take-off 23,133 kg (51,000 lb.)
Max. Landing 21,319 kg (47,000 lb.)
Max. Zero fuel 19,958 kg (44,000 lb.)
With option <0004 (JAA) > incorporated, weight limits change to:
Max. Taxi and ramp 24,154 kg (53,250 lb.)
Max. Take-off 23,995 kg (52,900 lb.)
Max. Landing 21,205 kg (46,750 lb.)
NOTE: See AFM (CSP A-12) for other weight limitations and aircraft eligibility.
8.
Minimum Flight Crew Minimum Flight Crew: 2 (Pilot and co-pilot)
9.
Maximum Seating Capacity:
50 pax plus 5 crew members
48 pax plus 5 crew members if Forward Wardrobe is installed (TC601R12721).
For CL-600-2B19 in the “Green Configuration”, refer to Note (6).
10.
Cargo compartment loading Aft Baggage Compartment
* Note: Values marked with asterisk are obtained with the incorporation of
Modification TC601R100914
11.
Environmental Flight Envelope Refer to approved Airplane Flight Manual
12.
Other Limitations Refer to approved Airplane Flight Manual.
13.
Auxiliary Power Unit (APU)
Class Volume (m3) Max. Allowable Load (Kg)
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本文链接地址：European Aviation Safety Agency TYPE-CERTIFICATE DATA SHEET CL-600(4)
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