CL650/Type Data Sheet

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Revision as of 21:08, 5 March 2024 by Pilsner (talk | contribs) (Pilsner moved page CL650/General Information to CL650/General Type Information: Misspelled title)

Weights

Basic Empty Weight 27,150 lbs 12,315 kg
Operating Empty Weight (Pilots & Equipment) 27,680 lbs 12,556 kg
Maximum Zero Fuel Weight 32,000 lbs 14,515 kg
Maximum Take-off Weight 48,200 lbs 21,863 kg
Maximum Landing Weight 38,000 lbs 17,236 kg
Fuel Capacity at International Standard Atmosphere (ISA) temperature of +15 °C 20,000 lbs 9,098 kg

Procedure Capabilities

Approach Category C
Precision Approaches ILS CAT II/80 ft RA
RNAV/RNP Approaches RNP AR 0.3 nm/LPV
Available SBAS Providers WAAS, EGNOS, GAGAN, MSAS
Equipment Code M-SBDE1E2E3FGHIJ1J4J5J7M3RWXYZ/LB1V1D1
PBN Capability Code PBN/A1L1B1C1D1O1S1T1

Service Bulletins

Steep Approach Capability 650–34–008 Not Implemented
RNP AR Approach Capability 650–34–009 Implemented
Runway Awareness and Advisory System 650–34–010 Not Implemented
Flex & Maximum Take-off Thrust Limit 650–34–012 Implemented (See Avionics Options)