Bombardier Challenger 650 Airplane Flight Manual CL-600-2B16 – Training Edition PDF

Description

Bombardier Challenger 650 Airplane Flight Manual CL-600-2B16 – Training Edition

This is the complete Airplane Flight Manual for the Bombardier Challenger 650, model CL-600-2B16, applicable to serial number 6050 and subsequent. Published under document number PSP 650-1 and issued as a Training Edition, this 945-page manual is the operational reference covering limitations, emergency procedures, normal procedures, abnormal procedures, and performance data for the Challenger 650. The document carries the watermark “FOR TRAINING PURPOSES ONLY / NO UPDATES PROVIDED FOR THIS COPY” and is intended for familiarization and training rather than as a current, updated operational AFM.

File Details

• Manual Type: Airplane Flight Manual (AFM) – Training Edition
• Manufacturer: Bombardier Inc.
• Model: CL-600-2B16 Challenger 650
• Serial Applicability: Serial No. 6050 and subsequent
• Document Number: PSP 650-1
• Revision: 15 (March 25, 2019)
• First Issued: October 27, 2015
• Maximum Take-Off Weight: 21,863 kg / 48,200 lb
• Language: English
• Page Count: 945
• File Format: PDF

Chapters Covered

The Bombardier Challenger 650 Airplane Flight Manual is organized into eight chapters, each addressing a distinct area of aircraft operation and systems knowledge.

• Chapter 1 – Introduction: general information, scope of the AFM, limitations, status of AFM information, emergency procedures, normal procedures, abnormal procedures, performance, supplements, appendices, pagination, definitions, abbreviations, registry codes, service bulletins
• Chapter 2 – Limitations: kinds of airplane operation, structural weight, centre of gravity limits, altitude and temperature operating limits, take-off limitations, rotation rate and pitch attitude, pitch trim, cold weather operations, operation in icing conditions, cowl anti-ice system, wing anti-ice system, super-cooled large droplet icing, enhanced take-off procedures, runway slopes, tailwind conditions, approaches, minimum flight crew, maximum occupants, maximum crosswind component, engines, engine indications, engine operating limits, oil temperature, oil pressure, continuous engine ignition, autothrottle, automatic performance reserve, starter cranking limits, engine relight, fuel, fuel temperature, fuel grades, fuel additives, fuel jettison, fuel transfer, oil grades, oil consumption, oil level, oil replenishment, auxiliary power unit, APU indications, maximum operating speed and Mach number, RVSM maximum operating speed, flaps extended speed, landing gear operating and extended speeds, tire limit speed, turbulence penetration speed, minimum operating limit speed, design maneuvering speed, maneuvering limit load factors, side slip maneuvers, air-conditioning and pressurization, automatic flight control system, bleed air systems, electrical systems, flight controls, flaps, flight spoilers, stall protection system, thrust reversers, taxi and landing lights, wheel brake cooling limitations, configuration deviation list, electrical/avionics equipment, flight management system, navigation receivers, TAWS, RAAS, integrated flight information system, synthetic vision system, datalink
• Chapter 3 – Emergency Procedures: rejected take-off, engine fire/severe engine damage (in flight and on ground), double engine failure, jet pipe overheat, engine oil pressure low, uncommanded thrust reverser deployment, post-shutdown engine tail pipe fire, N1/N2 overspeed, engine overtemperature, engine starter fails to cutout, uncommanded acceleration, smoke/fire/fumes, smoke or fumes removal, emergency descent, uncontrollable loss of cabin pressure, high rate of cabin pressurization or over-pressurization, autopilot failure, AFCS messages failure, uncommanded yaw motion, APU fire, APU overspeed, APU overtemperature, bleed air leaks, ditching and forced landing, emergency evacuation, loss of all normal electrical power, aileron/elevator/rudder system jammed, stabilizer trim runaway, stall recovery, overspeed warning, low fuel, wing leading edge overheat, fuselage/wing anti-ice duct failure, unreliable airspeed, gear up disagree, gear down disagree, landing gear lever jammed, landing gear up/unsafe landing, main landing gear bay overheat, nose door fails open, parking brake on, excessive asymmetry or loss of braking, passenger door failure, configuration warning
• Chapter 4 – Normal Procedures: power plant first flight of the day, engine vibration test, before starting engines, starting engines using APU air supply, starting engine using external air supply, starting engine using engine cross bleed air, failure to start, after starting engines, ATS check, APR check, anti-ice cowl check, thrust reverser check, before take-off, high crosswind take-off, after take-off, climb, cruise, descent, approach, before landing, go-around, after landing, engine shutdown, air-conditioning and pressurization, bleed leak detection test, air-conditioning on ground using APU, unpressurized take-off and landing, auxiliary power unit, automatic flight control system, doors, electrical, electronic flight instruments, fire protection system, flight controls, navigation systems, fuel, hydraulic power, ice and rain protection, landing gear wheels and brakes, lighting, oxygen system, stall protection, aural/visual warning system, consolidated checklists, severe turbulence penetration
• Chapter 5 – Abnormal Procedures: power plant, single engine procedures, air start, air-conditioning and pressurization, automatic flight control system, auxiliary power unit, doors, electrical, fire protection, flight controls, fuel, hydraulic power, ice and rain protection, instruments system, landing gear wheel and brake system, miscellaneous systems, aural/visual warning system
• Chapter 6 – Performance: general, conversion data, calibration, flight capabilities, thrust settings, take-off performance, obstacle clearance, enroute performance, approach and landing climb, landing performance, turn-around time
• Chapter 7 – Supplements: noise characteristics, operation on wet and contaminated runways, operation at airport elevations up to 14,000 feet, Category II operations, flight with landing gear down, operation with airplane systems inoperative, approaches below 4.5 degrees, steep approaches up to 5.5 degrees, additional take-off performance information, operational capabilities, operation with cracked windshield faceply, runway awareness and advisory system, RNP authorization required approach operations, operation on wet grooved runways, FAA steep approach into London City Airport
• Chapter 8 – Appendices: configuration deviation list covering communications, landing gear, lights, structures, doors, fuselage, stabilizers, windows, and wings

Together, these chapters give a Challenger 650 pilot or maintenance technician the full operational framework for the aircraft: from pre-flight checks and normal procedures through emergency and abnormal situations, and on to the precise performance data needed for flight planning and obstacle clearance. The manual goes well beyond surface-level information, detailing engine operating limits for the CF34-3B, fuel system management including auxiliary and tail tank transfer logic, hydraulic system architecture, flight control system behavior, ice and rain protection logic, and a comprehensive set of performance charts for take-off, climb, and landing. The emergency and abnormal procedures chapters cover everything from rejected take-off and engine fire to unreliable airspeed, jammed flight controls, and loss of electrical power, with boxed immediate-action steps and expanded checklists. The normal procedures chapter includes consolidated checklists covering every phase of flight from pre-start through securing the aircraft.

Why This Manual Matters

Operating a Challenger 650 demands exact adherence to limitations and procedures. This Airplane Flight Manual is the reference that defines the approved flight envelope, the correct crew actions for abnormal and emergency situations, and the performance data that determines whether a given take-off or landing is safe. Having the complete manual available in PDF form means you can search the content, print the pages you need, and keep the full reference on any device – laptop, tablet, or phone – wherever maintenance or flight planning is happening. The performance chapter alone contains take-off distance charts, obstacle clearance calculations, climb gradients, and landing field length data that are essential for safe flight planning, all presented with worked examples that show exactly how to apply the corrections for temperature, altitude, wind, runway slope, and anti-ice configuration.

The Training Edition of this manual is intended for familiarization and training purposes, providing a comprehensive study reference for the Challenger 650 systems, procedures, and performance. It is a substantial technical document – 945 pages – that covers the aircraft in thorough detail and includes the full range of supplements covering special operations such as wet and contaminated runways, steep approaches, Category II operations, and RNP AR approach procedures.

Get Instant Access

This Bombardier Challenger 650 Airplane Flight Manual is delivered as an instant PDF download. There is no shipping, no waiting, and no physical media. You receive the complete manual immediately after purchase, ready to view on any device and to print if you prefer a paper reference. Whether you are studying the aircraft, preparing for a type rating, or maintaining a Challenger 650, this manual gives you the complete operational and technical reference in one file.