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General| Brand | BOMBARDIER |
|---|---|
| Model | Challenger 601-3A CL-600-2B16 |
| Category | Tools |
| Language | English |
General details about the training program.
Necessary qualifications for enrolling in the training course.
Covers the practical training phases involving simulators and aircraft.
Outlines the criteria and methods for successfully completing the course.
Details the curriculum for ground school modules.
Details the curriculum for flight training modules.
Details the structural makeup of the aircraft fuselage and its sections.
Describes the passenger-crew, baggage, and emergency exit doors.
Explains the AC electrical system and its four subsystems.
Describes the DC power supply derived from AC via TRUs and the battery.
Covers the internal and external lighting systems.
Explains the visual and aural warning systems for malfunctions.
Details the aircraft's fuel storage, distribution, and control systems.
Describes cockpit, passenger compartment, and service lighting.
Details landing, taxi, navigation, anticollision, and emergency lights.
Details the system that indicates non-urgent malfunctions with amber lights.
Describes the system providing distinct audible tones for hazardous situations.
Details the location and configuration of fuel tanks, including the tail tank.
Explains fuel flow from tanks via gravity, ejectors, and pumps.
Details the panel for controlling and indicating fuel quantity, temperature, and system status.
Describes the single-point pressure refueling and overwing fueling procedures.
Details the additional fuel tank, its transfer system, and fuel jettison.
Breaks down the APU into its six main sections.
Lists the various systems associated with the APU operation.
Describes the procedure and indications for starting the APU.
Details the GE Series CF34 engines, their specifications, and modular concept.
Explains the self-contained and automated engine oil system.
Details the integrated hydromechanical-electronic fuel system.
Describes the dual high-energy ignition system.
Covers engine power control via the throttle quadrant and related systems.
Explains the primary engine instruments and their operation.
Details the procedures for ground, airstart, and windmilling starts.
Covers automatic performance reserve and engine speed control.
Describes the electrically energized, pneumatically operated thrust reverser system.
Details the sensing loops and detection units for fire and overheat warnings.
Covers the engine and APU fire extinguishing systems using Firex bottles.
Describes the system for detecting overheat conditions in the MLG bays.
Details the system for visual indication of overheat in engine jet pipe and pylon areas.
Details the control and indication of 10th-stage bleed-air valves.
Describes the control and operation of 14th-stage bleed-air valves.
Explains the system providing warm air for cockpit and windshield.
Covers the system for detecting and indicating bleed-air leaks.
Explains the function and operation of the ice detection system.
Details the pneumatically and electrically operated anti-icing systems.
Focuses on cowl and wing anti-icing using bleed air.
Covers electrically heated windshields and ADS probes.
Explains how air conditioning is achieved through bleed air and ACUs.
Describes the cockpit and cabin temperature control systems.
Lists the electropneumatic valves controlling the AC system.
Explains air distribution via ducting to occupied areas.
Covers general, ground, and in-flight operation of the AC system.
Describes the system for ventilation during unpressurized flight or emergencies.
Divides pressurization into automatic, manual, and emergency systems.
Identifies the sources of air for normal and emergency pressurization.
Lists the main components of the pressurization system.
Explains the automatic cabin pressure selector and its controls.
Describes the manual control for pressurization system operation.
Details the valves that meter air from occupied areas to the atmosphere.
Outlines the safety systems for controlling cabin pressure.
Describes the system for rapid decompression in emergencies.
Explains the components and operation of hydraulic system number 1.
Describes the components and operation of hydraulic system number 2.
Details the components and operation of hydraulic system number 3.
Covers normal, abnormal, and emergency operating conditions for the pumps.
Lists subsystem components powered by each hydraulic system.
Details the operation of the landing gear and its controls.
Explains how the WOW system provides air/ground information.
Describes the main landing gear structure, actuators, and doors.
Details the nose landing gear assembly, actuators, and doors.
Details the brake application, antiskid system, and parking brakes.
Explains the function and features of the antiskid system.
Explains how to set and release the parking brakes.
Details the actuation of ailerons, elevators, and rudders by PCUs.
Explains how roll control is maintained via hydraulically powered ailerons.
Describes how yaw control is maintained with the hydraulically powered rudder.
Details how pitch control is achieved through hydraulically powered elevators.
Explains pitch trim achieved by varying horizontal stabilizer angle.
Covers electrically actuated flaps and hydraulically powered spoilers.
Details the flap system, including inboard and outboard flaps.
Covers the system providing stall warnings and protection.
Integrates VHF, HF, SELCAL, audio, transponder, and CVR systems.
Lists systems for short-range navigation using radio navaids.
Details the VHF NAV systems for VOR, LOC, GS, and MKR navaids.
Explains the DME systems for measuring slant range distance.
Describes the ADF system for reception of ground station signals.
Shows the EHSI displays for primary navigation selections.
Illustrates common EFIS failure displays.
Covers the DAFCS and its constituent systems.
Explains the dual IRS for accurate aircraft attitude and navigation data.
Details the DADS for detecting and measuring flight environmental data.
Covers the EFIS components for displaying flight information.
Describes the MFD system, its components, and capabilities.
Covers the FMS for lateral and vertical navigation guidance.
Covers the AFCS, including FD, autopilot, and yaw damper functions.
Details the demand-type crew oxygen system with its cylinder and regulators.
Explains the components and operation of the crew oxygen system.
States the limitations of the crew oxygen system.
Outlines the sequence for performing a preflight walkaround inspection.
Lists abbreviations related to the aircraft's electrical system.
Lists abbreviations related to the aircraft's fuel system.
Lists abbreviations related to the aircraft's powerplant and APU.
Lists abbreviations related to the aircraft's hydraulic systems.
Lists abbreviations related to the aircraft's environmental systems.
Lists abbreviations related to the aircraft's anti-ice systems.
Lists abbreviations related to the aircraft's avionics systems.
Shows the pilot and copilot annunciator panels.
Displays controls for engine, hydraulic, and flight systems.
Illustrates various control panels including fire, fuel, and lighting systems.
