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General| Brand | FlightSafety |
|---|---|
| Model | LEARJET 45 |
| Category | Aircrafts |
| Language | English |
Provides an overview of the chapter's scope, covering airframe structure and general systems.
Discusses aircraft certification, operational limits, and the primary structural components.
Details the aircraft's structural design requirements, including fuselage, wings, and empennage.
Describes the fuselage construction, major assemblies, and basic sections.
Covers the radome, aluminum construction, avionics bay, and nose wheelwell.
Details the cockpit and passenger areas, including dimensions and cabin features.
Explains the passenger/crew door, emergency exit hatch, and tailcone access doors.
Describes the windshield and cabin windows, including construction and features.
Locates the fuselage fuel tank aft of the rear pressure bulkhead.
Describes the tailcone section, access doors, baggage compartment, and equipment bay.
Details the wing's swept planform, aspect ratio, and specific features like winglets and anti-icing.
Describes the T-tail empennage, vertical stabilizer, rudder, horizontal stabilizer, and delta fins.
Lists the locations and quantity of static discharge wicks on the aircraft.
Shows the location of antennas, emphasizing their importance in external inspection.
Outlines the primary and secondary DC power sources and AC power provision.
Explains the split bus system, power distribution, and sources like batteries, generators, GPU, and APU.
Details the main batteries, emergency battery, GPU, and APU as DC power sources.
Describes the standard emergency battery, its location, duration, and function.
Explains GPU connection, voltage/amp limits, and system indications.
Describes the optional APU, its ground certification, and operation with generators.
Details the engine-driven starter/generators, their ratings, and automatic on-line operation.
Explains the functions of GCUs including voltage regulation and current limiting.
Covers the switch panel layout, dark cockpit integration, and manual override options.
Describes the function of switches and indicators on the electrical control panel.
Details components like fuses, contactors, and circuit breakers.
Explains the basic DC power distribution and the split bus system.
Mentions AC power is provided by alternators for windshield ice/fog protection.
Covers battery overheat, single and dual generator failures.
Explains the use of lighting for cockpit, instruments, and cabin illumination.
Divides airplane lighting into interior and exterior categories.
Details lighting locations for cockpit, cabin, baggage, and maintenance areas.
Lists exterior lights including landing, taxi, recognition, navigation, and anticollision lights.
Describes the dual bulb landing lights and single filament taxi lights.
Consists of outboard bulbs of landing light assemblies.
Covers wing-tip position lights and tail-mounted position light.
Optional lights installed on the horizontal stabilizer.
Describes dual selectable beacon/strobe units for anticollision.
Provides visual detection of ice buildup on wings.
Optional lights for baggage compartment and refueling areas.
Discusses effects of single and dual generator failures on exterior lighting.
Explains the system's purpose in warning for malfunctions and unsafe conditions.
Describes the components: CWP, CAS, voice messages, and master lights.
Details the switch/indicators, bulb redundancy, and their flashing behavior.
Covers system test, bulb change, and dimming function.
Located in the center instrument panel, it contains displays and aural systems.
Serves as a backup display for warnings and primary for cautions/advisories.
Describes audio tones and voice messages, their precedence, and muting.
Provides visual and aural alerts for unsafe takeoff configurations.
Details degraded system displays during dual generator failure.
Covers fuel storage, quantity indicating, transfer, vent, and refueling systems.
Explains the system's role in storage, transfer, and low-pressure distribution.
Describes the wet-wing design, fuel capacity, collector tanks, and scavenge jet pumps.
Details the single bladder-type fuel cell, its capacity, and refueling port.
Explains the system using capacitance probes and microprocessor for fuel quantity.
Covers the engine/fuel control panel, crossflow valve, standby pumps, and fuselage transfer lines.
Details fuel routing from wing tanks, filters, fuel control unit, and manifolds.
Explains the function of motive flow pumps and jet pumps in fuel transfer.
Describes airframe and engine mounted fuel filters and their bypass capability.
Covers firewall shutoff valves, their location, and electrical actuation.
Explains the function and indication of low fuel pressure switches.
Describes the system for wing and fuselage tank pressurization and ventilation.
Connects high points of wing tanks with fuselage tank for pressure equalization.
Locates and describes various drain valves.
Covers aircraft servicing, fueling types, and defueling procedures.
Details the system for simultaneous wing and fuselage tank filling.
Describes refueling via fuselage filler port.
Explains defueling via suction through SPPR nozzle.
Introduces the APU as an electrical and pneumatic source for ground operations.
Describes the APU as a self-contained unit with fire detection and external power/fuel requirements.
Details the APU's self-contained systems and major sections.
Explains the fans and vents installed in the aft equipment bay for cooling.
Lists the main APU systems: Lubricating, Ignition, Electrical, Fuel, Protection, and Fire Detection.
Covers APU operation via control panel, ECU, and starting system.
Explains pneumatic output control via Bleed Air Valve and PACK switch.
Describes APU generator operation and its effect on aircraft buses.
Details conditions causing automatic shutdown or preventing APU start.
Describes controls and indicators for APU maintenance purposes.
Covers periodic oil changes and adding oil.
Describes the Learjet 45 powerplant, engine-related sub-systems, controls, and instrumentation.
Details the TFE731 engines, thrust ratings, and thrust reversers.
Divides the engine into seven major sections: Air Inlet, Fan, Compressor, Combustor, Turbine, Exhaust, and Accessory.
Explains the display of engine instruments on the pilot's inboard display unit (DU2).
Lists indications appearing in the EICAS engine field and their color coding.
Details CAS messages related to engine and thrust reverser systems.
Located between DU2 and DU3, displays engine warnings.
Covers engine control modes (computer-on/off) and components.
Describes the DEEC's function, location, and input/output parameters.
Explains the system's role in pressurizing, filtering, heating, and delivering fuel to the engine.
Covers Ignition, Starter, Engine Synchronization, APR, Vibration Monitor, and EDS.
Details the system for lubrication, cooling, and heating of engine fuel.
Explains the electrically controlled, hydraulically actuated target-type thrust reversers.
Describes the pneumatic system's role in anti-icing, air conditioning, and pressurization.
Explains LP and HP bleed-air usage for various aircraft systems.
Details the LP and HP bleed-air systems and APU bleed-air.
Covers bleed switches, ECS controller, PRSOVs, and SOVs.
Describes the alternate system for cabin pressurization using LP bleed air.
Explains HP bleed-air usage for actuation power and pressurization jet pump.
Mentions CAS messages and CWP annunciators for alerting the crew.
Controls engine/APU bleed-air supply pressure to the ECU.
Details equipment designed to detect and prevent ice buildup on critical surfaces.
Emphasizes turning on anti-icing equipment before encountering icing conditions.
Describes the ice detection probe and its automatic deicing cycle.
Covers engine bleed-air and electrical heating systems for anti-icing.
Outlines the system's components for cockpit/cabin distribution, pressurization, and ventilation.
Explains primary heating/cooling via bleed-air mixing and ACM.
Lists major tailcone components: PRSOV, pre-cooler, ECU, and water separator.
Describes the system for independent cockpit and cabin temperature control.
Details air distribution to cockpit and cabin via ducts and diffusers.
Provides heat to the baggage compartment to prevent freezing.
Provides electrical heat to pilot and copilot rudder pedal areas.
Explains how the system maintains cabin altitude lower than actual airplane altitude.
Describes the pressurized area and the role of the CPCS.
Lists key components: control panel, controller, indicators, outflow valves, and jet pump.
Provides crew interface for system operation and monitoring.
Details the dual-channel microprocessor unit controlling pressurization.
Covers primary/secondary displays, CAS messages, and protection features.
Explains system test, automatic mode, and manual mode operations.
Discusses unique flight profiles for cabin pressure control at high altitude airports.
Outlines the hydraulic system components and inputs for display.
Describes the engine-driven pumps and auxiliary pump for hydraulic fluid supply.
Details reservoir, shutoff valves, pumps, filter manifolds, accumulators, and landing gear control module.
Explains normal operation of the main and auxiliary hydraulic systems.
Covers normal and abnormal indications on EICAS/MFD and RMU.
Describes servicing via the ground service panel.
Introduces the electrically controlled, hydraulically actuated landing gear and brake systems.
Describes the landing gear configuration and door operation.
Details the indicating system, main gear, nose gear components, and operation.
Covers the brake-by-wire system, operation, emergency, and parking brakes.
Explains the digital nose wheel steering system, components, and operation.
Covers primary mechanical controls and secondary electrical/hydraulically actuated surfaces.
Describes primary flight control surfaces and their mechanical operation.
Details elevators, ailerons, and rudder systems.
Covers horizontal stabilizer, trim systems, flaps, and spoilers.
Explains the stall warning system, AOA sensors, and indications.
Describes the Honeywell Primus 1000 avionics system and its displays.
Covers the "glass cockpit" design, system functions, and components.
Details the IC-600 computers, their functions, and redundancy.
Explains the dual-channel DAUs for engine and systems data acquisition.
Located on the electrical control panel, controls power to avionics busses.
Covers VHF communication, navigation, DME, transponder, and RMUs.
Provides airspeed, altitude, and temperature data via ADCs.
Describes the dual AHRS for attitude and heading information.
Provides flight path, navigation, engine, and systems information on display units.
Explains how to switch display units for redundancy.
Describes procedures for handling a single display unit failure.
Outlines operation with multiple display unit failures.
Alerts pilots to discrepancies between displayed data sources.
Displays attitude, heading, navigation, and airspeed data.
Allows setting of barometric correction in inches of mercury or HectoPascals.
Details airspeed display formats, trend vectors, and selected speeds.
Describes the vertical speed display and its indicators.
Engages normal or high-speed climb/descent profiles.
Allows definition of waypoints with altitudes for vertical navigation.
Provides graphic depiction and definition of holding patterns.
Covers linking FMS approaches to the flight plan for lateral and vertical steering.
Allows setting of radio frequencies and transponder codes.
Contains worldwide or regional navigation data, updated regularly.
Describes the Primus 660 X-band radar for weather detection and ground mapping.
Details TCAS I and TCAS II operations, controls, and displays.
Explains the selectable traffic altitude bands for TCAS.
Covers primary mechanical controls and secondary electrical/hydraulically actuated surfaces.
Describes primary flight control surfaces and their mechanical operation.
Details elevators, ailerons, and rudder systems.
Covers horizontal stabilizer, trim systems, flaps, and spoilers.
Explains the stall warning system, AOA sensors, and indications.
Covers system storage, crew distribution, passenger distribution, and components.
Describes the quick-donning mask system for crew oxygen supply.
Explains the system for providing oxygen to passengers during emergencies.
Provides guidance on planning oxygen requirements.
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