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Introduces major airplane systems, with detailed descriptions in subsequent chapters.
Covers DC and AC electrical power sources, batteries, generators, inverters, and distribution.
Details the DC power sources, including batteries, generators, and their respective controls and indicators.
Details AC power sources, including inverters, controls, and operation.
Details DC power sources, including batteries, generators, and their respective controls and indicators.
Details AC power sources, including inverters, controls, and operation.
Details the fuel storage capacity, tip tank attachment, baffles, jet pumps, and venting systems.
Details fuel storage capacity, tip tank attachment, baffles, jet pumps, venting, and fuselage tanks.
Lists the engine systems, including oil, fuel, ignition, power control, instrumentation, starting, synchronizing, and thrust reversers.
Explains the engine power control via the thrust lever and its quadrant operation.
Covers sensing elements, control units, fire lights, and the fire detection system test.
Covers the two-bottle extinguishing system common to both engines, agent type, and operation.
Describes the various anti-ice systems for engines, windshield, radome, wings, horizontal stabilizer, and pitot/static systems.
Describes anti-ice systems for engines, windshield, and wings.
Details bleed air supply, routing, and differences in systems based on serial numbers.
Illustrates and describes the air-conditioning system for later serial numbers.
Illustrates and describes the air-conditioning system for earlier serial numbers.
Locates the module on the copilot's instrument panel and details its controls.
Covers normal system operation before takeoff, during flight (automatic/manual), descent, and landing.
Details the emergency source of bleed air for increasing cabin airflow during leaks or malfunctions.
Explains how engine-driven pumps supply fluid, valve operation, and system pressure.
Covers the landing gear indicating system, gear position lights, warning system, and components.
Explains the hydraulic brake system, antiskid systems, emergency brakes, and parking brakes.
Covers the manually operated primary flight controls, including elevators, ailerons, and rudder.
Describes hydraulically actuated spoilers and flaps, electrically controlled.
Covers systems providing stall warnings, including stall vanes, shakers, nudgers, stick pushers, and indicators.
Covers the pitot-static system, air data sensor, and RAM AIR TEMP gage.
Covers the JET FC 110 AFCS, its workload reduction capabilities, and autopilot/yaw damper operation.
Explains the Collins FD 108 flight director system, including ADI, HSI, mode selector, and command bars.
Covers oxygen system components: cylinder, shutoff valve, regulator, indicators, and distribution systems.
General| Manufacturer | Learjet |
|---|---|
| Model | 24 |
| Role | Business jet |
| Crew | 2 |
| Passenger Capacity | 8 |
| Length | 43 ft 3 in (13.18 m) |
| Wingspan | 35 ft 7 in (10.85 m) |
| Max Takeoff Weight | 13, 500 lb (6, 123 kg) |
| Thrust | 2, 950 lbf (13.1 kN) each |
| Number Built | 259 |
| Wing Area | 21.5 m² (231 sq ft) |
| Engines | 2 × General Electric CJ610 turbojets |
| Service Ceiling | 13, 715 m (45, 000 ft) |
| Rate of Climb | 35 m/s |
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