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Learjet 25B - Page 317

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16-iii
ILLUSTRATIONS
Figure Title Page
16-1 Pitot-Static System (Typical) ................................................................................. 16-2
16-2 Pitot Head (Typical) ............................................................................................... 16-3
16-3 Pitot-Static Drains (Typical)................................................................................... 16-3
16-4 Static Ports (Typical).............................................................................................. 16-3
16-5 ALTERNATE STATIC SOURCE Valve ................................................................ 16-4
16-6 RAM AIR TEMP Gage.......................................................................................... 16-5
16-7 Autopilot Flight Controller .................................................................................... 16-5
16-8 Control Wheel Switches (Pilot’s)........................................................................... 16-6
16-9 Autopilot Effort Indicators ..................................................................................... 16-7
16-10 Flight Director Panels ............................................................................................ 16-9
16-11 ADI and HSI Symbology..................................................................................... 16-10
16-12 Altimeter System ................................................................................................. 16-12
16-13 Air Data Panel...................................................................................................... 16-13
16-14 Air Data Panel Indications ................................................................................... 16-14
16-15 Air Data Display Unit (ADDU)........................................................................... 16-14
FOR TRAINING PURPOSES ONLY
LEARJET 20 SERIES PILOT TRAINING MANUAL
FlightSafety
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