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FlightSafety LEARJET 45 - Page 30

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ILLUSTRATIONS (CONT.)
Figure Title Page
2-24 System with Double Generator Failure (In Flight) ................................................ 2-37
2-25 Emergency Power Supply System ......................................................................... 2-38
TABLES
Table Title Page
2-1 Electrical Limits ..................................................................................................... 2-14
2-2 CAS Message Database and Logic Summary ....................................................... 2-17
2-3 Normal Contactor Operation.................................................................................. 2-19
2-4 DC Power Distribution with Double Generator Failure ........................................ 2-39
2-5 Abnormal Contactor Operation.............................................................................. 2-40
LEARJET 45 PILOT TRAINING MANUAL
2-iv
FOR TRAINING PURPOSES ONLY
FlightSafety
international

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