EasyManua.ls Logo

FlightSafety LEARJET 45 - Page 110

Default Icon
539 pages
Print Icon
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Loading...
LEARJET 45 PILOT TRAINING MANUAL
4-17
FOR TRAINING PURPOSES ONLY
FlightSafety
international
Chpt CAS Message Logic Summary
T/O
Inhibit
Land
Inhibit
1 NO NOAny main entry door pin not closed
1
1
NO NO
NO NO
Emergency escape hatch exit not fully latched
Tailcone or baggage door not fully latched
YES YES
Any pin not in agreement with the door open, ground only
NO NO
6
6
APU fire detected
NO NO
7 Low oil pressure, < 50 psi
L R OIL PRESS LOW
L R ENGINE CHIP
L R ENGCMPTR FAULT
L R FUEL PRESS LOW
L R ENG FIRE FAIL
L R OIL FILTER
L R ENGCMPTR FAULT
L R FUEL HEATER
L R APR FAULT
L R CHECK EDS
L R ENGINE CHIP
L R FUEL FILTER
L R ENG SHUTDOWN
L R ENG VIB MON
L R OIL FILTER
L R FUEL FILTER
L R FUEL HEATER
1
APU amps > 300
NO NO
Low pressure to engine fuel pump inlet (< 1 psi)5/7
YES YES
Metal particles detected in oil (ground)7
ENTRY DOOR
EMERGENCY EXIT
EXTERNAL DOORS
ENTRY DOOR PIN
APU FIRE
APU AMPS HIGH
NO NO
DEEC fault7
YES YES
Fuel/oil cooler failure – fuel too cold
5/7
YES YES
Oil filter has an impending bypass (ground)7
YES YES
Fire sensing element shorted (ground)7
YES YES
Engine/airframe fuel filter impending bypass (ground)7
YES YES
DEEC has detected minor malfunction (ground)7
Metal particles in oil (inflight)7
YES YES
Engine/airframe fuel filter impending by-pass (inflight)7
YES YES
Collector msg for fuel/oil/hyd press/gen fail, enabled by TL cutoff7
NO NO
YES YES
EDS has lost power, EDS built-in-test equipment (BITE)
has detected a system failure, the EDS memory is 85%
full, or the system has detected an engine condition
which is out of acceptable parameters
7
YES YES
Fuel/oil cooler failure – fuel too hot5/7
YES YES
L or R detected APR fault7
YES YES
6
APU fault/fail
APU FAIL
YES YES
6
APU is operating and ready for load
APU AVAILABLE
YES YES
DOORS
APU
ENGINE
Engine vibration beyond preset G limits7
NO NO
Engine oil filter impending by-pass (inflight)7
YES YES
L R ENG FIRE FAIL
Engine fire sensing element is shorted (inflight)7
YES YES
Table 4-2.7. CWP/CAS MESSAGE SUMMARY (CONT)

Table of Contents