Learjet 35 - Page 34

2B-10 Developed for Training Purposes Leerjet 35/36
February 2007
CAE SimuFlite
Crossflow Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPEN
Check that the amber disagreement light cycles properly,
the right low fuel pressure annunciator extinguishes, and
fuel crossflow annunciator illuminates.
Right Standby Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
Ensure light in switch (if applicable) illuminates.
Left Standby Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
Both fuel pressure annunciators remains extinguished and
light in switch (if applicable) extinguishes.
Crossflow Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSE
The left fuel pressure annunciator illuminates.
Right Standby Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
Right low fuel pressure annunciator illuminates.
Crossflow/XFER-FILL/FUS VAL Switches . . . . . . . CLOSED/
.................................................................... ........... OFF/OFF
If external power not used:
One Engine. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . START
Go to Engine Start in Starting Engines checklist, page
2B-28.
Warning Systems Check. . . . . . . . . . . . . . . . . . COMPLETED
Test the warning system using the rotary test switch.
Cabin Altitude Warning:
Rotary Test Switch . . . . . . . . . . . . . . . . . . . . . . . . CABIN ALT
Test Button . . . . . . . . . . . . . . . . . . . . . . . . . DEPRESS/HOLD
The cabin altitude warning horn sounds.
Horn Silence Switch . . . . . . . . . . . . . . . . ON MOMENTARILY
The cabin altitude warning horn ceases for approximately 60
seconds.
Test Button . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .RELEASE
Mach Warning/Stick Puller:
Rotary Test Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . .MACH