737 Flight Crew Operations Manual
Normal Procedures -
Amplified Procedures
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
D6-27370-866-EGP NP.21.11
Verify that the standby hydraulic LOW QUANTITY light is
extinguished.
Verify that the standby hydraulic LOW PRESSURE light is
extinguished.
Verify that the STBY RUD ON light is extinguished.
ALTERNATE FLAPS master switch – Guard closed
ALTERNATE FLAPS position switch – OFF
Verify that the FEEL DIFF PRESS light is extinguished.
Verify that the SPEED TRIM FAIL light is extinguished.
Verify that the MACH TRIM FAIL light is extinguished.
Verify that the AUTO SLAT FAIL light is extinguished.
NAVIGATION panel ...........................................................................Set
VHF NAV transfer switch – NORMAL
IRS transfer switch – NORMAL
FMC source select switch – NORMAL
DISPLAYS panel .................................................................................Set
SOURCE selector – AUTO
CONTROL PANEL select switch – NORMAL
Fuel panel ............................................................................................Set
Verify that the ENG VALVE CLOSED lights are illuminated dim.
Verify that the SPAR VALVE CLOSED lights are illuminated dim.
Verify that the FILTER BYPASS lights are extinguished.
CROSSFEED selector – Closed
Verify that the VALVE OPEN light is extinguished.
FUEL PUMP switches – OFF
Verify that the center tank fuel pump LOW PRESSURE lights are
extinguished.
Verify that the main tank fuel pump LOW PRESSURE lights are
illuminated.
Electrical panel ....................................................................................Set
BATTERY switch – Guard closed
CAB/UTIL power switch – ON
September 15, 2016
To Next Page
Loading...
