787 Flight Crew Operations Manual
DO NOT USE FOR FLIGHT
Supplementary Procedures -
Electrical
Copyright © The Boeing Company. See title page for details.
SP.6.2 D615Z003-TBC
Electrical Power Up
The following procedure is accomplished to permit safe application of
electrical power.
Note: Electrical power initialization is described in Chapter 1,
Airplane General (Refer to Common Core System
in Chapter 1,
Section 40, for additional information.).
BATTERY switch .............................................................................. ON
C1 and C2 ELEC pump selectors .....................................................OFF
DEMAND pump selectors ................................................................OFF
WIPER selectors ...............................................................................OFF
Landing gear lever.............................................................................. DN
ALTN FLAPS selector ......................................................................OFF
Electrical power ........................................................................ Establish
If external power is desired:
EXT PWR AVAIL light(s) – Illuminated
EXT PWR switch(es) – Push
If APU power is desired:
APU GENERATOR switches – ON
Note: Prior to APU start, confirm that the left CCR is online
(indicated by the captain’s inboard and lower display unit
showing the default formats.)
APU selector – START, then ON
February 15, 2010
To Next Page
Loading...
