Honeywell GNS-XLS Operator's Manual page 367

DISPLAY MSG: The DISPLAY AFIS MSG Page is accessed here.
For a detailed discussion of this page, see
WGT/BAL PAGE FOR J32
AIRCRAFT CONFIGURA-
TION
J32 aircraft weight and bal-
ance information for a specific
flight is entered on this page.
See Figure 8-46. Any enter-
able field may be left blank.
20:11: UTC hours and min-
utes.
FUEL: Pounds of fuel on
board. Input range is 0 to 3248 pounds. Entry is checked against
maximum limit.
TAXI: Pounds of fuel (estimated) for taxi. Input range is 0 to 999
pounds.
BURN: Pounds of fuel burn-off (estimated) for the flight. Input
range is 0 to 3248 pounds. Entry is checked against maximum
limit.
P ALT: Current pressure altitude at departure airport. Input range
is 0 to 9999.
MTOW: Maximum takeoff weight in pounds. Input range is 0 to
16204.
ROW: Row numbers.
ADULT: Number of adult passengers in row. Input range for each
entry is 0 - 3 for rows 1 through 6 and 0 - 1 for row 7. Sum of adults
plus children must not exceed the maximum value for the row. If
the maximum value for the row is exceeded, both fields will blink
and the entry will not be accepted. An * may be entered in the first
ADULT field to indicate all seats are filled by adults. No other
entries are needed.
CHILD: Number of child passengers in row. Input range for each
entry is 0 - 3 for rows 1 through 6 and 0 - 1 for row 7. Sum of adults
plus children must not exceed the maximum value for the row. If
the maximum value for the row is exceeded, both fields will blink
and the entry will not be accepted.
Rev 8
GNS-X
Apr/00
20:11
<
FUEL 1300
TAXI
<
BURN
P ALT2992
<
MTOW15189
ROW
<
ADULT 2123021
CHILD 1210310
<
FMS with Regional Airline AFIS
LS
Section 7.
WGT BAL
&
AFT WT130
80 POD WT 50
800 CLSTWT 10
TEMP C+28
1234567
TRANSMIT
Figure 8-46
>
>
>
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8-37