EasyManua.ls Logo

Thales FMGS - Page 352

Thales FMGS
703 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...
36
MULTIPHASE
LATERAL F-PLN management
J43126AA 00
© THALES AVIONICS S.A.
AIRBUS A318/319/320/321
When DIR TO is inserted:
If HDG is not correct
for FMS intercept (INTCPT) computation:
"NO NAV INTERCEPT" s-pad msg (white) is displayed.
HDG should be adjusted.
If HDG is correct for FMS intercept (INTCPT) computation:
"ADJUST DESIRED HDG/TRK" s-pad msg (amber) is displayed
F-PLN page
First line: FROM waypoint is named IN-BND,
TO WPT is the selected DIR TO WPT.
In the example, since AMB is not in ACTIVE F-PLN, it is followed by a
F-PLN DISCONTINUITY.
See below for Lateral Guidance and INTCPT computation.
FROM THV001 {}
UTC SPD/ALT
IN-BND 1520 / -----
BRG009° 116
AMB 1537 " / "
---F-PLN DISCONTINUITY--
ADABI 1545 .79/ "
UN874 30NM
BOKNO 1549 " / "
DEST UTC DIST EFOB
EGLL27R 1625 512 4.3
ADJUST DESIRED HDG/TRK£$
FROM THV001 {}
UTC SPD/ALT
IN-BND 1520 / -----
BRG009° 121
AMB 1537 .79/ FL360
---F-PLN DISCONTINUITY--
ADABI 1545 .79/ "
UN874 30NM
BOKNO 1549 " / "
DEST UTC DIST EFOB
EGLL27R 1625 517 4.3
NO NAV INTERCEPT £$

Table of Contents