Honeywell GNS-XL - Manual (Page 131)

System Operation
3-17a GNS-X L Flight Management System
Rev. 4
Nov/04
4. Select the FMS as the NAV source.
5. The FMS will fly the remainder of the SID to HQM.
NOTE: This is known as the FMS HEADING/INTERCEPT proce-
dure.
Overfly then Intercept Procedures
For procedures that require over-flying a waypoint (Figure 3-21a),
then a turn to intercept a course to the next waypoint, follow these
operational requirements for the example following:
1. Prior to departure, when the first waypoint is designated fly-over,
select MAN leg change mode on NAV Page 1 and press
ENTER
.
2. Select the FMS as the NAV source.
3. Accurately fly the runway course or heading.
4. Immediately after passing ZH582, do a Direct To ZH554, enter
255 in the DTK field on NAV Page 1 and press ENTER.
NOTE: This is known as the FMS Pseudo Vortac procedure.
250° hdg
227°
226°
D RD46°
18000
33
HOQUIAM
(ELMAA5.HQM)
SEATTLE-TACOMA
INTL 429
ELMAA
N47 08.9 W123 24.5
D5
158°
At or above
3000'
SEATTLE
ELMAA 5 DEPARTURE
116.8 SEA
NAA7 26.1 W122 18.5
D
(H)
HOQUIAM
117.7 HQM
N46 56.8 W124 08.9
D
(H)
This SID requires a mnimum climb gradiant of:
Rwys 16 L/R: 550' per nm to 3000'.
TAKE OFF
Rwys 16L/R: intercept and proceed via Seattle
R-158, cross Seattle 5 DME fix at or above 3000'
then turn RIGHT to 250 heading to intercept
and proceed via Seattle R-277 to Elmaa Int,
then via (transition) or (assigned route).
TRANSITION
Hoquiam (ELMAA5.HQM): From Elmaa Int to
Hoquiam VORTAC(33nm): Via Hoquiam R-046.
THIS CHART: FOR ILLUSTRATION PUPOSES ONLY
Heading mode or Manual required
Figure 3-20