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holding pattern fix.
The RTE HOLD page is used by the flight crew to enter and
review data for a specific holding pattern.
Page Access
The RTE LEGS HOLD AT page is accessed from the RTE LEGS
page by selecting the HOLD mode key on the MCDU.
The RTE HOLD page is accessed from the HOLD AT page by:
* Entering HOLD AT XXXXX in the scratchpad and selecting
LSK 6L
* Entering the holding pattern fix waypoint in line 6L and
selecting LSK 6L
* Entering PPOS at line 6R and selecting LSK 6R.
Rte Legs Hold At Page Information
Line select keys 1L through 5L show the active waypoint and
subsequent waypoints in the active flight plan with this data:
* Computed course to waypoint
* Computed leg length
* Speed and altitude.
Line select key 6L shows the HOLD AT box prompts. The flight
crew enters the desired waypoint for the holding pattern fix
point.
Line select key 6R shows the PPOS prompt. The flight crew
enters the desired position for the holding pattern fix point.
Rte Hold Page
Line select key 1L shows the FIX data. This is the holding
pattern fix point as defined on the HOLD AT page.
SHZ 001-003 PRE SB 737-34-1666; SHZ 009-999 PRE SB
737-34-1666 AND PRE SB 737-34-1918
Line select key 2L shows QUAD/RADIAL prompt. This data field
shows the holding quadrant and radial of the holding pattern. It
is entered through the MCDU.
Line select key 3L shows the INBD CRS/DIR prompt. This data
field shows the inbound course and the direction of the holding
pattern. It is entered through the MCDU or contained in the
navigation data base.
SHZ ALL
Line select key 4L shows the LEG TIME prompt. The leg time is
entered through the MCDU. The default times are 1.5 minutes
above 14000 feet and 1.0 minutes at or below 14000 feet.
FMCS - DISPLAYS - CDU - HOLD PAGE
EFFECTIVITY
SHZ ALL 34-61-00
Page 98.75
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737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
34-61-00-074
Line select key 5L shows the LEG DIST (leg distance) prompt.
This data field lets the flight crew enter the leg distance for the
holding pattern.
Line select key 6L shows one of these prompts:
* NEXT HOLD (selects the HOLD AT page)
* ERASE (shows when data is being modified).
SHZ 001-003 PRE SB 737-34-1666; SHZ 009-999 PRE SB
737-34-1666 AND PRE SB 737-34-1918
Line select key 1R shows the SPD/TGT ALT prompt. This data
field shows the best speed and altitude for the holding pattern. It
is entered through the MCDU or contained in the NDB.
SHZ ALL
Line select key 2R shows the FIX ETA prompt. This data field
shows the time at which the holding pattern fix is reached.
Line select key 3R shows the EFC TIME prompt. This data field
shows the time at which the holding pattern is exited.
Line select key 4R shows the HOLD AVAIL prompt. This data
field shows the holding time available before exit is necessary
to reach the destination with the necessary fuel reserves.
Line select key 5R shows the BEST SPEED prompt. This data
field shows the best holding speed for the current altitude and
conditions.
Line select key 6R shows the EXIT HOLD prompt. This data field
shows when the airplane is in an active holding pattern. After
selection of this prompt, the EXEC key lights and EXIT HOLD is
replaced with EXIT ARMED. When the EXEC key is pushed, the
airplane exits the holding pattern from the FIX point and
resumes the active flight plan.
FMCS - DISPLAYS - CDU - HOLD PAGE
EFFECTIVITY
SHZ ALL 34-61-00
Page 98.76
D633A101-SHZ1 Jun 10/2007
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
34-61-00-074
FMCS - DISPLAYS - CDU - HOLD PAGE
FMCS - DISPLAYS - CDU - HOLD PAGE
EFFECTIVITY
SHZ ALL 34-61-00
Page 98.77
D633A101-SHZ1 Jun 10/2003
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
34-61-00-074
THIS PAGE IS INTENTIONALLY LEFT BLANK
FMCS - DISPLAYS - CDU - HOLD PAGE
34-61-00
Page 98.78
D633A101-SHZ1 Oct 10/2003
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
General
The FIX INFO page is used by the flight crew to show the current
bearing and distance from a selected reference point (SRP). It is
also used to calculate the abeam point of the airplane along the
flight plan route from the entered SRP.
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