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Inflight Accuracy Checks ......................................................5-111
Check Distance/Radial from a Known Position .................... 5-111
Check or Change Distance/Radial of Pilot Waypoint
from REF WPT .....................................................................5-112
Best Computed Position Update .......................................... 5-113
Sensor Computed Position Update ...................................... 5-114
FUEL AND PERFORMANCE..................................................... 5-115
Introduction ..............................................................................5-115
FUEL MANAGEMENT................................................................ 5-116
FUEL OPTIONS Page ............................................................. 5-116
FUEL Page 1............................................................................ 5-117
FUEL Page 2............................................................................ 5-119
FUEL Page 3............................................................................ 5-121
FUEL Page 4............................................................................ 5-122
FUEL Page 5............................................................................ 5-124
PERFORMANCE........................................................................ 5-125
PERF Page 1 ........................................................................... 5-125
ABNORMAL PROCEDURES..................................................... 5-127
Engine Failure/Shutdown......................................................... 5-127
Power Failure (Inflight Initialization)......................................... 5-128
Power Failure For Up To Seven Minutes ............................. 5-128
Power Failure For Over Seven Minutes ............................... 5-130
NAV Sensor Accuracy Messages............................................ 5-131
Section V
Operations
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INTRODUCTION
This section of the manual contains those FMS flight operating
procedures designed to be used on a typical flight and are arranged
in the order they would normally employed. This section also
contains procedures, which may be used in the event of an electrical
power failure, engine shutdown, or fuel flow system failure.
NOTE: Given the capabilities and versatility of the FMS, many
programming options are available to the pilot through
which the same results can be achieved. This section
does not discuss all the possible programming options for
each operation.
NOTE: Some differences may be observed between FMS
displayed courses and those published on aeronautical
charts. These differences are due to the fact that the
charts are published using the VOR radials that define the
route, whereas the FMS displays the computed course
using local magnetic variation. FPL legs with XXX°
displays may vary from the published data by the amount
of difference between the defining VOR facility declination
(i.e., the angle formed between the VOR 0° radial and
True North) and the magnetic variation at the originating
waypoint. Mag variation constantly shifts with time,
whereas the station declination is constant until the station
is realigned. Station declination may vary by several
degrees from local mag variation, depending upon how
long ago the station was realigned with local variation.
Legs that have CRS XXX° or HDG XXX° displays on the
FPL pages should agree with the published data on the
charts, since these are provided as part of the navigation
data base and are not computed by the FMS.
Section V
Operations
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Change 1
Intentionally left blank
Section V
Operations
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Change 1
PRE-DEPARTURE
Start-Up
1. Press the ON/OFF key to activate the system. The system will
come on and will self test. The self-test page will be displayed
showing the results of each test performed. If the self test is
successful, the Initialization page will appear. The line at the top
of the page will indicate the name of the aircraft as programmed
in the Configuration Module.
NOTE: Should a failure message appear while the system is
going through self test, one of the following will occur:
• The self test page will not disappear if a serious failure of
the FMS occurs.
• Failures of a minor nature will allow the pilot to continue
with the initialization process after alerting the pilot of the
failure. Press the MSG key to view the message. No
other page, except the MSG page, may be viewed until
the initialization process is completed.
　
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