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accuracy prior to use.
Use of pilot defined FMS approaches, in instrument meteorological conditions, is prohibited.
The FMS must not be used for navigation unless it is receiving suitable navigation information
from the following sources:
• One VOR/DME, or
• Two DMEs, or
• One inertial reference system (IRS), or
• GPS (if installed). If GPS is the only available sensor, use of FMS for navigation is not
approved unless an appropriate RAIM availability prediction program has been run. Refer to
Collins FMS and Database Services for the latest applicable prediction program.
Airplane operation must not be predicated upon performance data; ETE/ETA and fuel remaining.
On airplanes 5301 to 5499 NOT incorporating Service Bulletin 604–34–031:
The FMS latitude limits are ±80°.
FMS flight plans must be identical when conducting dual FMS approach operations.
LIMITATIONS
Navigation Systems Limitations
02−09−1
REV 75, Feb 17/09
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. FLIGHT MANAGEMENT SYSTEM (CONT'D)
Use of FMS instrument approaches past the Final Approach Fix is prohibited, unless APPR is
annunciated on the PFD.
Use of VNAV vertical guidance for a V-MDA type approach between the final approach fix and
the missed approach fix is prohibited.
CAUTION
Errors to VNAV defined paths may occur because of coding errors in
the navigation data base and because of altimetry errors. The actual
VNAV path may deviate significantly below the intended VNAV path in
very cold temperatures, unless an approved temperature compensation
function (if equipped) is used to correct for non−standard temperatures.
Database coding of VNAV altitudes for approach waypoints may result
in VNAV paths continuing below Minimum Descent Altitude (MDA),
Decision Altitude (DA), or Decision Height (DH), or ending at an altitude
too high to continue a safe descent to landing. Baro VNAV paths (often
called pseudo−glide paths) are not equivalent to an ILS glideslope.
Position along an approach must be verified prior to commencement of
VNAV descent, as displayed by the FMS. The required visual reference
must be obtained prior to commencing descent below published MDAs,
DAs, or DHs.
On airplanes 5301 to 5499 NOT incorporating Service Bulletin 604–34–031:
Capture and tracking of DME arcs outside of the published end points of an approved IFR
procedure is prohibited.
Use of VNAV raw data without a flight director is prohibited.
Use of VNAV data with a non FMS mode is prohibited.
Use of VNAV in missed approach procedures is prohibited.
Editing of the runway extension waypoint distance during visual approach while it is the active
leg, is prohibited.
Editing the fuel quantity on the FUEL MGMT page is prohibited.
Automatic transition from FMS to ILS (NAV to NAV capture) is prohibited when in DCP
reversion.
The FMS with inputs from GPS may only be used for approach guidance if the reference
coordinate data system for the instrument approach is WGS–84 or NAD–83.
On airplanes 5301 to 5560 NOT incorporating Service Bulletin 604–31–015 or 604–34–031
Rev 1 or later revision:
Navigation must not be predicated on the expanded localizer displayed on the PFDs.
LIMITATIONS
Navigation Systems Limitations
02−09−2
REV 71, Oct 31/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. FLIGHT MANAGEMENT SYSTEM (CONT'D)
On airplanes 5500 and subsequent and airplanes incorporating Service Bulletin
604–34–031:
The FMS thrust setting data is the primary means of information provided two air data
computers are available.
The FMS V speed data is the primary means of information provided two flight management
computers are available.
LBA Certified Airplanes
Thrust setting data and V speed data must be determined using the performance data
contained in this AFM and not using the FMS.
AR Certified Airplanes
The FMS V speed data is advisory only.
The following V speed database must be verified to be current and valid:
ALL REGISTRIES
EXCEPT FAA FAA REGISTRY
Airplanes 5301, 5303 to 5639
without SB 604–11–001
part number
815–2055–002
part number
815–2057–002
Airplanes 5302, 5640 and Subs and Airplanes
5301, 5303 to 5639 with SB 604–11–001
part number
815–2054–002
part number
815–2056–002
On airplanes NOT incorporating Service Bulletin 604–34–035:
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庞巴迪挑战者604飞机飞行手册CL604 Airplane Flight Manual 1(56)
