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• The FMS is approved for use with software program version NZ5.8 as displayed on the
FMS CDU “NAV IDENT” page 1/1.
• If a difference exists between the AFM and the Honeywell FMS Pilot’s Operating Manual,
the AFM shall take precedence.
• Use of the FMS database for IFR is prohibited unless the database is current or the pilot
verifies waypoints for accuracy by reference to current publications.
• The FMS must not be used as a navigation source unless it is receiving suitable
navigation information from the following:
− One VOR /DME, or
− Two DMEs, or
− One inertial reference system.
• The flight plans on the paired FMSs must be identical when conducting FMS approaches.
• Instrument approaches must be accomplished only in accordance with instrument
approach procedures that are contained in the FMS database. The database must
incorporate the current update cycle. The pilot must verify approach waypoints for
accuracy by reference to current publications.
• Use of FMS as a sole NAV source for instrument approaches past the Final Approach Fix
is prohibited unless APP is annunciated on the PFD.
• Fuel display parameters are advisory only, and must not be used to replace primary fuel
quantity or fuel flow indications for fuel load and range planning.
• The aircraft must have other approved navigation equipment, appropriate to the route,
installed and operating.
• Use of FMS as the PFD NAV SRC ILS, LOC, LOC−BC, LDA, SDF and MLS approaches
beyond the Final Approach Fix is prohibited.
• Capture and tracking of DME arcs outside of the published end points of an approved IFR
procedure is prohibited.
• The GPS sensor(s) must be deselected when on approach in airspace not referenced to
WGS−84 or NAD−83.
• GPS updating is not approved when other navigation sensors are deselected, inoperative
or in any other way not providing accurate navigation data to the FMS.
LIMITATIONS
NAVIGATION SYSTEMS
DOT Approved
REV 53, Jan 29, 2007
Airplane Flight Manual
CSP 700−1A
02−09−1
1. NAVIGATION SYSTEMS (CONT'D)
A. Flight Management System − Batch 2 IAC and Batch 2+ IAC airplanes only <NZ5.8 on
FMS CDU “NAV IDENT” page> (Cont’d)
• Before compliance with any ATC clearance or instruction which is displayed by the
datalink, the ATC clearance or instruction must be independently verified with the
originating ground station.
• The FMS has been demonstrated capable of and has been shown to meet the
requirements of the following:
− North Atlantic Tracks (NAT) Minimum Navigational Performance Standards (MNPS)
Airspace
− Providing two FMS installations are operating with each receiving information
from at least two inertial reference systems, the FMS has been demonstrated
capable of flight into NAT MNPS airspace and has been shown to meet the
accuracy specification in accordance with AC 120−33 or AC 91−49.
− GPS Enroute, Terminal and Approach Navigation
− Use of the FMS with the GPS is approved for supplemental means of navigation
source for enroute and terminal operations. GPS-only approaches are
approved.
− Precision RNAV
− The FMS installation meets the airworthiness certification requirements of JAA
Temporary Guidance Leaflet No. 10, Airworthiness and Operational Approval
for Precision RNAV Operations in Designated European Airspace.
− When in Precision RNAV Operations, Pilot is to monitor lateral deviation
indicator on MFD. The maximum value of lateral deviation permitted on the
digital deviation display on the MFD in MAP mode is +/− 0.5 nm cross track
error.
− GPS is required for takeoff in Precision RNAV airspace.
− If equipped with Laseref III, Precision RNAV operations with only IRS position
for more than seven (7) minutes is prohibited.
− If equipped with Laseref IV, Precision RNAV operations with only IRS position
for more than twenty (20) minutes is prohibited.
− Compliance with AC 90−100 U.S. Terminal and Enroute Area Navigation (RNAV)
Operations
− When equipped with an operating FMS and GPS, the aircraft meets the
functional +/− 1.0 nm accuracy requirements of AC 90−100 U.S. Terminal and
Enroute RNAV Operations.
− When in U.S. Terminal and Enroute RNAV Operations, Pilot is to monitor lateral
deviation indicator on MFD. The maximum value of lateral deviation permitted
on the digital deviation display on the MFD in MAP mode is +/− 0.5 nm cross
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Bombardier LIMITATIONS(12)
