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LIMITATIONS Navigation Systems Limitations Vol. 1 02.09.1
REV 1, Dec 21/06
1. FLIGHT MANAGEMENT SYSTEM
The flight management system (FMS) must be operated in accordance with the latest edition of the following;
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Airplane Flight Manual, and
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Flight Management System FMS–6000 Pilot’s Guide, part number 523–08007938–001117 or later applicable revision.
The FMS is approved for use only with the SCID 832–4117–094 (no SAR) or SCID 832–4117–095 (with SAR) software program versions or later applicable revisions.
FMS database information must be verified as being current. Waypoints must be checked for 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;
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One VOR/DME, or
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Two DMEs, or
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One inertial reference system (IRS), or
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GPS, if GPS is the only available sensor. Use of FMS for navigation is not approved unless the Collins prediction program 832–3443–008, or later applicable version, has been run. Airplane operation must not be predicated upon performance data; ETE/ETA and fuel remaining.
FMS flight plans must be identical when conducting dual FMS approach operations.
Use of FMS instrument approaches past the Final Approach Fix is prohibited, unless APPR is
annunciated on the PFD.
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. 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.
Use of VNAV vertical guidance for a V-MDA type approach between the final approach fix and the missed approach fix is prohibited.
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.
LIMITATIONS Navigation Systems Limitations Vol. 1 02.09.2
REV 1, Dec 21/06
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本文链接地址：庞巴迪挑战者605公务机机组操作手册 CL605-CHAPTER 2 -限制 LIMITATIONS(18)
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