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To be used for navigation, the FMS must be receiving suitable navigation
information from the following sources:
• One VOR / DME, or
• Two DMEs, or
• GPS. If the GPS is the only available sensor, use of the FMS for
navigation is not approved unless the Collins prediction program
[832-3443-007, or later applicable version] has been run.
IFR enroute and terminal navigation is prohibited unless the pilot verifies the
currency of the database or verifies the waypoints for accuracy by reference to
current publications.
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 instrument approaches is prohibited unless APPR is annunciated
on the PFD.
(Continued)
For aircraft 20002 thru 20050 not incorporating Service Bulletin 100-11-01
(Replacement of Airspeed Limits Placard for MTOW Increase to 38 850 lb/
17 622 kg):
The performance database part number must be verified as: 815-5959-001.
EFFECTIVITY
LIMITATIONS
DOT Approved Jul 31/2006 Airplane Flight Manual 02-04-05
REV 6 CSP 100-1
SYSTEMS LIMITATIONS (Cont)
AVIONICS (Cont)
FLIGHT MANAGEMENT SYSTEM (Cont)
Use of VNAV vertical guidance for 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 co-ordinate data system for the instrument approach is WGS-84 or
NAD-83.
When the altimeter is adjusted to show the Height Above Ground (QFE) rather
than sea level, VNAV must not be used.
FMS range and fuel management information is advisory only.
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. 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.
Approval Status:
Provided the FMS is receiving adequate usable signals, the FMS has been
demonstrated capable of and has been shown to meet the performance requirements
for the following operations:
Lateral Navigation — VFR/IFR enroute oceanic and remote, enroute domestic,
terminal operation, and instrument approach using WGS-84 (or NAD 83)
coordinate reference datum in accordance with the performance/accuracy
requirements of AC20-130A.
(Continued)
LIMITATIONS
02-04-06 Airplane Flight Manual DOT Approved Jul 31/2006
CSP 100-1 REV 6
SYSTEMS LIMITATIONS (Cont)
AVIONICS (Cont)
FLIGHT MANAGEMENT SYSTEM (Cont)
Primary Means Oceanic and Remote — Use of the FMS with GPS has been
found to comply with the requirements of FAA Notice 8110.60 for GPS primary
means of navigation in oceanic and remote airspace, when used in conjunction
with the Collins prediction program 832-3443-005 and with two
operational GPS receivers and with two operational FMS systems.
NAT MNPS — Provided dual FMS and dual GPS are installed and operating,
the FMS with GPS inputs has been demonstrated capable of flight into North
Atlantic (NAT) minimum navigation performance specification (MNPS) and
has been shown to meet the accuracy specification in accordance with AC 120-
33 or AC 91-49.
P-RNAV — The FMS installation has been demonstrated to meet the P-RNAV
requirements of JAA TGL 10, provided the operator implements navigation
database integrity checks using appropriate software tools or approved procedures
as per TGL 10 section 10.6.
RNP-5/BRNAV — This FMS installation has been demonstrated to meet the
RNP-5 airspace (BRNAV) requirements of AC 90-96 and JAA AMJ 20X2
Leaflet 2, Revision 1.
RNP-10 — Provided dual FMS and dual GPS are installed and operational,
this FMS installation with GPS with RAIM has been demonstrated to meet the
　
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