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CSP 700−5000−6
Volume 1
02−09−1
1. NAVIGATION SYSTEMS (CONT'D)
A. Flight Management System (Cont’d)
• 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.
• 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
track error.
LIMITATIONS
NAVIGATION SYSTEMS
Flight Crew Operating Manual REV 14, Jan 29, 2007
CSP 700−5000−6
Volume 1
02−09−2
1. NAVIGATION SYSTEMS (CONT'D)
A. Flight Management System (Cont’d)
− BRNAV / RNP−5
− The FMS installation meets the requirements of RNP−5 in accordance with AC
90−96, Approval of US Operators and Aircraft to Operate under Instrument
Flight Rules (IFR) in European Airspace Designated for Basic Area Navigation
(BRNAV / RNP−5) and JAA Temporary Guidance Leaflet No. 2, rev. 1, AMJ
20X2, JAA Guidance Material on Airworthiness Approval and Operational
Criteria for the use of Navigation Systems in European Airspace Designated for
Basic RNAV Operations. In addition, the FMS installation has received
airworthiness approval in accordance with Advisory Circular AC 20−130A.
− RNP 10
− The FMS installation with the IRS has been demonstrated to meet the criteria of
FAA Order 8400.12A “Required Navigation Performance 10 (RNP−10)
Operational Approval” as a primary means of navigation for flight up to 6.2
hours in duration without updating. The determination of flight duration starts
when the system is placed in the navigation mode.
− The FMS with the GPS with RAIM has been demonstrated to meet the criteria
of FAA Order 8400.12A “Required Navigation Performance 10 (RNP−10)
Operational Approval” as a means of navigation for flights without time
limitations when a second GPS is installed.
− VNAV
− The VNAV vertical guidance has been demonstrated capable of and has been
shown to meet the accuracy requirements of VFR/IFR enroute, terminal and
approach VNAV operations in accordance with the criteria of AC20−129.
− The use of VNAV temperature compensation in the “HOT & COLD” mode is
　
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