曝光臺(tái) 注意防騙 網(wǎng)曝天貓店富美金盛家居專營(yíng)店坑蒙拐騙欺詐消費(fèi)者

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 GPS is approved for supplemental means 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.
− The FMS database integrity does not meet the integrity requirements of TGL 10
section 8.2, therefore during Precision RNAV Operations, waypoints must be verified
as per TGL section 10.6.
− 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.
• The demonstration of performance with the above criteria does not constitute approval to
conduct terminal airspace PRNAV operations.
LIMITATIONS
NAVIGATION SYSTEMS
REV 53, Jan 29, 2007 Flight Crew Operating Manual
CSP 700−6
Volume 1
02−09−5
1. NAVIGATION SYSTEMS (CONT'D)
B. Flight Management System − Batch 1 IAC airplanes only <NZ5.2 on FMS CDU “NAV
IDENT” page> (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.
• The demonstration of performance with the above criteria does not constitute any
required operational approval to conduct MNPS, oceanic / remote airspace RNP−5 or
RNP−10 operations.
• 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 demonstration of performance with the above criteria does not constitute
any required operational approval to conduct VNAV operations.
− The VNAV system information is not temperature compensated. FMS generated
altitude and V-paths are not corrected for non-ISA conditions.
− Use of VNAV vertical guidance is prohibited when the barometric altitude is corrected
to the landing field elevation (QFE operation).
− While using VNAV vertical guidance, all flight plan changes must be initiated to the
coupled FMS.
NOTE
In DUAL or INITIATED TRANSFER mode, flight plan
changes that affect the vertical path made on one FMS
may not synchronize properly on the crosside FMS
resulting in an offset in the vertical path between the two
FMSs. Accomplishing a vertical DIRECT−TO on either
FMS will resolve this offset.
LIMITATIONS
NAVIGATION SYSTEMS
Flight Crew Operating Manual REV 53, Jan 29, 2007
CSP 700−6
Volume 1
02−09−6
　
中國(guó)航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：Bombardier_Global_Express_XRS-Limitations(15)