曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

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.
− 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.
LIMITATIONS
NAVIGATION SYSTEMS
Flight Crew Operating Manual REV 53, Jan 29, 2007
CSP 700−6
Volume 1
02−09−2
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)
− 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.
Effectivity:
• Airplanes 9002 thru 9153 not incorporating Service Bulletin:
• SB 700−31−021, Integrated Avionics Computers (IAC) − Batch 2 IAC Upgrade.
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 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.
− 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
prohibited.
− The VNAV temperature compensation is per Section 9.18.1 of Transport
Canada Aeronautical Information Publication (AIP).
− Use of VNAV vertical guidance is prohibited when the barometric altitude is
corrected to the landing field elevation (QFE operation).
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：Bombardier_Global_Express_XRS-Limitations(13)