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时间:2010-03-23 19:57来源:蓝天飞行翻译 作者:admin
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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
DOT Approved
REV 53, Jan 29, 2007
Airplane Flight Manual
CSP 700−1A
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).
LIMITATIONS
NAVIGATION SYSTEMS
DOT Approved
REV 53, Jan 29, 2007
Airplane Flight Manual
CSP 700−1A
02−09−3
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)
• The demonstration of performance with the above criteria does not constitute any
required operational approval to conduct MNPS, terminal airspace PRNAV, U.S. RNAV
Q−Routes, Type A and Type B RNAV SIDs and STARs, oceanic / remote and terminal
airspace RNP−5 and RNP−10, or VNAV operations.
B. Flight Management System − Batch 1 IAC airplanes only <NZ5.2 on FMS CDU “NAV
IDENT” page>
• The flight management system (FMS) must be operated in accordance with the latest
edition of the following:
(1) Airplane Flight Manual, and
(2) Honeywell Flight Management System FMZ Pilot’s Operating Manual, publication
number A28−1146−155−00, dated September 2000 or latest applicable revision.
(3) For airplanes 9125 and subsequent, and airplanes 9002, 9004 thru 9124
incorporating Service Bulletin 700−34−025, Honeywell Flight Management System
 
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