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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
DOT Approved
REV 53, Jan 29, 2007
Airplane Flight Manual
CSP 700−1A
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
DOT Approved
REV 53, Jan 29, 2007
Airplane Flight Manual
CSP 700−1A
02−09−6
1. NAVIGATION SYSTEMS (CONT'D)
C. Standby Instrument
On airplanes 9159 and subsequent:
• Use of the integrated standby instrument localizer display for LOC BC approaches is
prohibited.
LIMITATIONS
NAVIGATION SYSTEMS
DOT Approved
REV 53, Jan 29, 2007
Airplane Flight Manual
CSP 700−1A
02−09−7
LIMITATIONS
NAVIGATION SYSTEMS
DOT Approved
REV 53, Jan 29, 2007
Airplane Flight Manual
CSP 700−1A
02−09−8
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