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Flight Manual and the Honeywell (formerly Allied Signal) Enhanced Ground Proximity
Warning System Pilot’s Guide P/N 060−4241−0000 REV D or latest approved edition.
• During QFE operations with no GPS sensors available, the terrain awareness alerting
and display system must be inhibited by selecting the EGPWS TERRAIN switch to
OFF when the barometric altitude is corrected to the landing field elevation.
• The TERR switch must be selected OFF when within 15 Nm of an intended take-off
or landing airport not contained in the EGPWS database.
• The terrain data base, terrain displays and alerting system do not account for
man-made obstructions, except for all known man-made obstructions in Canada, the
United States and Mexico.
• Airplane navigation must not be predicated upon the use of the terrain display.
(2) TERRAIN AVOIDANCE MANEUVERING
• The terrain display provides situational awareness only, and may not provide the
accuracy and / or fidelity upon which to solely base terrain avoidance maneuvering.
• When an Enhanced Ground Proximity Warning System alert, caution, or warning
occurs, a standard GPWS escape maneuver must be initiated. Only vertical
maneuvers are recommended, unless operating in visual meteorological conditions
(VMC) and / or the pilot determines, based upon all available information, that turning
in addition to the vertical escape maneuver is the safest course of action.
M. RAT Generator test
A RAT generator test must be accomplished in accordance with Chapter 4, NORMAL
PROCEDURES − AIRPLANE PREPARATION − Flight Compartment Originating Check −
RAT Generator Test.
LIMITATIONS
SYSTEMS
REV 12, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−5000−6
Volume 1
02−08−3
LIMITATIONS
SYSTEMS
Flight Crew Operating Manual Mar 12, 2004
CSP 700−5000−6
Volume 1
02−08−4
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1. NAVIGATION SYSTEMS
A. Flight Management System
• 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 for the CD−820,
publication number A28−1146−149−00, dated May 2000 or latest applicable revision,
and
(3) Honeywell Flight Management System FMZ Pilot’s Operating Manual, publication
number A28−1146−185−00, dated June 2004 or latest applicable revision.
• The FMS is approved for use with software program version NZ5.8 as displayed on the
FMS CDU “NAV IDENT” page 1/1.
Effectivity:
• Airplanes 9127 thru 9174 not incorporating Service Bulletin:
• SB 700−1A11−31−007, Integrated Avionics Computer (IAC) System − Batch 2+ IAC
Upgrade.
• Use of the FMS TOLD function is prohibited.
• If a difference exists between the AFM and the Honeywell FMS Pilot’s Operating Manual,
the AFM shall take precedence.
• Use of the FMS database for IFR is prohibited unless the database is current or the pilot
verifies waypoints for accuracy by reference to current publications.
• The FMS must not be used as a navigation source unless it is receiving suitable
navigation information from the following:
− One VOR /DME, or
− Two DMEs, or
− One inertial reference system.
• The flight plans on the paired FMSs must be identical when conducting FMS approaches.
• Instrument approaches must be accomplished only in accordance with instrument
approach procedures that are contained in the FMS database. The database must
incorporate the current update cycle. The pilot must verify approach waypoints for
accuracy by reference to current publications.
• Use of FMS as a sole NAV source for instrument approaches past the Final Approach Fix
is prohibited unless APP is annunciated on the PFD.
• Fuel display parameters are advisory only, and must not be used to replace primary fuel
quantity or fuel flow indications for fuel load and range planning.
• The aircraft must have other approved navigation equipment, appropriate to the route,
installed and operating.
• Use of FMS as the PFD NAV SRC for ILS, LOC, LOC−BC, LDA, SDF and MLS
approaches beyond the Final Approach Fix is prohibited.
• Capture and tracking of DME arcs outside of the published end points of an approved IFR
procedure is prohibited.
LIMITATIONS
NAVIGATION SYSTEMS
REV 14, Jan 29, 2007 Flight Crew Operating Manual
　
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