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K. Nose Wheel Steering System
. Towbarless towing is prohibited, unless the operation is performed in compliance with the Airplane Maintenance Manual towbarless towing requirements.
L. Enhanced Ground Proximity Warning System (EGPWS)
(1) SYSTEM LIMITATIONS
.
The system must be operated in accordance with the latest edition of the Airplane 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.
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LIMITATIONS NAVIGATION SYSTEMS
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:
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