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operationmust be in accordance with the limitations specified in the basic Airplane FlightManual,
and as amended by the Configuration Deviation List.
Airplane Flight Manual
CSP C-012 DOT Approved
REV 2, Feb 24/04
LIMITATIONS
Systems Limitations
02--08--4
14. ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS)
General <2040>
S The system must be operated in accordance with the Enhanced Ground Proximity Warning
System Pilot’s Guide P/N 060--4241--0000 REV B or later applicable edition.
S Pilots are authorized to deviate from their current air traffic control (ATC) clearance to the
extent necessary to comply with an EGPWS.
CAUTION
When there is no GPS input, theEGPWSmay fail to alert
when a terrain threat exists, during ambient surface
temperatures below ISA, during non-standard
temperature lapse rates or if incorrect barometric
settings are set on the altimeter <2040, 1027 & 2040, 1047 & 2040>.
System Limitations <2040>
S 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.
S Airplane navigation must not be predicated upon the use of the terrain display.
S To avoid giving unwanted alerts, the terrain awareness alerting and display functions must
be inhibited by selecting the GRND PROX, TERRAIN switch OFF when within 15 nm of
take-off, approach or landing of an airport not contained in the EGPWS airport database.
Terrain Avoidance Maneuvering <2040>
S The terrain display provides situational awareness only, and may not provide the accuracy
and / or fidelity upon which to solely base terrain avoidance maneuvering.
S When an enhanced ground proximity 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.
Both GPS Inoperative <1027 & 2040>
S With both GPS sensors inoperative <1027 & 2040>, the GRND PROX, TERRAIN switch
should be selected to OFF unless the FMS position has been updated within five (5)
minutes prior to take-off.
S With both GPS sensors inoperative <1027 & 2040>, the terrain awareness alerting and display
system must be inhibited by selecting the GRND PROX, TERRAIN switch to OFF during
QFE operations.
Airplane Flight Manual
CSP C-012 DOT Approved
REV 2, Feb 24/04
LIMITATIONS
Systems Limitations
02--08--5
15. PNEUMATIC SYSTEM
S Wing and / or cowl anti-ice selection is prohibited with the APU as a bleed source in manual
mode.
16. MULTI-FUNCTION DISPLAYS
S Flicker may occur on the MFD with a large number of FMS symbols selected for display
and larger ranges selected. To manually declutter the MFD:
S Reduce range selected,
S Deselect TCAS overlays,
S Deselect radar / terrain overlays,
S Deselect some of the FMS symbology.
Airplane Flight Manual
CSP C-012 DOT Approved
REV 2, Feb 24/04
LIMITATIONS
Systems Limitations
02--08--6
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Airplane Flight Manual
CSP C-012 DOT Approved
Sep 09/02
LIMITATIONS
Navigation Systems Limitations
02---09---1
1. FLIGHT MANAGEMENT SYSTEM
S Options <1214>:
Airplanes equipped with FMS--4200 (FMC 822--0783--015) (SCID 832--4119--016):
S The flight management system (FMS) must be operated in accordance with the latest
edition of the following:
S Airplane Flight Manual, and
S Flight Management System Pilot Guide, part number 523--0778363.
S The FMS installation meets the requirements of JAA Temporary Guidance Leaflet No.
2, Rev. 1: AMJ 20X2--JAA Guidance Material on Airworthiness Approval and
Operational Criteria for Use of Navigation Systems in European Airspace Designated
for Basic RNAV Operations.
S The FMS is approved for use only with software program version SCID 832--4119--016.
S ILS, LOC, LOC-BC, LDA, SDF and MLS approaches using the FMS are prohibited.
S The FMS is approved for use only during enroute, terminal and non-precision approach
phases of flight.
S FMS range and fuel management information is advisory only.
S IFR enroute and terminal navigation is prohibited unless the pilot verifies the currency
of the database or verifies waypoints for accuracy by reference to current publications.
S Instrument approaches must be accomplished with instrument approach procedures
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