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C. APU Generator
· The load limit on the APU generator is 40 kVA.
· For operations above 37,000 feet, if the APU generator is powering a bus, the associated
hydraulic pump must be selected off (1B − AC BUS 3; 2B − AC BUS 2; 3A − AC BUS 4;
3B − AC BUS 1).
D. Flight Spoilers
· Flight Spoilers must be retracted below 300 feet AGL.
E. Stall Protection System
· Both stall protection pusher switches must remain on for the duration of the flight.
F. Thrust Reversers
· Thrust reversers must not be selected in flight. Positioning of thrust levers in the reverser
range while in flight is prohibited.
· The thrust reversers are intended for use during full stop landings. Touchandgo
maneuvers after deployment of the thrust reversers is prohibited.
· Backing the airplane with the use of reverse thrust is prohibited.
G. Wheel Brake Cooling Limitations
Brake and tire cooling times (established in accordance with Chapter 6; PERFORMANCE −
TAKEOFF
PERFORMANCE − Maximum Allowable Brake Temperature for Takeoff)
must be
observed between a landing or a lowenergy
rejected takeoff
(RTO) and a subsequent
takeoff,
to ensure that sufficient brake energy is available to bring the airplane to a complete
stop, if the subsequent takeoff
is rejected.
H. Traffic Alert And Collision Avoidance System (TCAS)
Pilots are authorized to deviate from their Air Traffic Control (ATC) clearance in order to
comply with a TCAS resolution advisory (RA) command.
Maneuvers must not be based solely on information presented on the MFD traffic display.
JAA Certified Airplanes
The use of TCAS must comply with the appropriate national operational regulations.
I. Flight Controls − Flaps
Flight with slats / flaps extended at altitudes above 18,000 feet is prohibited.
LIMITATIONS
SYSTEMS
Flight Crew Operating Manual REV 48, Dec 01, 2005
CSP 700−6
Volume 1
02−08−2
1. SYSTEMS (CONT'D)
J. Configuration Deviation List
If the airplane is to be operated with certain secondary airframe and/or any nacelle parts
missing, operation must be in accordance with the limitations specified in the basic Airplane
Flight Manual, and as amended by the Airplane Flight Manual, CONFIGURATION
DEVIATION LIST (APPENDIX 1).
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.
LIMITATIONS
SYSTEMS
REV 51, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−6
Volume 1
02−08−3
1. SYSTEMS (CONT'D)
Effectivity:
• Airplanes 9002 thru 9122 not incorporating Service Bulletin:
　
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