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• The maximum negative relief differential pressure is −0.5 psi.
• During taxi and take-off, the pressure differential must not exceed 0.1 psi.
• During initial landing (at touchdown), the pressure differential must not exceed 1.0 psi.
• Auxiliary pressurization (AUX PRESS) system operations are prohibited at altitudes
greater than 41,000 feet.
• APU bleed extraction above 45 °C OAT for air-conditioning operation is prohibited.
• Use of the EMER DEPRESS switch above 15,000 feet is prohibited.
B. Automatic Flight Control System
• Maximum altitude for flight with the yaw damper disengaged is 41,000 feet.
• The minimum autopilot engage height is 400 feet AGL.
• The minimum autopilot use height is:
− For a precision approach (Category I or II ILS) is 50 feet AGL, and
− For a non-precision approach is 400 feet AGL.
JAA Certified Airplanes
• The minimum autopilot use height is:
− For a precision approach (Category I or II ILS) is 80 feet AGL, and
− For a non-precision approach is 400 feet AGL.
• Use of the NAV guidance panel switch for approaches with VOR as a NAV source is
prohibited.
• Use of FLC mode with the speed bug above 0.85 Mach is prohibited.
NOTE
Large wind gradients, such as climbing or descending thru the jet
stream, may cause undesirable pitch and/or speed changes in FLC.
If this occurs it is recommended that another vertical mode (PIT,
VS) be selected.
LIMITATIONS
SYSTEMS
REV 7, Dec 01, 2005 Flight Crew Operating Manual
CSP 700−5000−6
Volume 1
02−08−1
1. SYSTEMS (CONT'D)
B. Automatic Flight Control System (Cont’d)
Effectivity:
• Airplanes 9127 thru 9153 not incorporating Service Bulletin:
• SB 700−1A11−31−002, Integrated Avionics Computers (IAC) − Batch 2 IAC
Upgrade.
Use of FLC mode with the speed bug in the MACH mode is prohibited.
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. Touch-and-go
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 −
TAKE-OFF PERFORMANCE − Maximum Allowable Brake Temperature for Take-off) must be
observed between a landing or a low-energy rejected take-off (RTO) and a subsequent
take-off, to ensure that sufficient brake energy is available to bring the airplane to a complete
stop, if the subsequent take-off 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 7, Dec 01, 2005
CSP 700−5000−6
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
　
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