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DOT Approved
REV 39, Dec 01, 2003
Airplane Flight Manual
CSP 700−1A
02−06−4
1. MANEUVERING LOADS
A. Maneuvering Limit Load Factors
These load factors limit the permissible angles of bank in turns and the severity of pullup
and
pushover
maneuvers:
· Slats / flaps retracted: −1.0 G to +2.5 G.
· Slats / flaps extended: 0.0 G to +2.0 G.
LIMITATIONS
MANEUVERING LOADS
DOT Approved
REV 39, Dec 01, 2003
Airplane Flight Manual
CSP 700−1A
02−07−1
LIMITATIONS
MANEUVERING LOADS
DOT Approved
REV 39, Dec 01, 2003
Airplane Flight Manual
CSP 700−1A
02−07−2
THIS PAGE INTENTIONALLY LEFT BLANK
1. SYSTEMS
A. AirConditioning
and Pressurization
· Pack discharge temperatures during manual mode temperature control operations must
be kept between 5 °C and 60 °C.
· One pack must be selected off if pack control is in manual mode.
· The maximum relief differential pressure is 10.73 psi.
Effectivity:
· Airplanes 9002 thru 9158 not incorporating Service Bulletin:
· SB 700−21−034, Modification − Pressurization Control − Cabin Altitude Reduction
During Flight for Improved Passenger Comfort.
· The maximum relief differential pressure is 10.02 psi.
· The maximum negative relief differential pressure is −0.5 psi.
· During taxi and takeoff,
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 airconditioning
operation 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 nonprecision
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 nonprecision
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
DOT Approved
REV 48, Dec 01, 2005
Airplane Flight Manual
CSP 700−1A
02−08−1
1. SYSTEMS (CONT'D)
B. Automatic Flight Control System (Cont’d)
Effectivity:
· Airplanes 9002 thru 9153 not incorporating Service Bulletin:
· SB 700−31−021, 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. 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
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