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C. Slat/Flap Extended Speed
The maximum speeds at which the slats/flaps may be extended are:
· Slats extended: 225 KIAS
· Flaps to 6 degrees: 210 KIAS
· Flaps to 16 degrees: 210 KIAS
· Flaps to 30 degrees: 185 KIAS
D. Maximum Landing Gear Operating Speed
· The maximum airspeed at which it is safe to retract the landing gear is 200 KIAS.
· The maximum airspeed at which it is safe to extend the landing gear is 200 KIAS.
E. Maximum Landing Gear Extended Speed
The maximum airspeed at which the airplane may be flown with the landing gear extended is
250 KIAS / 0.7 M.
Flight at altitudes above 20,000 feet with the landing gear extended is prohibited.
F. Tire Limit Speed
The tire limit speed is 183 knots ground speed.
G. Turbulence Penetration Speed
Maximum air speed for turbulence penetration is 300 KIAS or .80 Mach, whichever is lower.
NOTE
Turbulence penetration maneuvers must be accomplished in
accordance with the procedures detailed in Chapter 7;
SUPPLEMENTARY PROCEDURES − FLIGHT IN TURBULENCE.
H. Minimum Operating Limit Speed
Intentional speed reduction below the onset of stall warning, as defined by stick shaker
operation, is prohibited.
VMCG is 80 KIAS and VMCA in the takeoff
configuration is 86 KIAS.
LIMITATIONS
OPERATING SPEEDS
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 1
02−06−6
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
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 1
02−07−1
LIMITATIONS
MANEUVERING LOADS
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 1
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
REV 48, Dec 01, 2005 Flight Crew Operating Manual
CSP 700−6
Volume 1
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.
　
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