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operation is prohibited.
LIMITATIONS
POWER PLANT
REV 6, Aug 30, 2005 Flight Crew Operating Manual
CSP 700−5000−6
Volume 1
02−05−9
LIMITATIONS
POWER PLANT
Flight Crew Operating Manual REV 6, Aug 30, 2005
CSP 700−5000−6
Volume 1
02−05−10
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1. OPERATING SPEEDS
A. Maximum Operating Speed and Mach Number
Maximum operating limit speeds as given in Figure 02−06−1.
GF0206_001 NEW_MMO.PLT
Maximum Operating Speed and Mach Number
Figure 02−06−1
LIMITATIONS
OPERATING SPEEDS
Mar 12, 2004 Flight Crew Operating Manual
CSP 700−5000−6
Volume 1
02−06−1
1. OPERATING SPEEDS (CONT'D)
B. Design Maneuvering Speed
CAUTION
Avoid rapid and large alternating control inputs, especially in
combination with large changes in pitch, roll, or yaw (e.g. large side
slip angles), as they may cause structural failure at any speed,
including below VA
Full application of rudder and aileron controls as well as maneuvers that involve angles of
attack near the stall, must be confined to speeds below VA.
Values of VA are given in Figure 02−06−2, for varying pressure altitudes and airplane
weights.
NOTE: For 51,000 feet, the maneuvering ’g’ was reduced to 2.3 ’g’ due to stall limitations.
LIMITATIONS
OPERATING SPEEDS
Flight Crew Operating Manual Mar 12, 2004
CSP 700−5000−6
Volume 1
02−06−2
1. OPERATING SPEEDS (CONT'D)
B. Design Maneuvering Speed (Cont’d)
LIMITATIONS
OPERATING SPEEDS
Design Maneuvering Speeds
Figure 02−06−2
REV 8, Jan 05, 2006 Flight Crew Operating Manual
CSP 700−5000−6
Volume 1
02−06−3
1. OPERATING SPEEDS (CONT'D)
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 take-off configuration is 86 KIAS.
LIMITATIONS
OPERATING SPEEDS
Flight Crew Operating Manual Mar 12, 2004
CSP 700−5000−6
Volume 1
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
Mar 12, 2004 Flight Crew Operating Manual
CSP 700−5000−6
Volume 1
02−07−1
LIMITATIONS
MANEUVERING LOADS
Flight Crew Operating Manual Mar 12, 2004
CSP 700−5000−6
Volume 1
02−07−2
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1. SYSTEMS
A. Air-Conditioning 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 9127 thru 9158 not incorporating Service Bulletin:
• SB 700−1A11−21−004, Modification − Pressurization Control − Cabin Altitude
Reduction During Flight for Improved Passenger Comfort.
The maximum relief differential pressure is 10.02 psi.
　
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