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airplane nose; >30 knots
windspeed.
After brakes release, set thrust smoothly to reach TOGA
by 60 KIAS.
ROLLING TAKE-OFF PROCEDURE applies (refer to the
Flight Crew Operating Manual, Volume 2 -- NORMAL
PROCEDURES -- TAKE-OFF -- Rolling Take-Off
Procedure).
Airplane Flight Manual
CSP C-012 DOT Approved
Sep 09/02
LIMITATIONS
Operating Speeds
02--06--1
1. MAXIMUM OPERATING SPEED AND MACH NUMBER
Maximum operating limit speeds as given in Figure 02--06--1, must not be deliberately exceeded
in any regime of flight (climb, cruise or descent), unless a higher speed is specifically authorized
for flight test or training operations.
Effectivity: <1030>
S Airplanes equipped for operation in Reduced Vertical Separation Minimum (RVSM) airspace:
2. RVSM MAXIMUM CRUISE MACH NUMBER
The maximum cruise Mach number during flight in RVSM airspace is 0.82.
3. DESIGN MANEUVERING SPEED
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.
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.
4. FLAPS EXTENDED SPEED
The maximum speeds at which the flaps may be extended are:
FLAPS 1: 230 KIAS
FLAPS 8: 230 KIAS
FLAPS 20: 220 KIAS
FLAPS 30: 185 KIAS
FLAPS 45: 170 KIAS
5. MAXIMUM LANDING GEAR OPERATING SPEED
S The maximum airspeed at which it is safe to extend the landing gear is 220 KIAS.
S The maximum airspeed at which it is safe to retract the landing gear is 200 KIAS.
6. MAXIMUM LANDING GEAR EXTENDED SPEED
The maximum airspeed at which the airplane may be flown with the landing gear extended and
locked is 220 KIAS.
Airplane Flight Manual
CSP C-012 DOT Approved
REV 3, May 03/05
LIMITATIONS
Operating Speeds
02--06--2
Maximum Operating Speed and Mach Number
Figure 02--06--1
Airplane Flight Manual
CSP C-012 DOT Approved
REV 3, May 03/05
LIMITATIONS
Operating Speeds
02--06--3
Design Maneuvering Speeds
Figure 02--06--2
Airplane Flight Manual
CSP C-012 DOT Approved
Sep 09/02
LIMITATIONS
Operating Speeds
02--06--4
7. TIRE LIMIT SPEED
The tire limit speed is 195 knots ground speed.
8. MAXIMUM AIRSPEED FOR ADG OPERATION
The maximum speed for ADG operation is VMO/MMO.
9. TURBULENCE PENETRATION SPEED
Maximum air speed for turbulence penetration is 280 KIAS or 0.75 Mach, whichever is lower.
10. MINIMUM OPERATING LIMIT SPEED
Intentional speed reduction below the onset of stallwarning, as defined by stick shaker operation,
is prohibited unless a lower speed is specifically authorized for flight test or training operations.
11. WINDSHIELD WIPER OPERATION
The windshield wiper must not be operated above 250 KIAS.
If the windshield wiper has failed in a non-parked position, the airplane speed must not exceed
250 KIAS.
Airplane Flight Manual
CSP C-012 DOT Approved
REV 2, Feb 24/04
LIMITATIONS
Maneuvering Loads
02--07--1
1. MANEUVERING LIMIT LOAD FACTORS
These load factors limit the permissible angles of bank in turns and the severity of pull-up and
push-over maneuvers:
Flaps up: --1.0 G to 2.5 G
Flaps down: 0.0 G to 2.0 G
2. SIDE SLIP MANEUVERS
Avoid unnecessary and large side-slip maneuvers during low speed high altitude cruise.
Airplane Flight Manual
CSP C-012 DOT Approved
Sep 09/02
LIMITATIONS
Maneuvering Loads
02--07--2
THIS PAGE INTENTIONALLY LEFT BLANK
Airplane Flight Manual
CSP C-012 DOT Approved
Sep 09/02
LIMITATIONS
Systems Limitations
02--08--1
1. AIR-CONDITIONING AND PRESSURIZATION
S The maximum relief differential pressure is 8.7 psi. The maximum negative differential
pressure is --0.5 psi.
S During taxi, take-off and landing, the pressure differential must not exceed 0.1 psi.
S The airplane must be completely depressurized prior to opening any of the airplane doors.
S The maximum altitude for single pack operation is 25,000 feet.
S To preclude possible crew and/or passenger ear damage, use of the EMER DEPRESS
switch above 15,000 feet is prohibited.
2. AUTOMATIC FLIGHT CONTROL SYSTEM
S Operation with the autopilot engaged is prohibited at altitudes below 600 feet AGL,
except when performing the following:
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