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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 .
LIMITATIONS Operating Speeds Vol. 1 02.06.3
Oct 05/06
4. FLAPS EXTENDED SPEED The maximum speeds at which the flaps may be extended are: Flaps to 20 degrees: 231 KIAS Flaps to 30 degrees: 197 KIAS Flaps to 45 degrees: 189 KIAS
5. MAXIMUM LANDING GEAR OPERATING SPEED The maximum airspeed at which it is safe to extend the landing gear is 197 KIAS / 0.6 MI. The maximum airspeed at which it is safe to retract the landing gear is 197 KIAS / 0.6 MI.
6. MAXIMUM LANDING GEAR EXTENDED SPEED
The maximum airspeed at which the airplane may be flown with the landing gear extended and locked is 250 KIAS / 0.7 MI.
Flight at altitudes above 20,000 feet with the landing gear extended is prohibited.
7. TIRE LIMIT SPEED
The tire limit speed is 182 knots ground speed.
8. TURBULENCE PENETRATION SPEED
Maximum air speed for turbulence penetration is 280 KIAS or 0.75 Mach, whichever is lower.
9. MINIMUM OPERATING LIMIT SPEED
Intentional speed reduction below the onset of stall warning, as defined by stick shaker operation, is prohibited unless a lower speed is specifically authorized for flight test or training operations.
LIMITATIONS Operating Speeds Vol. 1 02.06.4
Oct 05/06
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CL.605 Flight Crew Operating Manual
PSP 605.6
LIMITATIONS Maneuvering Loads Vol. 1 02.07.1
Oct 05/06
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:
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Flaps up: .1.0 G to 2.5 G.
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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.
LIMITATIONS Maneuvering Loads Vol. 1 02.07.2
Oct 05/06
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CL.605 Flight Crew Operating Manual
PSP 605.6
LIMITATIONS Systems Limitations Vol. 1 02.08.1
Oct 05/06
1. AIR-CONDITIONING AND PRESSURIZATION
The maximum relief differential pressure is 9.2 psi.
The maximum negative differential pressure is –0.5 psi.
During taxi, take-off and landing, the pressure differential must not exceed 0.2 psi.
The airplane must be completely depressurized prior to opening any of the airplane doors.
2. AUTOMATIC FLIGHT CONTROL SYSTEM
The minimum autopilot engage height after take-off is 320 feet AGL.
The minimum autopilot use height for visual and non-precision approaches is 320 feet AGL.
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