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LIMITATIONS
Operating Speeds
Vol. 1 02−06−1
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
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 .
DFM0206_002
Design Maneuvering Speeds
Figure 02−06−2
LIMITATIONS
Operating Speeds
Vol. 1 02−06−2
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
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 02−06−3
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
LIMITATIONS
Operating Speeds
Vol. 1 02−06−4
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
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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.
LIMITATIONS
Maneuvering Loads
Vol. 1 02−07−1
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
LIMITATIONS
Maneuvering Loads
Vol. 1 02−07−2
Oct 05/06
CL−605 Flight Crew Operating Manual
PSP 605−6
THIS PAGE INTENTIONALLY LEFT BLANK
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.
The minimum autopilot use height for precision approaches (ILS) is 80 feet AGL.
Operations with an ILS glidepath angle that exceeds 3.5 degrees are prohibited.
3. BLEED AIR SYSTEMS
The bleed air 10th stage valves must be closed for take-off and landing if the engine cowl and/or
wing anti-ice systems have been selected on.
If above 40,000 feet, one air-conditioning unit or cowl anti-ice system must be selected on for
each engine.
4. ELECTRICAL SYSTEMS
A. Permissible Loads on AC System
Individual AC generator loading must not exceed the following values:
ALTITUDE (FEET)
LOAD LIMITATION (KVA)
MAIN GENERATOR (EACH) APU GENERATOR
0 to 20,000 30 30
20,001 to 35,000 30 0
35,001 and above 25 0
B. Permissible Loads on DC Systems
The maximum permissible continuous load on each TRU is 100 amps.
5. FLIGHT CONTROLS – LIFT/DRAG DEVICES
A. Flaps
Enroute use of flaps is prohibited.
Flight with flaps extended at altitudes above 15,500 feet is prohibited.
B. Flight Spoilers
Flight below an altitude of 300 feet AGL with flight spoilers extended is prohibited.
　
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