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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. MAXIMUM AIRSPEED FOR ADG OPERATION
On airplanes 5301 to 5407:
The maximum airspeeds for continuous operation of the air-driven generator are as follows:
• Following automatic or manual deployment, the maximum airspeed is 250 KIAS.
• When operationally necessary (e.g. windmill airstarts), speeds up to 330 KIAS are permitted
for a period of twelve (12) minutes, and speeds between 330 and 348 KIAS are permitted for
a period of four (4) minutes.
• For flight test or pilot training deployment, the maximum airspeed is 215 KIAS.
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 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
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
LIMITATIONS
Operating Speeds
Vol. 1 02−06−4
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
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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
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
LIMITATIONS
Maneuvering Loads
Vol. 1 02−07−2
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
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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) with a glidepath angle of
3.5 degrees or less is 80 feet AGL.
The minimum autopilot use height for precision approaches (ILS) with a glidepath angle between
3.5 and 4 degrees is 160 feet AGL.
On airplanes incorporating Service Bulletin 604–34–012:
The ADC source coupled to the active autopilot must be the same as that coupled to the ATC
transponder during flight in RVSM airspace.
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.
C. Circuit Breaker Reset (In Flight)
A circuit breaker must not be reset or cycled (i.e., opened or closed) unless doing so is
consistent with explicit procedures specified in the Airplane Flight Manual or unless, in the
judgement of the Pilot-in-Command, that resetting or cycling of the circuit breaker is
necessary for the safe completion of the flight.
LIMITATIONS
Systems Limitations
Vol. 1 02−08−1
REV 71, Oct 31/07
CL−604 Operating Manual
PSP 604−6
5. FLIGHT CONTROLS – LIFT/DRAG DEVICES
　
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