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LIMITATIONS
Operating Speeds
02−06−3
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
LIMITATIONS
Operating Speeds
02−06−4
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
THIS PAGE INTENTIONALLY LEFT BLANK
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
02−07−1
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
LIMITATIONS
Maneuvering Loads
02−07−2
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
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) 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
02−08−1
REV 71, Oct 31/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
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.
To ensure adequate maneuver margins, flight spoilers must not be extended in flight at
airspeeds below the recommended approach speed plus 10 KIAS (refer to Chapter 6;
PERFORMANCE – LANDING PERFORMANCE).
6. STALL PROTECTION SYSTEM
Both stall protection system pusher switches must remain on for all phases of flight.
The stall protection test indicator must only be used for stall protection system functional test
purposes.
7. THRUST REVERSERS
Thrust reversers are approved for ground use only.
The thrust reversers are intended for use during full stop landings. Do not attempt a go-around
maneuver after deployment of the thrust reversers.
Backing the airplane with the use of reverse thrust is prohibited.
Take-off with any of the following thrust reverser icons or EICAS messages displayed is
prohibited:
• REV icon on N1 gauge,
• L (R) REV UNLOCKED caution message, and
• L (R) REV UNSAFE caution message.
During landing, application of maximum reverse thrust is not permitted at airspeeds below
60 KIAS. Below 60 KIAS, reverse thrust must be reduced to 60% N1 or less.
　
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