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PSP 604−6
7. PERFORMANCE (CONT'D)
DFO1_0622_004 block_time_all.uni
SUPPLEMENTARY PROCEDURES
Flight With Landing Gear Down
Vol. 1 06−22−6
REV 66, Feb 01/07
Block Time vs Range
Figure 06−22−4
CL−604 Operating Manual
PSP 604−6
7. PERFORMANCE (CONT'D)
DFO1_0622_005
SUPPLEMENTARY PROCEDURES
Flight With Landing Gear Down
Vol. 1 06−22−7
REV 66, Feb 01/07
Long Range Cruise Speed (KIAS)
Figure 06−22−5
CL−604 Operating Manual
PSP 604−6
SUPPLEMENTARY PROCEDURES
Flight With Landing Gear Down
Vol. 1 06−22−8
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
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NOTE
These supplementary procedures are only applicable to airplanes
5442 and 5467, on the CAA (UK) Registry.
1. GENERAL
These supplementary procedures must be used when conducting operation under the CAA (UK)
Registry.
These data complement or supersede data contained in the basic Operating Manual. These
supplementary procedures must, therefore, be used in conjunction with the basic Operating
Manual.
The effect of these supplementary procedures on the basic Operating Manual is given below.
2. INTRODUCTION
The general information in Chapter 1 is applicable.
3. OPERATING LIMITATIONS
The operating limitations in Chapter 2 are applicable, except as modified by the following:
A. Introduction
CERTIFICATION CATEGORY
This airplane is eligible for certification in the transport category (passenger).
KINDS OF AIRPLANE OPERATION
The standby altimeter is not approved for use during RVSM operations.
B. Operating Speeds
MAXIMUM OPERATING SPEED AND MACH NUMBER
Maximum operating limit speeds, as given in Figure 06−23−1, 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.
SUPPLEMENTARY PROCEDURES
CAA (UK) Registry Operation
Vol. 1 06−23−1
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
3. OPERATING LIMITATIONS (CONT'D)
DFO1_0623_001 Vmo_Mmo_afm.uni
SUPPLEMENTARY PROCEDURES
CAA (UK) Registry Operation
Vol. 1 06−23−2
REV 66, Feb 01/07
Maximum Operating Speed and Mach Number
Figure 06−23−1
CL−604 Operating Manual
PSP 604−6
3. OPERATING LIMITATIONS (CONT'D)
C. Systems Limitations
AUTOMATIC FLIGHT CONTROL SYSTEM
The minimum autopilot engage height after take-off is 1,000 feet AGL.
The minimum autopilot use height for visual and non-precision approaches is 1,000 feet AGL.
FLIGHT CONTROLS – LIFT/DRAG DEVICES
Flight Spoilers
Flight below an altitude of 800 feet AGL with flight spoilers extended is prohibited.
4. EMERGENCY PROCEDURES
The emergency procedures in Chapter 3 are applicable.
5. NORMAL PROCEDURES
The normal procedures in Chapter 4 are applicable, except as modified by the following;
A. Taxiing and Take-Off
AFTER TAKE-OFF PROCEDURE
(1) Airspeed ...........................................V2 + 10 to 15 KIAS
(2) Flight and engine instruments ............................Monitor Check that engine indications
remain within limits, and flight
instruments indicate the
desired climb profile.
At a safe altitude, not below 1,000 ft AGL:
(3) AP switch/light ...................................................Press in to engage, if required.
Check the following:
• Heading mode engaged.
• Speed bug set to 200 KIAS.
NOTE
The use of excessive pitch mode (VS) on the FCP could cause
autopilot uncommanded disengagement.
Autopilot can be re-engaged after disengagement.
(4) Climb thrust .............................................................. Set the computed climb thrust
setting.
(5) IGNITION, CONT switch/light...................... As required
B. Approach and Landing
CIRCLING APPROACH
When performing a circling approach, maintain the airplane configuration from the final
approach fix (FAF) onwards (Flaps 30° and landing gear down). At the circling MDA with the
field in sight, maneuver to establish a downwind leg parallel to the runway, at a distance of
approximately 1 1/2 miles.
SUPPLEMENTARY PROCEDURES
CAA (UK) Registry Operation
Vol. 1 06−23−3
REV 66, Feb 01/07
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CL−604 Operating Manual
PSP 604−6
5. NORMAL PROCEDURES (CONT'D)
B. Approach and Landing (Cont’d)
　
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