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CL−604 Operating Manual
PSP 604−6
7. SUPPLEMENTARY PROCEDURES (CONT'D)
In all instances, changes to the thrust settings must be made accordingly, in order to maintain
the desired speed.
CIRCLING
If the circling altitude is lower than 1,000 feet AGL, the autopilot must not be used.
If the autopilot is used, altitude hold is accomplished by selecting ALT mode, which will
maintain the pressure altitude existing at the time of selection. Turns are accomplished in the
heading mode, and descents made with the vertical speed mode.
MISSED APPROACH
The autopilot may be engaged after a missed approach, at a safe altitude (not below 1,000
feet AGL). The missed approach altitude should already have been selected, when tracking
inbound towards the fix. Turns are accomplished in the heading mode, and climbs made with
thrust adjustments to achieve the appropriate climb speed, enabling the autopilot to capture
the preselected missed approach altitude.
8. PERFORMANCE
The performance data in Chapter 6 of the Airplane Flight Manual are applicable, except as
modified by the following:
A. General
CL−604 airplanes are classified in Air Navigation Orders, Performance Group A and JAR
OPS 1, Performance Class A.
SUPPLEMENTARY PROCEDURES
CAA (UK) Registry Operation
Vol. 1 06−23−6
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
1. GENERAL
These supplementary procedures must be used when conducting operations with some specific
airplane systems inoperative.
These data complement or supersede data contained in the basic Operating Manual. This
supplement must, therefore, be used in conjunction with the basic Operating Manual.
These supplementary procedures are applicable only when used in conjunction with a Minimum
Equipment List approved by the appropriate authority.
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 per MMEL or as modified by the
following:
A. Hydraulic AC Motor Pump Inoperative
APR must be selected off, when dispatching with one hydraulic AC motor pump (1B or 2B)
inoperative.
4. EMERGENCY PROCEDURES
The emergency procedures in Chapter 3 are applicable.
5. NORMAL PROCEDURES
The normal procedures in Chapter 4 are applicable.
6. ABNORMAL PROCEDURES
The abnormal procedures in Chapter 5 are applicable.
SUPPLEMENTARY PROCEDURES
Operation with Systems Inoperative
Vol. 1 06−24−1
REV 71, Oct 31/07
CL−604 Operating Manual
PSP 604−6
7. SUPPLEMENTARY PROCEDURES
The supplementary procedures in Chapter 6 are applicable, except as modified by the following:
A. Category II Operations (Airplanes on the German Registry)
The maximum landing weight limited by climb requirements when dispatching with one
hydraulic AC motor pump inoperative is determined from Figure 06−24−1.
B. Category II Operations (Airplanes on the CAA (UK) Registry)
The maximum landing weight limited by climb requirements when dispatching with one
hydraulic AC motor pump inoperative is determined from Figure 06−24−1.
Example: ANTI-ICE ON
Associated Conditions:
Temperature = –8°C
Airport pressure altitude = 6,000 ft
Wing and cowl anti-ice = On
10th stage bleeds = Closed
As shown in the example (Figure 06−24−1, Anti-ice On), the maximum landing weight
limited by climb requirements is 21,100 kg (46,518 lb).
Example: ANTI-ICE OFF
Associated Conditions:
Temperature = 27°C
Airport pressure altitude = 6,000 ft
Wing and cowl anti-ice = Off
10th stage bleeds = Closed
As shown in the example (Figure 06−24−1, Anti-ice Off), the maximum landing weight
limited by climb requirements is 20,600 kg (45,415 lb).
SUPPLEMENTARY PROCEDURES
Operation with Systems Inoperative
Vol. 1 06−24−2
REV 71, Oct 31/07
CL−604 Operating Manual
PSP 604−6
7. SUPPLEMENTARY PROCEDURES (CONT'D)
DFM0708_014
SUPPLEMENTARY PROCEDURES
Operation with Systems Inoperative
Vol. 1 06−24−3
REV 71, Oct 31/07
Landing Weight Limited by Climb Requirements − Category II Operations
Figure 06−24−1
CL−604 Operating Manual
PSP 604−6
7. SUPPLEMENTARY PROCEDURES (CONT'D)
C. Airworthiness Flight Test/Crew Training (Airplanes on the CAA (UK) Registry)
When dispatching with one hydraulic AC motor pump inoperative, airworthiness flight
　
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