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subsequent landing flaps 45° configuration, are given in Figure 06−10A−1. The chart
incorporates all applicable anti-icing and 10th stage bleeds combinations.
NOTE
If ice accumulation is suspected on unprotected surfaces, then reduce the
maximum landing weight values derived from Figure 06−10A−1 by 800 kg
(1764 lb).
Example: ANTI-ICE ON
Associated Conditions:
Temperature = −8° C
Airport pressure altitude = 4,000 ft
Cowl anti-ice = On
10th stage bleeds = Closed
For the above associated conditions (Anti-ice On), the maximum landing weight limited by
climb requirements is 24,100 kg (53,131 lb). The landing weight in this case is greater than
the maximum approved landing weight (Refer to: Chapter 2; LIMITATIONS – STRUCTURAL
WEIGHT) and is not considered limiting.
Example: ANTI-ICE OFF
Associated Conditions:
Temperature = 27° C
Airport pressure altitude = 4,000 ft
Wing and cowl anti-ice = Off
10th stage bleeds = Closed
For the above associated conditions (Anti-ice Off), the maximum landing weight limited by
climb requirements is 23,700 kg (52,250 lb). The landing weight in this case is greater than
the maximum approved landing weight (Refer to: Chapter 2; LIMITATIONS – STRUCTURAL
WEIGHT) and is not considered limiting.
SUPPLEMENTARY PROCEDURES
Category II Operation
Vol. 1 06−10A−11
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
DFM0704A_001 ldg_watlim_405_ha_Cll.uni
SUPPLEMENTARY PROCEDURES
Category II Operation
Vol. 1 06−10A−12
REV 66, Feb 01/07
Landing Weight Limited by Climb Requirements − Approach Flaps 20°/Landing Flaps 45°
Figure 06−10A−1
CL−604 Operating Manual
PSP 604−6
NOTE
These supplementary procedures are only applicable to airplanes
5442 and 5467, on the CAA (UK) Registry.
These supplementary procedures do not constitute approval to
conduct Category II operations. Such authorization must be obtained
by the operator from the appropriate authorities.
1. GENERAL
The CL 600-2B16 (CL–604) airplane has been shown to meet the airworthiness requirements for
Category II Operations contained in Appendix 1 of AC 120-29 and JAR AWO, Subpart 2.
The following data must be used when conducting Category II operations.
These data complement or supersede data contained in the basic Operating Manual. This
supplement must, therefore, be read in conjunction with the basic Operating Manual.
The effect of this Supplement on the basic Operating Manual is given in paragraphs (2) to (7).
2. INTRODUCTION
The general information in Chapter 1 is applicable.
SUPPLEMENTARY PROCEDURES
Category II Operation
Vol. 1 06−10B−1
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
3. OPERATING LIMITATIONS
The operating limitations in Chapter 2 are applicable, except as modified by the following:
• An ILS approach to Category II minima must not be commenced or continued unless all
required airborne equipment, specified in the Category II Required Equipment List below
and their ground installations, are operating satisfactorily.
CATEGORY II REQUIRED EQUIPMENT LIST
EQUIPMENT PRIOR TO APPROACH
VHF NAV 1 and 2 Both must be operational.
PFD 1 and 2 One (1) PFD available and operational for each side.
STAB Channel 1 and 2 One (1) channel must be operational.
Radio Altimeter Both must be operational.
IRS Any two (2) must be operational.
ADC 1 and 2 Both must be operational.
FD 1 and 2 Both must be operational.
EFIS Comparator Monitors Must be operational.
AFCS Pitch Trim Must be operational.
Autopilot Must be operational.
Hydraulics (3) All systems must be on and operational.
Electrics Two (2) generators on and sharing load (see NOTE).
NOTE
Approach to Category II minima may be continued with one generator, if
an engine fails during final approach (Refer to Chapter 5; ABNORMAL
PROCEDURES).
• Operation of the autopilot is prohibited below 80 feet AGL.
• The approved flap configurations for approach are:
• 45° for all engines operating, and
• 20° for one engine inoperative.
• The minimum decision height for Category II operations is 100 feet AGL.
• Wind limits for autopilot approaches are:
• 8 knots crosswind, and
• 9 knots tailwind.
NOTE
Demonstrated headwind is 16 knots.
• The maximum ILS glidepath angle for Category II operations is 3.5 degrees.
SUPPLEMENTARY PROCEDURES
Category II Operation
　
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