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The data in this supplement must be used when conducting Category II operations.
These data complement or supersede data contained in the basic Airplane Flight Manual. This
supplement must therefore, be read in conjunction with the basic Airplane Flight Manual.
The effect of this Supplement on the basic Airplane Flight Manual is given in paragraphs
(2) to (7).
2. INTRODUCTION
The general information in Chapter 1 is applicable.
SUPPLEMENT 4A
Category II Operations
07−04A−01−1
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
3. LIMITATIONS
The 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
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,
• 9 knots tailwind.
NOTE
Demonstrated headwind is 16 knots.
• The maximum ILS glidepath angle for Category II operations is 3.5 degrees.
SUPPLEMENT 4A
Category II Operations
07−04A−01−2
REV 68, Apr 16/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
4. EMERGENCY PROCEDURES
The emergency procedures in Chapter 3 are applicable, except as modified by the following:
A. Autopilot Failure
Indication: Abnormal autopilot operation and/or AFCS MSGS FAIL warning message,
“CAVALRY CHARGE” aural and/or flashing AP (red) message on the
primary flight displays.
Continue approach if the following can be accomplished above 500 feet AGL:
(1) Autopilot ....................................................... Disconnect
(2) AFCS SEL 1(2) switch (centre
pedestal)...............................................................Select to operative AFCS channel.
Check AFCS 1 (2) INOP
status message on.
(3) Autopilot ............................................................ Engage and monitor operation.
(4) Approach ......................................................... Continue to Category II minima.
If below 500 feet AGL, on a stabilized approach:
(1) Autopilot ....................................................... Disconnect
(2) Manual control.................................................. Resume
(3) Approach ......................................................... Continue to Category I minima.
If below 200 feet AGL and non-visual:
(1) Go-around ........................................................... Initiate
SUPPLEMENT 4A
Category II Operations
07−04A−01−3
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
5. NORMAL PROCEDURES
The normal procedures in Chapter 4 are applicable, except as modified by the following:
A. Prior to Approach:
Airplane must be properly configured prior to approach:
(1) Landing weight .....................................................Check within limits. See Chapter 6;
PERFORMANCE – LANDING
PERFORMANCE.
(2) NAV SOURCE switches........................................... Set to onside ILS (green) or armed
(cyan) by FMS for both PFDs.
(3) IRS and ADC source selectors................................. Set to NORM.
(4) IRS switches.........................................................Check set to NAV.
(5) RA TEST switch ....................................................Press Check 50 feet RA displayed
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庞巴迪挑战者604飞机飞行手册CL604 Airplane Flight Manual 2(73)
