曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
• 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 4B
Category II Operations
07−04B−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 4B
Category II Operations
07−04B−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
on PFDs (OFF flag may flash
at end of test).
(6) Decision height......................................................... Set on both PFDs.
(7) MDA ......................................................................... Set as a barometric DH, in case
RA fails.
(8) Runway Course........................................................ Set on both PFDs, or armed
(cyan) by FMS.
(9) EFIS .....................................................................Check that no comparator flags are
displayed.
(10) CAS......................................................................Check that the following messages
are not displayed:
• AFCS MSGS FAIL warning
message,
• AP PITCH TRIM, EFIS
COMP INOP and EFIS
COMP MON caution
messages,
• FD 1 and 2 FAIL status
messages.
(11) Stabilizer and elevator position ............................Check valid on F/CTL synoptic page.
(12) Approach mode ....................................................... Arm
B. Before Landing:
(1) Autopilot ........................................................Disengage at an altitude not less than
80 feet AGL.
SUPPLEMENT 4B
Category II Operations
07−04B−01−4
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
6. ABNORMAL PROCEDURES
The abnormal procedures in Chapter 5 are applicable, except as modified by the following:
A. Single Engine Approach and Landing
(1) Approach .......................................................... Conduct under Category I operations.
B. Engine Failure During Final Approach
Continue approach if the following can be accomplished above 800 feet AGL:
(1) Autopilot ....................................................... Disconnect
(2) Operating engine.............................................. Increase thrust as required.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
庞巴迪挑战者604飞机飞行手册CL604 Airplane Flight Manual 2(78)
