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
− END −
No
Copilot’s Radio Altimeter has failed (if installed):
NOTE
With one radio altimeter failed, both TCAS (if installed) and
GPWS (if installed) remain operational.
(1) No further action required.
END
ABNORMAL PROCEDURES
Instruments System
05−15−4
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. INSTRUMENTS SYSTEM (CONT'D)
G. Inertial Reference System Failure
Indication: Similar to EFIS comparator monitor failures; erratic primary flight display
data.
NOTE
If an IRS is in attitude mode, a heading drift rate of up to 15 degrees
per hour can occur. The FMS heading on the IRS CONTROL page
should be updated periodically from the best available alternate
navigation source.
Pilot’s IRS has failed:
Yes
(1) IRS source selector ......................................Select to an operative IRS.
Check PFD 1 indicates IRS 2
source selected (If IRS 3 is
installed and selected, PFD 1
indicates IRS 3 source
selected).
NOTE
1. Windshear detection (if installed) is operative on
copilot’s side only.
2. If IRS 3 is not installed, pilot’s flight director is
inoperative, FD 1 FAIL status message comes on.
− END −
No
Copilot’s IRS has failed:
(1) IRS source selector ..............................................Select to an operative IRS.
PFD 2 indicates IRS 1 source
selected (If IRS 3 is installed
and selected, PFD 2 indicates
IRS 3 source selected).
NOTE
1. Windshear detection (if installed) is inoperative on both
sides.
2. If IRS 3 is not installed, copilot’s flight director is inoperative,
FD 2 FAIL status message comes on.
END
ABNORMAL PROCEDURES
Instruments System
05−15−5
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
ABNORMAL PROCEDURES
Instruments System
05−15−6
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
THIS PAGE INTENTIONALLY LEFT BLANK
1. LANDING GEAR, WHEEL AND BRAKE SYSTEM
A. Inboard Anti-Skid Failure
Indication: A/SKID INBD caution message on.
NOTE
A/SKID INBD caution message indicates anti-skid braking is lost on 1
or 2 inboard wheels, or parking brake shut-off valve has failed (PARK
BRAKE SOV caution message on).
CAUTION
Extreme caution is required during braking to avoid tire damage or
blowout. Maximize use of reverse thrust.
(1) Actual landing distance .................................... Increase as applicable by factor given
below:
WITHOUT THRUST REVERSERS WITH THRUST REVERSERS
2.05 (105%) 1.65 (65%)
If excessive asymmetry or loss of braking is observed:
(2) Wheel brakes ....................................................Release momentarily.
(3) ANTI-SKID switch.................................................Select to OFF.
(4) Wheel brakes .................................................. Re-apply as required.
END
ABNORMAL PROCEDURES
Landing Gear, Wheel and Brake System
05−16−1
REV 74, Nov 07/08
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. LANDING GEAR, WHEEL AND BRAKE SYSTEM (CONT'D)
B. Outboard Anti-Skid Failure
Indication: A/SKID OUTBD caution message on.
NOTE
A/SKID OUTBD caution message indicates anti-skid braking is lost on
1 or 2 outboard wheels.
CAUTION
Extreme caution is required during braking to avoid tire damage or
blowout. Maximize use of reverse thrust.
(1) Actual landing distance .................................... Increase as applicable by factor given
below:
WITHOUT THRUST REVERSERS WITH THRUST REVERSERS
2.05 (105%) 1.65 (65%)
If excessive asymmetry or loss of braking is observed:
(2) Wheel brakes ....................................................Release momentarily.
(3) ANTI-SKID switch.................................................Select to OFF.
(4) Wheel brakes .................................................. Re-apply as required.
END
C. Anti-Skid (Inboard and Outboard) Failure
Indication: A/SKID INBD caution message and A/SKID OUTBD caution message on.
NOTE
A/SKID INBD and A/SKID OUTBD caution messages indicate anti-skid
braking is lost on 2 or more wheels.
(1) ANTI-SKID switch.................................................Select to OFF.
CAUTION
Extreme caution is required during braking to avoid tire damage or
blowout. Maximize use of reverse thrust.
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(25)
