曝光台 注意防骗
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A hard landing is described as follows:
• A landing at a vertical descent rate greater than 600 feet per minute or 10 feet per
second when the aircraft gross weight is less than or equal to the maximum landing
weight.
• A landing at a vertical descent rate greater than 360 feet per minute or 6 feet per second
when the aircraft gross weight is greater than the maximum landing weight, but less than
or equal to the maximum take-off weight.
• A landing where the aircraft makes a skid on the prepared runway surface, or lands with
an uncontrolled sideways skid or continues to move from the prepared surface to a
runway surface that is not prepared.
• A landing where the aircraft touches the ground with one or more landing gear on a
surface other than the prepared surface.
• A landing where the aircraft nose landing gear touches the ground before both main
landing gear have touched the ground.
• A landing where the aircraft bounces or skips after initial impact and the ground spoilers
subsequently deploy while the aircraft is still in the air.
• A landing that results in a burst tire.
A hard de-rotation is described as follows:
• The brakes were applied before the nose landing gear touches the ground.
• Full or nearly full nose-down elevator was applied before the nose landing gear touches
the ground.
• Forward column pressure was applied by the pilot at a high pitch attitude, following main
landing gear touchdown, in order to rapidly lower the nose landing gear to the ground.
NORMAL PROCEDURES
Approach and Landing
Vol. 1 04−08−19
REV 77, Oct 20/09
CL−604 Operating Manual
PSP 604−6
NORMAL PROCEDURES
Approach and Landing
Vol. 1 04−08−20
REV 77, Oct 20/09
CL−604 Operating Manual
PSP 604−6
THIS PAGE INTENTIONALLY LEFT BLANK
1. SHUTDOWN
A. Shutdown Check
The following procedures will be accomplished when the airplane has come to a complete
stop.
(1) PARKING BRAKE ....................................... As required Ensure that chocks are in
place before releasing parking
brake.
NOTE
Inform ground crew of ‘Hot Brakes’ condition as soon as
possible.
(2) Thrust reverse levers..............................................Stow Check the following:
• REV icon goes out.
• REV UNLOCKED caution
message out.
(3) APU (if required)..................................................... Start Ensure that operating
limitations/envelope is
considered.
NOTE
The APU, PWR FUEL switch/light must be selected off between
each APU start attempt. The APU, PWR FUEL switch/light
should be firmly pressed once only. If pressed twice, an
immediate shutdown may occur.
(a) BLEED AIR, APU LCV
switch/light ....................................................Check pressed out.
(b) APU, PWR FUEL switch/light .................... Press in and check the following:
• PWR FUEL light on, and
• APU gauges displayed on
status page.
(c) APU, START/STOP switch/light................ Press in and check the following:
• START light on.
• 60% rpm – START light out.
NOTE
Greater than 30% rpm
within 60 seconds.
• 95% rpm + 4 seconds
(approx) – AVAIL light on.
• 100% rpm + 15 seconds
(approx) – APU GEN OFF
caution message on.
NORMAL PROCEDURES
Shutdown
Vol. 1 04−09−1
REV 66, Feb 01/07
▼
CL−604 Operating Manual
PSP 604−6
1. SHUTDOWN (CONT'D)
A. Shutdown Check (Cont’d)
On airplanes 5301 to 5360 not incorporating Service Bulletin 604–49–006 or 604–49–009:
(c) APU, START/STOP switch/light................ Press in and check the following:
• START light on.
• 60% rpm – START light
out.
NOTE
Maximum 60 seconds
below 60% rpm.
• 95% rpm + 4 seconds
(approx) – AVAIL light on.
• 100% rpm + 15 seconds
(approx) – APU GEN OFF
caution message on.
After APU RPM and EGT have stabilized:
(d) AC POWER, APU GEN switch..................... Select to ON.
If APU is unavailable:
(3) EXT POWER, AC switch/light ...........................Press in Check IN USE light on.
(4) AC POWER, GEN 1 and 2
switches................................................................Select to OFF/RESET.
After the engine two minute cool-down period:
(5) Engine that was started first ...........................Shutdown
NOTE
Prior to shutdown, operate the engine at or near IDLE for a minimum of
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庞巴迪挑战者604操作手册 Operating Manual 1(104)
