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
The maximum crosswind component for takeoff and landing on a wet runway
with water depth no more than 3.00 mm (0.125 inch) is defined in the
following table for different values of the coefficient of friction:
1. Operation on runways with a coefficient of friction less than 0.3 is
prohibited.
MAXIMUM CROSSWIND COMPONENT -
CONTAMINATED RUNWAYS
1. The maximum crosswind component for takeoff and landing on a
contaminated runway is 10 knots (5 meters/sec).
2. Operation on runways with a coefficient of friction less than 0.3 is
prohibited.
Reported Runway
Coefficient of Friction
Maximum Crosswind
Component
0.3 - 0.35 (Poor braking) 10 knots (5 meters/sec)
0.35 - 0.5 (Medium braking) 15 knots (8 meters/sec)
0.5 - 0.6 (Good braking,
equivalent to dry)
Takeoff - 28 knots (14 meters/sec)
Landing - 24 knots (12 meters/sec)
EFFECTIVITY
LIMITATIONS
DOT Approved Jul 31/2006 Airplane Flight Manual 02-03-05
REV 6 CSP 100-1
OPERATIONAL LIMITATIONS (Cont)
COLD WEATHER OPERATIONS (Cont)
NOTE: - Comprehensive procedures for operating in cold weather are
provided in the Flight Crew Operating Manual, Supplement 1 -
Cold Weather Operations.
- Takeoff is permitted with frost adhering to the underside of the
wing that is caused by cold soaked fuel, in accordance with the
instructions provided in the Flight Crew Operating Manual,
Supplement 1 - Cold Weather Operations.
EN ROUTE
Maximum Pressure Altitude ........................................................45 000 ft
MANEUVERING LOAD FACTORS
Flaps Up .............................................................................+2.6 g to -1.0 g
Flaps Extended.................................................................. +2.0 g to 0.0 g
OPERATION WITH TYPE II, III & IV ANTI-ICING FLUIDS
When Type II, III & IV anti-icing fluids have been applied:
The wing anti-ice system must only be selected ON, if required, just prior to
thrust increase for takeoff.
MANEUVERS
Aerobatic maneuvers and spins are prohibited.
LIMITATIONS
02-03-06 Airplane Flight Manual DOT Approved Jul 31/2006
CSP 100-1 REV 6
OPERATIONAL LIMITATIONS (Cont)
ALTITUDE/TEMPERATURE LIMITATIONS
Figure 02-03-02
ALTENV_BD100_30OCT02
80 70 60 50 40 30 20 10 0 10 20 30 40 50 60
TEMPERATURE oC
5
0
5
10
15
20
25
30
35
40
45
50
PRESSURE ALTITUDE 1000 FEET
For aircraft 20006 thru 20033 not incorporating Service Bulletin
SB100-52-05 (Replacement of Passenger Door Telescopic Struts for
Improved Cold Weather Operation):
Operation is prohibited if the airplane, with engines shut down, is exposed to
a ground ambient temperature of -20 °C (-4 °F) or below for a period of more
than 2 hours, unless an approved procedure is used to warm the airplane
following this exposure.
EFFECTIVITY
LIMITATIONS
DOT Approved Aug 16/2005 Airplane Flight Manual 02-04-01
REV 4 CSP 100-1
SYSTEMS LIMITATIONS
AIR CONDITIONING AND PRESSURIZATION
AIR CONDITIONING
Do not select the AIR SOURCE switch to TRIM AIR ONLY while the aircraft
is on the ground.
The pack must be operating (APU or engine running and AIR SOURCE
switch— NORM or PACK ONLY) when the aircraft electrical power is
on (BATTs or EXT PWR — On) for more than 30 minutes and the OAT is
above 40 °C (104 °F).
OXYGEN
The following aircraft certification requirements are in addition to the requirements
of applicable operating rules. The most restrictive requirements (certification
or operating) must be observed.
Crew and passenger oxygen masks are not approved for use above 40 000 feet
cabin altitude. Prolonged operation of passenger masks above 25 000 feet
cabin altitude is not recommended.
PRESSURIZATION
The maximum differential pressure on the ground (during taxi) must not
exceed 0.1 psi.
The maximum differential pressure during landing must not exceed 1.0 psi.
The maximum positive differential pressure is 9.4 psi. The maximum negative
differential pressure is -0.5 psi.
AUTOFLIGHT
Do not intentionally overpower the autopilot.
Operation with an ILS glidepath angle that exceeds 3.5 degrees is prohibited.
Autopilot Minimum Use Height:
Climb, En Route, or Descent..................................................... 700 feet AGL.
Approach
Precision............................................................................... 80 feet AGL.
Visual and non-precision.................................................... 200 feet AGL.
The maximum altitude with yaw damper off is 31 000 ft.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
Bombardier_Challenger_Global_00-Limitations(5)
