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MODEL CL-600-2A12
AIRPLANE FLIGHT MANUAL
PSP 601-1A-1
3. OPERATING LIMITATIONS (Cont'd)
H. OPERATION IN ICING CONDITIONS (Cont'd)
(2) Wing Anti-ice System
(a) Ground Operations
The wing anti-ice system must be on for take-off when the OAT is
5°C (41°F) or below and visible moisture in any form is present
(such as fog with visibility of one mile or less, rain, snow,
sleet and ice crystals).
The wing anti-ice system must also be on for take-off when the
OAT is 5°C (41°F) or below and the runway is contaminated with
surface snow, slush or standing water.
When Type II, III or 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 take-off.
(b) Flight Operations
NOTE
Icing conditions exist in flight at a TAT of
10°C (50°F) or below and visible moisture in
any form is encountered (such as clouds,
rain, snow, sleet or ice crystals), except
when the SAT is -40°C (-40°F) or below.
The wing anti-ice system must be on:
At or above 22,000 feet:
• when ice is indicated by the ice detection system, or
• when in icing conditions, if an ice detector has failed.
Below 22,000 feet:
• when in icing conditions, or
• when ice is indicated by the ice detection system.
(3) Super-Cooled Large Droplet Icing
Continued operation in areas where super-cooled large droplet (SLD)
icing conditions exist is prohibited.
SLD icing conditions are indicated by ice accretion on the flight
compartment side windows.
• The wing anti-icing system must be ON in SLD icing conditions.
• The cowl anti-icing system must be ON in SLD icing conditions.
• Leave icing conditions when side window icing occurs.
DOT Approved
LIMITATIONS Jan 14/05
Page 6B 44,600/45,100
DOT Approved
Sep 11/06
44,600/45,100
LIMITATIONS
Page 6C
3. OPERATING LIMITATIONS (Cont’d)
I. COLD WEATHER OPERATIONS
Take-off is prohibited with frost, ice, snow or slush adhering to any
critical surface (wings, horizontal stabilizer, vertical stabilizer,
control surfaces, engine inlets and upper surface of the fuselage).
W A R N I N G
Even small amounts of frost, ice, snow or
slush on the wing leading edges and forward
upper wing surface may adversely change the
stall speeds, stall characteristics and the
protection provided by the stall protection
system, which may result in loss of control
on take-off.
N O T E
1. Comprehensive procedures for operating in
cold weather are provided in the Operating
Manual Volume 1, SUPPLEMENTARY PROCEDURES,
Cold Weather Operations.
2. Take-off 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 Operating Manual
Volume 1, SUPPLEMENTARY PROCEDURES, Cold
Weather Operations, Pre-Flight Preparation,
External Safety Inspection.
In addition to a visual check, a tactile check of the wing leading edge,
wing forward upper surface and wing rear upper surface is required during
the Walkaround Check List inspection to determine that the wing is free
from frost, ice, snow or slush when the outside air temperature (OAT) is
5C (41F) or less, or it cannot be determined that the wing fuel
temperature is above 0C (32F); and:
 There is visible moisture (rain, drizzle, sleet, snow, fog, etc); or
 Water is present on the wing; or
 The difference between the dew point temperature and the OAT is
3C (5F) or less; or
 The atmospheric conditions have been conducive to frost formation.
N O T E
Ice and frost may continue to adhere to wing
surfaces for some time even at outside air
temperatures above 5C (41F).
MODEL CL−600−2A12
AIRPLANE FLIGHT MANUAL
PSP 601−1A−1
LIMITATIONS
Page 6D
DOT Approved
Sep 11/06
44,600/45,100
THIS PAGE INTENTIONALLY LEFT BLANK
MODEL CL−600−2A12
AIRPLANE FLIGHT MANUAL
PSP 601−1A−1
DOT Approved
Jan 30/07
44,600/45,100
LIMITATIONS
Page 7
4. POWER PLANT LIMITATIONS
A. ENGINES
Type: Two General Electric CF34-1A or
Two General Electric CF34-3A or
Two General Electric CF34-3A2
N O T E
Mixing of CF34-1A, CF34-3A and CF34-3A2
engines is permitted.
B. ENGINE OPERATING LIMITS
Condition N1
(% rpm)
N2
(% rpm)
ITT
(C)
Time Limit
for ITT
Maximum take-off (APR operating) 98.6 99.4 857 5 minutes
　
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