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CSP C-012 DOT Approved
REV 2, Feb 24/04
LIMITATIONS
Operating Limitations
02--04--2
2. OPERATION IN ICING CONDITIONS
A. Cowl Anti-ice System
Ground Operations
S The cowl anti-ice system must be ON when the OAT is 10°C (50_F) or below and visible
moisture in any formis present (such as fogwith visibility of 1,500meters (onemile) or less,
rain, snow, sleet and ice crystals).
S The cowl anti-ice system must also be ON when the OAT is 10°C (50_F) or below when
operating on runways, ramps, or taxiways where surface snow, ice, standing water, or
slush is present.
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.
S The cowl anti-ice systemmust be ON:
S When in icing conditions, or
S when ICE is annunciated by the ice detection system.
Airplane Flight Manual
CSP C-012 DOT Approved
REV 2, Feb 24/04
LIMITATIONS
Operating Limitations
02--04--3
2. OPERATION IN ICING CONDITIONS (CONT’D)
B. Wing Anti-ice System
Ground Operations
S Thewing anti-ice systemmust be ONfor take-offwhen theOAT is 5°C (41_F) or belowand
visiblemoisture in any form is present (such as fog with visibility of 1,500meters (onemile)
or less, rain, snow, sleet and ice crystals).
S Thewing anti-ice systemmust also beONfor take-offwhen theOAT is 5°C (41_F) orbelow
and the runway is contaminated with surface snow, slush or standing water.
S When Type II, III or Type 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.
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.
S The wing anti-ice system must be ON:
S When ICE is annunciated by the ice detection system, or
S when in icing conditions and the airspeed is less than 230 KIAS.
S Do not hold in icing conditions with the flaps / slats extended.
C. Super-Cooled Large Droplet Icing
S Continued operation in areas where super-cooled large droplet (SLD) icing conditions
exist is prohibited.
S SLD icing conditions are indicated by ice accretion on the flight compartment side
windows.
S The wing anti-icing system must be ON in SLD icing conditions.
S The cowl anti-icing system must be ON in SLD icing conditions.
S Leave icing conditions when side window icing occurs.
Airplane Flight Manual
CSP C-012 DOT Approved
REV 3, May 03/05
LIMITATIONS
Operating Limitations
02--04--4
3. COLD WEATHER OPERATIONS
Airplane operations in coldweather conditionsmust be conducted in accordancewith FlightCrew
Operating Manual Volume 2, Chapter 7, SUPPLEMENTARY PROCEDURES --- Cold Weather
Operations.
4. RUNWAY SLOPES
The maximum runway slopes approved for take-off and landing are:
+2% (uphill)
-- 2% (downhill)
5. TAILWIND CONDITIONS
The maximum tailwind component approved for take-off and landing is 10 knots.
6. MINIMUM FLIGHT CREW
The minimum flight crew is one pilot and one copilot.
7. CARGO
Flight must be within 60 minutes of a suitable airport, if cargo is carried in either cargo
compartment.
Airplane Flight Manual
CSP C-012 DOT Approved
Sep 09/02
LIMITATIONS
Power Plant
02--05--1
1. ENGINES
Type: General Electric CF34-8C5, quantity two.
A. Engine Indications
The engine limit display markings on EICAS must be used to determine compliance with the
maximum/minimum limits and precautionary ranges. If EICAS markings show more
conservative Limits than those specified below, the limit markings on the EICAS must be
used.
NOTE
Red -- Maximum and minimum Limitations
Amber -- Caution range
Green -- Normal operating range.
CF 34-8C5
INDICATION RED AMBER GREEN
N1 % RPM 99.5 -- 0 to 99.4
N2 % RPM 99.4 -- 0 to 99.3
ITT °C Variable -- Variable
OIL TEMP °C 164 156 to 163 -- 40 to 155
OIL PRESS psi 0 to 24 Variable Variable
B. Thrust Management Data
At take-off when the thrust levers are set to TOGA, the crew must verify the target N1 values
displayed correspond to the data presented on the thrust setting charts (±0.5%). Refer to
PERFORMANCE -- THRUST SETTINGS.
C. Engine Warm-up
The engine must remain at IDLE until oil pressure reaches normal operating range
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