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APU Start ........................................................................02-06-03
APU Operation ................................................................02-06-03
Approved Fuels/Oils ........................................................02-06-03
LIMITATIONS
DOT Approved May 30/2003 Airplane Flight Manual 02-01-01
REV 1 CSP 100-1
GENERAL
Observance of the limitations in this Airplane Flight Manual is mandatory.
BASIC LIMITATIONS
KINDS OF OPERATION
This airplane is certificated to the applicable regulations in the transport category
and is eligible for the following kinds of operations when the appropriate
instruments and equipment required by the airworthiness and operating requirements
are installed and approved and are operable.
This airplane is approved for:
- VMC (Visual Meteorological Conditions)
- IMC (Instrument Meteorological Conditions)
- Day
- Night
- Icing
The airplane is certified capable of RVSM operations in accordance with the
FAA “Interim guidance material on the approval of operations/aircraft for
RVSM operations.” 91-RVSM, dated June 30, 1999 and the JAA Temporary
Guidance Leaflet, TGL No.6, revision 1, RVSM.
NOTE: Compliance with the material above does not constitute an operational
approval.
RVSM operations must not be commenced or continued unless all of the
required equipment specified below is operational:
RVSM Required Equipment List
Equipment Requirements for RVSM
Autopilot (1) Must be operational.
Altitude alerting system Must be operational.
Altitude Reporting Transponder (2) One must be operational
Air Data Computers (2) Two must be operational
LIMITATIONS
02-01-02 Airplane Flight Manual DOT Approved May 30/2003
CSP 100-1 REV 1
OPERATION IN ICING CONDITIONS
Do not hold in icing conditions with flaps extended.
Super-Cooled Large Droplet Icing:
Flight in super-cooled large droplet icing (SLD) conditions may, but not necessarily
be indicated by ice accretion on the side windows.
When side window icing is observed:
- Wing and engine anti-icing systems must be on.
- Leave icing conditions as soon as possible.
Engine Anti-Ice Systems:
Ground operations. The engine anti-icing system must be ON when the
outside air temperature (OAT) on the ground and for takeoff is 10 °C (50 °F)
or below and visible moisture in any form is present (such as fog with visibility
of one mile (1500 m) or less, rain, snow, sleet, or ice crystals).
The engine anti-icing system must also be ON when the OAT is 10 °C (50 °F)
or below when operating on ramps, taxiways, or runways where surface snow,
ice, standing water, or slush is present.
Flight operations. Icing conditions exist when the static air temperature
(SAT) in flight is 10 °C (50 °F) to -40 °C (-40 °F) and visible moisture in any
form is present (such as clouds, rain, snow, sleet, or ice crystals).
The engine anti-icing system must be ON when the ICE DETECTED CAS
message is on, or in icing conditions.
Wing Anti-Ice System:
Ground operations. The wing anti-icing system must be ON for takeoff 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 (1500 m) or less, rain, snow, sleet, or
ice crystals).
The wing anti-icing system must also be ON when the OAT is 5 °C (41 °F) or
below when operating on ramps, taxiways, or runways where surface snow,
ice, standing water, or slush is present.
Flight operations. Icing conditions exist when the (SAT) in flight is 10 °C
(50 °F) to -40 °C (-40 °F) and visible moisture in any form is present (such as
clouds, rain, snow, sleet, or ice crystals).
The wing anti-icing system must also be ON when:
- the ICE DETECTED CAS message is on, OR
- in icing conditions.
LIMITATIONS
DOT Approved Aug 16/2005 Airplane Flight Manual 02-01-03
REV 4 CSP 100-1
COLD WEATHER OPERATIONS
Airplane operations in cold weather conditions must be conducted in accordance
with the Flight Crew Operating Manual - Volume 1, Supplement 1 -
COLD WEATHER OPERATIONS.
DITCHING
This airplane is certified for ditching when the appropriate safety equipment is
installed per applicable regulations.
MINIMUM FLIGHT CREW
The minimum flight crew shall consist of a pilot and a copilot.

(METRIC) LIMITATIONS
DOT Approved Feb 02/2005 Airplane Flight Manual 02-02-01
REV 2 CSP 100-1
(Metric)
WEIGHT AND C.G. LIMITATIONS
MAXIMUM RAMP WEIGHT................................................... 38 650 lb
17 532 kg
　
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