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transition from take-off to enroute configuration is completed,
whichever is higher.
Take-Off Flight Path The take-off flight path begins at the end of the take-off distance
and at a height of 35 feet above the take-off surface, and ends at
1,500 feet above the take-off surface, or at the point where
transition from take-off to enroute configuration is completed,
whichever is higher. This is also known as the Gross Take-off Flight
Path.
Net Take-Off Flight
Path
The net take-off flight path is the gross take-off flight path
diminished by 0.8% climb gradient capability (or equivalent
reduction in acceleration along that part of the take-off flight path at
which the airplane is accelerated in level flight). The net take-off
flight path must clear all obstacles in the take-off area by at least
35 feet vertically.
INTRODUCTION
General
01−01−6
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
4. DEFINITIONS (CONT'D)
E. Climb Gradient
Climb Gradient The ratio of the change in height, during a portion of a climb, to the
horizontal distance traversed in the same time interval.
Gross Gradient Climb gradient expressed as a percentage ratio, obtained using the
following formula:
(Change in height ÷ Horizontal distance travelled) x 100
The gradients shown on the charts are based on true (not
pressure) rates of climb.
Net Gradient The gross gradient reduced by the required margins.
First Segment The first segment starts from the 35-foot height and extends to the
point where the landing gear is fully retracted, at a constant V2
speed and flaps in the take-off position.
Second Segment The second segment starts at the point where the landing gear is
fully retracted up to at least 400 feet above the runway, flown at V2
speed and flaps in the take-off position.
Acceleration Segment The acceleration segment is the part of the take-off flight path that
begins at the end of the second segment and extends horizontally
over the distance required to retract flaps to zero, and accelerate to
the final take-off climb speed.
Final Segment The final segment starts from the end of the acceleration segment
and extends to the end of the take-off flight path, flown at the final
segment climb speed, flaps up.
F. Miscellaneous
APR Automatic performance reserve – In the event of an engine failure
during take-off, the APR system, if operating, will increase the
thrust rating of the remaining engine.
The APR rating must be set manually in the event of a
single-engine go-around.
Centre of Gravity (c.g.) The point at which the airplane would balance if suspended. The
c.g. distance from the reference datum is found by dividing the total
moment by the total weight of the airplane.
GW Gross weight – The maximum weight to which the airplane is
certificated.
MLW Maximum landing weight - The maximum airplane weight approved
for the landing touchdown at a maximum descent velocity of 10 feet
per second.
MTOW Maximum take-off weight – The maximum airplane weight
approved for the start of take-off or for landing at a reduced
descent velocity not to exceed 6 feet per second.
MZFW Maximum zero fuel weight.
INTRODUCTION
General
01−01−7
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
5. ABBREVIATIONS
The following abbreviations may be used by flight compartment displays, radio tuning units and
flight management system or be found throughout the manual. Some abbreviations may also
appear in lower case letters. Abbreviations having very limited usage are explained in the
systems chapters where they are used.
A
A/C Air-Conditioning
A/G Air/Ground
A/ICE Anti-ice
A/P Autopilot
A/S Airspeed
A/SKID Anti-skid
ABS Absolute
AC Alternating Current
ACCEL Acceleration, accelerate(d),
accelerometers
ACM Air Cycle Machine
ACMP Alternating Current Motor
Pump/Electric Hydraulic
Pump
ACT Active
ACU Air-Conditioning Unit
ADC Air Data Computer
ADDR Address
ADF Automatic Direction Finder
ADG Air Driven Generator
ADI Attitude Director Indicator
ADS Air Data System
AFCS Automatic Flight Control
System
AFT Afterward
AGL Above Ground Level
AHC Attitude Heading Computer
AIL Aileron
ALIGN Aligning, alignment
ALPHA Alpha
ALT Altitude, Altimeter
ALT Altitude Hold (PFD/FD)
ALT CAP Altitude Capture (PFD/FD)
ALT HOLD Altitude Hold
ALTN Alternate
　
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