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Chapter
sample pagination
Page Number
Section Within Chapter
01−01−2
GF0203_003
Additional identification data carried in the margin of the page are the date of issue or revision
date printed below the page number and the chapter title and subject carried in the masthead.
INTRODUCTION
General
01−01−2
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
3. PAGINATION (CONT'D)
Blank pages resulting from the end of a section and back-up pages for foldout illustrations or
illustrations that must be arranged as facing pages are provided to avoid the impression that a
page is missing. These pages are numbered and are included in the List of Effective Pages.
4. DEFINITIONS
The following definitions are for terms commonly used throughout the manual. Items not
commonly used will be defined in the respective sections where they apply.
A. Airspeeds
IAS Indicated airspeed – Airspeed indicator reading corrected for
instrument error. Values in this manual assume zero instrument
error.
CAS Calibrated airspeed – Indicated airspeed corrected for static source
position error.
EAS Equivalent airspeed – Calibrated airspeed corrected for
compressibility.
TAS True airspeed – Equivalent airspeed corrected for density.
M Indicated Mach number – Machmeter reading corrected for
instrument error.
MT True Mach number – Machmeter reading corrected for both
instrument and static source position errors.
V1 Take-off decision speed (formerly designated as Critical engine
failure recognition speed) – The speed used as a reference at
which, due to engine failure or other causes, the pilot may elect to
stop or continue the take-off.
V1MBE Maximum V1 for brake energy – The maximum speed on the
ground from which a stop can be accomplished within the energy
capabilities of the brakes.
V1MCG Minimum V1 limited by control on the ground – The take-off
decision speed following an engine failure at VMCG. V1 may not be
less than V1MCG.
V2 Take-off safety speed – Target climb speed to be attained at or
before a height of 35 feet above the runway during a continued
take-off, following an engine failure.
VA Design maneuvering speed – The maximum speed at which
application of full available aileron, rudder or elevator will not
overstress the airplane.
VEF Critical engine failure speed – The speed at which, if the critical
engine fails, the engine failure is recognized at V1.
VFE Maximum flap extended speed – is the highest speed permissible
with the wing flaps in a prescribed extended position.
VFTO Final take-off climb speed – The speed attained at the end of the
flight path acceleration segment during a continued take-off
following an engine failure, and is the climb speed scheduled for
the final take-off climb.
INTRODUCTION
General
01−01−3
REV 67, Mar 19/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
4. DEFINITIONS (CONT'D)
A. Airspeeds (Cont’d)
VLE Maximum landing gear extended speed – The maximum speed at
which the airplane can be safely flown with the landing gear
extended.
VLO Maximum landing gear operating speed – The maximum speed at
which the landing gear can be safely extended or retracted.
VMO/MMO Maximum Operating Limit Speed/Mach Number – The maximum
operating limit speed (airspeed or Mach number) is the speed that
may not be deliberately exceeded in any regime of flight (climb,
cruise, or descent) unless a higher speed is authorized for flight test
or pilot training operations.
VMCA Minimum control speed, air – Minimum flight speed at which the
airplane is controllable with a maximum of 5° bank, when the
critical engine suddenly becomes inoperative, with the remaining
engine at maximum take-off thrust.
VMCG Minimum control speed, ground – Minimum speed on the ground at
which control can be maintained and the take-off continued using
aerodynamic controls alone, when the critical engine suddenly
becomes inoperative, with the remaining engine at maximum
take-off thrust.
VMCL Minimum control speed during landing approach – Minimum flight
speed at which the airplane is controllable with a maximum of 5°
bank, when the critical engine suddenly becomes inoperative, with
the remaining engine at maximum take−off thrust.
VR Rotation speed – Speed at which rotation is initiated during take-off.
VREF Approach speed – The landing reference speed at a height of 50
　
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