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surface.
Position Correction: A correction applied to indicated airspeed or altitude to eliminate the
effect of the location of the static pressure source on the instrument
reading. No position corrections are required when using performance
section charts in Section IV since all airspeeds and altitudes in this
section are presented as “indicated” values except for stall speeds
which are presented as “calibrated” values.
RAT: Ram Air Temperature. RAT is displayed on each PFD. RAT is
ambient air temperature increased by ram rise due to Mach Number.
On the ground with engine(s) operating, RAT is ambient temperature.
Reference Zero: The point in the takeoff flight path at which the airplane is 35 feet
above the takeoff surface and at the end of the takeoff distance
required.
Stall Warning-HIGH: When the STALL WARN HI CAS message is displayed, the Stall
Warning-HIGH Performance tables should be used.
Stall Warning-NORMAL: When the STALL WARN HI CAS message is not displayed, the Stall
Warning-NORMAL Performance tables should be used.
Takeoff Climb Increment
(TCI):
Altitude increment to be added to the airport barometric altitude to
obtain level off altitude. This increment includes corrections for nonstandard
temperature.
Takeoff Field Length: The Takeoff Field Length given for each combination of gross weight,
ambient temperature, altitude, wind and runway gradients is the
greatest of the following:
a. 115 percent of the two-engine horizontal takeoff
distance from start to a height of 35 feet above runway
surface.
b. Accelerate-stop distance.
c. The engine-out accelerate-go distance.
No specific identification is made on the charts as to which of these
distances governs a specific case.
510FM-05 AA 4-9
SECTION IV - PERFORMANCE MODEL 510
GENERAL
FAA APPROVED
U.S. Configuration
DEFINITIONS (Continued)
(Continued Next Page)
TEMP Ambient Temperature used to determine airplane performance from
performance charts. For takeoff performance, use RAT displayed on
each PFD with engine(s) operating. For landing performance, use
reported temperature from an appropriate ground station.
True Airspeed (KTAS): The airspeed (knots) of an airplane relative to undisturbed air.
V1: Takeoff Decision Speed. The distance to continue the takeoff to 35
feet will not exceed the scheduled takeoff field length if recognition
occurred at V1 (accelerated-go). The distance to bring the airplane to
a full stop (accelerated-stop) will not exceed the scheduled takeoff
field length provided that the brakes are applied at V1.
V2: Takeoff Safety Speed. This climb speed is the actual speed at 35 feet
above the runway surface as demonstrated in flight during takeoff with
one engine inoperative.
VAPP: The landing approach climb airspeed (1.3 VS1) with 15° flap position,
landing gear UP.
VENR: Single-engine enroute climb speed.
VFE: Maximum flap extended speed. The highest speed permissible with
wing flaps in a prescribed extended position.
VLE: Maximum landing gear extended speed. The maximum speed at
which an 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.
VMCA: Minimum airspeed in the air at which directional control can be
maintained, when one engine is suddenly made inoperative. VMCA is
a function of engine thrust which varies with altitude and temperature.
The VMCA presented was determined for maximum takeoff thrust.
Flaps 0° VMCA = 92 KIAS
Flaps 15° VMCA = 81 KIAS
4-10 AA 510FM-05
MODEL 510 SECTION IV - PERFORMANCE
GENERAL
FAA APPROVED
Configuration U.S.
DEFINITIONS (Continued)
VMCG: Minimum airspeed on the ground at which directional control can be
maintained, when one engine is suddenly made inoperative, using
only aerodynamic controls. VMCG is a function of engine thrust which
varies with altitude and temperature. The VMCG presented was
determined for maximum takeoff thrust.
VMCG = 73 KIAS.
VMO/MMO: Maximum operating limit speed.
VO: The maximum operating maneuvering speed is the maximum speed
at which application of full available aerodynamic control will not
overstress the airplane.
VR: The rotation speed is the speed at which rotation is initiated during
takeoff to attain the V2 climb speed at or before a height of 35 feet
above runway surface has been reached.
VREF: The airspeed equal to the landing 50-foot point speed with Flaps
LAND (Stall Warning-NORMAL) or with Flaps 15° (Stall Warning-
　
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