Specifications

INTRODUCTION
MODEL 560
Demonstrated Crosswind: The demonstrated crosswind velocity of 30 knots (measured at 30
feet above the runway surface) is the velocity of the crosswind
component for which adequate control of the airplane during takeoff
and landing was actually demonstrated during certification tests.
This is not limiting. The demonstrated crosswind velocity for an
airplane using thrust reversers is 30 knots.
DG: Directional Gyro
DH: Decision Height
DME: Distance Measuring Equipment
Engine Cycle: Any operational sequence involving engine start, power to 80
percent N
1
or above and engine shutdown.
Engine Out Accelerate-Go The
horizontal distance from brake release to the point where the
Distance airplane attains a height of 35 feet above the runway surface on a
takeoff during which an engine is recognized to have failed at V
1
and the takeoff is continued.
°F: Temperature in degrees Fahrenheit
FAA: Federal Aviation Administration
Flameout: Unintentional loss of engine during operation.
FM: Frequency Modulation
G: Acceleration due to gravity. One G equals the pull of gravity with
no acceleration.
Gross Climb Gradient: The climb gradient that the airplane can actually achieve with ideal
ambient conditions (smooth air).
HF: High Frequency
Hot Start: An engine start, or attempted start, which results in an interstage
turbine temperature exceeding 550°C or which otherwise exceeds
the engine starting temperature envelope limits.
Hr: Hour
HSI: Horizontal Situation Indicator
Hz: Hertz
In. Hg: Inches of Mercury
IOAT: The indicated outside air temperature as read from the pilot’s panel.
It is the same as RAT.
IFR: Instrument Flight Rules
I 56OMB-01 Configuration AA Introduction-7