Technical data

Document N° :
F2-1.0/R80/F/EU
Pioneer 200
Flight Manual
Section: 0
REVISION :
0
Dated: 20-04-2002
Sect : 0 -Page: 7 of 8
By :www.aeroprogetti.net
V x BEST ANGLE-OF-CLIMB
SPEED
The speed which results in the greatest gain of altitude
in a given horizontal distance.
V y BEST RATE-OF-CLIMB SPEED The speed which results in the greatest gain in altitude
in a given time.
METEOROLOGICAL TERMINOLOGY
OAT OUTSIDE AIR
TEMPERATURE
The free static air temperature. It is expressed in either
degrees Celsius or degrees Fahrenheit.
STANDARD TEMPERATURE Standard Temperature is 15 degrees C at sea level
pressure altitude.
PRESSURE ALTITUDE The altitude read from the an altimeter when the
altimeter's barometric scale has been set to 1013 mb
(29.92 inches of mercury).
ENGINE POWER TERMINOLOGY
BHP BRAKE HORSEPOWER The power developed by the engine.
RPM REVOLUTIONS PER MINUTE Engine speed.
STATIC RPM The engine speed attained during a full-throttle engine
runup when the airplane is on the ground and
stationary.
AIRPLANE PERFORMANCE AND FLIGHT PLANNING TERMINOLOGY
MAXIMUM CROSSWIND VELOCITY The velocity of the crosswind component for which
adequate control of the airplane during takeoff and
landing was actually demonstrated during the
certification tests. The value shown is limiting.
USEABLE FUEL The fuel available for flight planning
UNUSABLE FUEL The quantity of fuel that cannot be safely used in flight
LPH LITRES PER HOUR The amount of fuel ( in litres ) consumed per hour
NMPL NAUTICAL MILES PER
LITRE
The distance ( in nautical miles ) which can be
expected per litre of fuel consumed at a specific
engine power setting and/or flight configuration.
g The acceleration due to gravity.