Symbols And Abbreviations - Guimbal CABRI G2 Flight Manual

Hélicoptères Guimbal
CABRI G2

Symbols and abbreviations

Symbol or abbreviation
Speeds
CAS ......................................................................... Calibrated airspeed
IAS............................................................................. Indicated airspeed
TAS .................................................................................. True airspeed
V ......................................................................... Never-exceed speed
NE
Vy ..................................................................... Best rate-of-climb speed
Meteorology
ISA.................................................... International standard atmosphere
OAT ................................................................... Outside air temperature
P ............................................................................. Outside air pressure
............................................................................... Relative air density
Altitude / Height
AGL .......................................................................... Above ground level
Z ................................................................................ Geometric altitude
Zp ................................................................................ Pressure altitude
Z ...................................................................... Relative density altitude
h .................................................................................. Geometric height
Power / Engine parameters
FLO ..................................................... First MLI limit is Full throttle limit
MCP ........................................................... Maximum continuous power
MLI ....................................................................... Multiple limit indicator
NR ....................................................................................... Rotor speed
NM .................................................................................... Engine speed
PWR ............................................................ First MLI limit is Power limit
Hover / Take-off / Landing
IGE ................................................................................ In ground effect
OGE ........................................................................ Out of ground effect
HIGE .................................................................... Hover in ground effect
HOGE ............................................................ Hover out of ground effect
Weight and balance
CG ................................................................................ Centre of gravity
MTOW ............................................................. Maximum take-off weight
Equipment
EPM.................................................................... Electronic Pilot Monitor
BARC ................................................ Boîtier Alarme Rotor et Carburant
RRM / GOV ................................................................. Engine governor
Original issue
Approved under DOA EASA.21J.211
SECTION 1
Designation
(Fuel and rotor alarm device)
GENERAL
1-5