HP d212 Manual do Utilizador Página 8

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FMS-D212-725-1
Page Intro-8
• COPYRIGHT © 2007 BY DART AEROSPACE LTD •
This document is private and confidential and is supplied on the express condition that it is not to be used for any
purpose or copied or communicated to any other person without written permission from Dart Aerospace Ltd.
Revision:
A
Unapproved Date: 07.06.01
FT Foot, Feet
GAS PROD (N
1
) Gas Producer RPM
GEN Generator
GOV Governor
GW Gross Weight
H
D
Density Altitude
H
P
Pressure Altitude
HSI Horizontal Situation Indicator
HTR Heater
HV Height-Velocity
HYDR SYS Hydraulic System
IGE In Ground Effect
IMC Instrument Meteorological Conditions
INCR Increase
INV Inverter
KCAS Knots Calibrated Airspeed
KG Kilogram(s)
KIAS Knots Indicated Airspeed
LB Pound(s)
M Meter(s)
MGT Measured Gas Temperature
MCP Maximum Continuous Power
MIN Minimum, Minutes(s)
NAV Navigation
NON ESS Non Essential
NORM Normal
N
1
Gas Producer rpm
N
2
Power Turbine rpm
N
R
Main Rotor rpm
OAT Outside Air Temperature
OGE Out of Ground Effect
PART SEP Particle Separator
PLT Pilot
PRI Primary
REL Release
RPM Revolutions per Minute
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