abriviations Flashcards
LSS
Lightning Sensor System
MAU
Modular Avionic Unit
MCDU
Multifunction Control Display Unit
MCL
Master Caution Light
MCP
Maximum Continuous Power
MDA
Minimum Descent Altitude
MFD
Multifunction Flight Display
MGB
Main Gear Box
MLG
Main Landing Gear
MRC
Modular Radio Cabinet
Nf
Power Turbine Speed
Ng
Gas Generator Speed
NLG
Nose Landing Gear
NR
Rotor Speed
NVG
Night Vision Goggle
OEI
One Engine Inoperative
OGE
Out of Ground Effect
PCM
Power Control Module
PFD
Primary Flight Display
PI
Power Index
PLA
Power Lever Angle (Throttle)
PMS
Power Management Switch
RAIM
Receiver Autonomous Integrity Monitor
RCP
Reconfiguration Control Panel
Reversion Control Panel
RFM
Rotorcraft Flight Manual
RNP
Required Navigation Performance
SAS
Stability Augmentation System
SID
Standard Instrument Departure
SOV
Shut-Off Valve
TA
Terrain Awareness
TAWS
Terrain Awareness and Warning System
TCAS
Traffic Collision and Alert System
TOC
Top of Climb
TOD
Top of Descent
TOP
Take off Power
TRSOV
Tail Rotor Shut Off Valve
TVC
Temperature Control Valve
VMS
Vehicle Monitoring System
Vlo
Maximum landing gear operation speed
Vle
Maximum landing gear extended speed
Vmini
Minimum airspeed for flight under IFR
Vne
Never exceed speed
VSI
Vertical Speed Indicator
Vy
Speed for best rate of climb
W.A.T.
Weight Altitude Temperature
WOW
Weight on Wheels
WX
Weather radar
Xfer
Transfer
XPDR
Transponder
AGL
Above Ground Level
AHRS
Attitude Heading Reference System
AP
Auto Pilot
ATT
Attitude hold
AWG
Aural Warning Generator
BL
Buttock Line
BOD
Bottom of Descent
BOW
Basic Operating Weight
CAT
Category
CCD
Cursor Control Devices
CCP
Cockpit Control Panel
CLTV
Collective
CPI
Crash Position Indicator
CVR
Cockpit Voice Recorder
DAU
Data Acquisition Unit
DCU
Data Collection Unit
DFDAU
Digital Flight Data Acquisition Unit
DGPS
Differential Global Position System
DH
Decision Height
EAPS
Engine Air Particle Separator
EASA
European Aviation Safety Agency
ECL
Engine Control Lever
ECS
Environmental Control System
ECU
Engine Control Unit
EDU
Electronic Display Unit
EEC
Electronic Engine Control
EFIS
Electronic Flight Instrument System
EGPWS
Enhanced Ground Proximity Warning System
EPU
Estimated Position Uncertainty
ESIS
Electronic Standby Instrument System
FAF
Final Approach Fix
FCU
Fuel Computer Unit
FD
Flight Director
FDR
Flight Data Recorder
FMM
Fuel Management Module
FMS
Flight Management System
FTR
Force Trim Release
GA
Go Around
GC
Guidance Controller
GW
Gross Weight
Hp
Pressure altitude
HPS
Hydraulic Power Supply
HSI
Horizontal Situation Indicator
IAS
Indicated Air Speed
IGB
Intermediate Gear Box
IGE
In Ground Effect
ILS
Instrument Landing System
ISA
International Standard Atmosphere
ITT
Inter Turbine Temperature
JAR
Joint Aviation Requirements
LG
Landing Gear
LGCP
Landing Gear Control Panel
APV
APproach with Vertical guidance
APCH
APproaCH
AR
Authorization Required
FAS
Final Approach Segment
FPAP
Flight Path Alignment Point
FTP
Fictitious Threshold Point
GNSS
Global Navigation Satellite System
GPA
Glide Path Angle
GPS
Global Positioning System
LPV
Localizer Performance with Vertical guidance
LNAV
Lateral NAVigation
LTP
Landing Threshold Point
MAP
Missed Approach Point
MSA
Minimum Safe Altitude
NLOC
Navigation LOCalizer
NGS
Navigation Glide Slope
PINS
Point IN Space
RF
Radius to Fix
RNAV
aRea NAVigation
RNP
Required Navigation Performance
ROD
Rate Of Descent
SBAS
Satellite Based Augmentation System
VNAV
Vertical NAVigation
VGP
Vertical Glide Path
ADC
Air Data Computer
ADI
Attitude Display Indicator
AFCS
Automatic Flight Control System
CAS
Crew Alerting System
CRS
Course
DOC
Documentation
MPOC
Minimum Pitch On Ground
OAC
Power Assurance Check
RA
Resulution Advisory
TA
Traffic Advisory
Zp
Pressure Alt
EHSI
Electronic Horizontal Situation Indicator
ACAS
Airborne Collision Avoidance System