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Tecnam P2010 - Page 405

Tecnam P2010
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AFMS N°D07 FOR GARMIN GFC700 AUTOPILOT AND VARIABLE PITCH PROPELLER EQUIPPED
AEROPLANES
Page APV1-13
Section 1 General-
ACRONYMS AND TERMINOLOGY
Ed. 1, Rev.0
Autopilot acronyms
AC
A/C
Advisory Circular
Aircraft
GNSS
GP
Global Navigation Satellite System
Glide Path
ADC
Air Data Computer
GPS
Global Position System
ADF
Automatic Direction Finder
GS
Glide Slope
ADI
Attitude Directional Indicator
GSA
Garmin Servo Actuator
AFCS
AHRS
Automatic Flight Control Systyem
Attitude Heading Reference System
GSM
HDG
Garmin Servo Mount
Heading
ALT
Altitude
HSDB
High Speed Data Bus
ALTS
Altitude Selector
IAU
Integrated Avionic Unit
AMPS
A/P
Ampere
Autopilot
LOC
LRU
Localizer
Line Repleaceable Unit
APR
Approach
LVL
Level
ARP
ASI
Aerospace Recommended Practice
Air Speed Indicator
MAG
MET
Magnetometer
Manual Electric Trim
BC
Back Course
MFD
Multi-Function Display
CAS
Caution Advisory System
NAV
Navigation
CDI
CS
Course Deviation Indicator
Certification Specifications
OAT
PFD
Outside Air Temperature
Primary Flight Display
CWS
Control Wheel steering
PFI
Primary Flight Information
DC
DME
Direct Current
Distance Measuring Equipment
PFT
PWM
Pre Flight Test
Pulse Width Modulation
EIS
Engine Indication System
SAE
SAE International
ESP
Electronic Stability and Protection
TDM
Time Division Multiplexing
FD
FLC
Flight Director
Flight Level Change
USP
VHF
Under Speed Protection
Very-High Frequency
GA
Go Around
VNV
Vertical Navigation
GDU
Garmin Display Unit
VS
Vertical Speed
GIA
Garmin Integrated Avionics
XPDR
Transponder

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