LSK
Line Select Key
TLB
Technical Log Book
THS
Trimmable Horizontal Stabilizer
EFIS
FCU
FMA
FMA 3 Colors
Electronic Instrument System ( EIS )
Consists of:
• Electronic Flight Instrument System ( EFIS )
• Electronic Centralized Aircraft Monitor ( ECAM )
ECAM
Electronic Centralized Aricraft Monitor
E/WD
Engine & Warning Display
SD
System Display
MCDU
Multipurpose Control Display Unit
ADR
Air Data Reference
ADIRS
Air Data Inertial Reference System
FADEC (ECU)
Full authority digital engine control (FADEC) (digitale Motorsteuerung mit allen Befugnissen) wird in der Luftfahrt im Allgemeinen eine autonome, volldigitale Triebwerksregelung verstanden
LGCIU
Landing Gear Control Interface Unit
SDAC
System Data Aquisition Concentrators
FWC
Flight Warning Computer
DMC
Display Management Computer
DFDR (Recorder)
Digital Flight Data Recorder
FDIU (Data)
Flight Data Interface Unit
QAR (Recorder)
Quick Access Recorder
SRS
Speed Reference System
SRS mode is a TAKE OFF or GO AROUND mode, the thrust is fixed and the pitch will maintain the min speed to V2 +10 with 2 engines and V2 in case of an engine failure; this mode requires slats being extended and it stops at acceleration altitude
FAC
Flight Augmentation Computer
RMP
Radio Management Panel
TAD (Terrain)
Terrain Awareness and Display
TCF (Terrain)
Terrain Clearance Floor
IDG
Integrated Drive Generatos
TR
Transformer Rectifier Unit
RAT
Ram Air Turbine
ACP
Audo Control Panel
SEC
Spoiler Elevator Computer
ELAC
Elevator and Aileron Computer
CVR
Cockpit Voice Recorder
CRT
Cathode Ray Tube
PTU
Power Transfer Unit
Between green and yellow system
FCDC (Data)
Flight Control Data Concentrators
CFDS (Fault)
Centralized Fault Display System
LAF
Load Alleviation Function
SFCC
Slats Flaps Control Computer
WTB
Wing Tip Brake
EIU
Engine Interface Unit
HMU
Hydromechanical Unit (ENG)
TLA
Thrust Lever Angle
FDU
Fire Detection Unit
Loop A & B
3 Sensors
SDCU
Smoke Detection Control Unit
TCAS (ACAS)
Traffic Alert and Collision Avoidance System
CPA (TCAS)
Closest Point of Approach
BMC
Bleed Air Monitoring Computers
IP (Bleed Air)
Bleed air taken from intermediate stage of compressor
HP (Bleed air)
Bleed air taken from high pressure stage of compressor
BSCU
Brake and Steering Control Unit
Two channels (active/standby)
FQI (fuel)
Fuel quantity indication computer
AEVC (Vent)
Avionics Equipment Ventilation Controller
CPC (Pressure)
Cabin Pressure Controller
ISIS
Integrated Standby Instrument System
CPDLC
Controller Pilot Direct Link Communications
CPDLC is a two-way data-link system by which controllers can transmit non urgent 'strategic messages to an aircraft as an alternative to voice communications
CFP
Computerized Flight Plan
ETP
Equal Time Point
An Equal Time Point is a point on the ETOPS route segment which is located at the same flying time (considering wind and temperature conditions) from the two associated suitable en-route Alternates
FLS
FMS Landing System
CFO
Company FMS Overlay
Last changed2 years ago
