ACRONYMS Flashcards
HYDRAULIC PTU Pump FAULT light
O-Overheated Reservoir
L-Low Reservoir Quantity
L-Low Reservoir Air Pressure
HYDRAULIC ENGINE Pump FAULT Light
P-Pump Low Pressure
O-Overheated Reservoir
L-Low Reservoir Quantity
L-Low Reservoir Air Pressure
HYDRAULIC Electric Pump FAULT light
P-Pump low pressure O-Overheated Reservoir L-Low Reservoir Quantity L-Low Reservoir Air Pressure O-Over heated Pump
Electrical Source Priority
G-Generator (Engine) E-External power A-APU R-RAT B-Batteries
Continuous Ignition Auto Operate
All A320 Aircraft: E-Engine flameout Detection F-Failure of EIU I-Inflight sub idle or surge S-Switch (ENG Master) Cycled ON/OFF/ON
CEO A320 Aircraft only:
M-MCT/FLEX or TOGA Selected
E-ENG A/I ON
A-Approach Idle
PACK FAULT Light
P- PACK Outlet overheat
C- Compressor outlet overheat
P- Position Disagree (Switch/Valve
ENG BLEED Auto Close (or FAULT Light)
A- APU BLEED ON (FAULT if no Bleed Auto close) S- Start Valve Open (“ “) O- Overpressure (“ “) L- Leak (“ “) O- Overtemp (“ “)
DITCHING pb Commands closed
O- Outflow Valve C- Cargo Isolation Valves R- Ram Air Inlet A- Avionics Ventilation Inlet and Extract Valves P- Pack Flow a Control Valves
Ventilation FAULT Lights (BLOWER & EXTRACT)
Blower and Extract:
S- Smoke
L- Low pressure (To/From Fan)
C-Computer power supply fail
Blower only:
D-Duct Overheat
IR Computer Information (AHRS Data)
F-Flight Path Vector A-Attitude A-Acceleration T-Track H-Heading A-Aircraft position G-Groundspeed
ADR Computer Information(Pitot Static Data)
B-Barometric altitude O-Overspeed Warning A-Angle of Attack T-Temperature S-Speed/Mach
ELAC (Elevator and Aileron Computer)
N-Normal pitch and roll
A-Alternate pitch
D-Direct Pitch and Roll
A-Abnormal Attitude
(eLac)
L- Load alleviation
A-Autopilot Commands
A- Aileron Droop
SEC (Spoiler and Elevator Computer)
N-Normal Roll
A- Alternate Pitch
D- Direct Pitch and Roll
A- Abnormal attitude
(Sec)
S- Spoiler/Speed Brakes
FAC (Flight Augmentation Computer)
Y- Yaw Control (Damping, Coordination, Trim, Travel)
A-Airspeed Computations (Speed (V/F/S/Green Dot), G’s)
W- Windshear Detection
L- Low Energy Warning
Normal Law Pitch Characteristic and Protection (Alternate*)
Note: * = normal and alternate
Characteristics: L-Load Factor Demand* A-Automatic Pitch Trim (Ground Mode) (Flight Mode*) (Flare Mode)
Protections:
M- Maneuver Protection P- Pitch Protection H- High Speed Protection (Stability*) A- Angle of attack Protection \+Alpha Max (Highest ELAC AoA) \+Alpha Floor (Autothrust TOGA) \+Alpha Prot - A- Autopilot Disconnect - S- Speed Brakes Inhibit - A- Angle of Attack Demand - P- Pitch Up Inhibit, Down Induced