Super Card Acronyms Flashcards
FAC (Flight Augmentation Computers) Functions
Y - Yaw Control
A - Airspeed Protection Computations (Alpha Prot/Hi-Lo)
W - Windshear Protection
L - Low Energy Warning
(AOM 1 22.40.1)
SEC (Spoiler Elevator Computer) Functions
S - Speed Brakes / Ground Spoilers A - Alternate Pitch D - Direct Pitch D - Direct Roll A - Abnormal Attitude N - Normal Roll Via Spoilers
ELAC (Elevator Aileron Computer) Functions
Fault Light-Power Up 8 sec. test
N—Normal Elevator, Aileron, Pitch & Roll A—Alternate Pitch D—Direct Pitch & Roll A—Abnormal Attitude A—Aileron Droop A—Autopilot Orders
Alpha Prot
A—⍺ is commanded instead of Load Factor
S—Speed Brake is Retracted
A—Autopilot is disengaged
P—Pitch Trim is inhibited
ADR Computers Provide (think pitot static)
A—Airspeed B - Barometric Altitude A - Airspeed M - Mach A - AOA T - Temperature O - Overspeed Protection
A—Altitude A—AOA T—Temp O—Overspeed M—Mach
IR Computers Provide (Think GPS)
G—Ground Speed A—Aircraft Position A—Attitude F—FPV H—Heading A—Acceleration T—Track
Normal Law Protections
B - Bank Angle Protection S - Speed Protection L - Load Factor Protection A - Angle of Attack Protection (⍺Prot) P—Pitch Angle Protection
Spoilers Inhibited When
S—SEC 1 and SEC 3 Failure A—Alpha Prot. or Alpha Floor F—Flaps in Config Full E—Elevator Failure (1) T—TOGA Thrust
Hydraulic PTU Pump Fault Light
O—Overheat Reservoir
L—Low Reservoir Quantity
L—Low Reservoir Air Pressure
Hydraulic Engine Pump Fault Light
P—Pump Low Pressure
O—Overheat Reservoir
L—Low Reservoir Quantity
L—Low Reservoir Air Pressure
Hydraulic Electric Pump Fault Light
P—Pump Low Pressure O—Overheat Reservoir L—Low Reservoir Quantity L—Low Reservoir Air Pressure O—Overheated Pump
Pack Fault Light
P—Pack Outlet Overheat
C—Compressor Outlet Overheat
S—Switch Pos. Disagree w/ Pack Flow Valve
Engine Bleed Valve Closes
A—APU Bleed On S—Starter Valve Open (Engine) O—Overpressure L—Leak (Bleed) O—Overheat
IDG Fault Light
HOT—High Oil Temp
LOP—Low Oil Pressure
Continuous Ignition Automatic When
M—Master is Cycled E—EIU Data Failed E—Engine Flameout or Surge • E—Eng. Anti-Ice On A—Approach Idle Selected T—Take Off Thrust Selected
Low Energy Warning Inhibited When
F—Flaps 1 or 0 A—Alpha Floor T—TOGA R—RA Failure A—Altitude above 2000 RA or below 100 RA G—GPWS Alert N—Normal Law Not Active
Electrical Priority
G—Generator E—External Power A—APU R—RAT B—Batteries
Wing Tip Brakes Engage (4 red collared breakers)
R—Runaway
O—Overspeed
A—Asymmetry
M—Movement Un-commanded
Ditching Push Button Closes
C—Cargo Isolation Valve R—Ram Air Inlet A—Avionics Inlet and Extract Valve P—Pack Flow Control Valves O—Out Flow Valve
Engine Starter Master Fault Light
M—Malfunction of Thrust Lever
A—Auto Start Abort
D—Disagree Between HP Fuel Valve
ECAMS Not Inhibited During T/O or Landing
F—Fire E—Engine Failure L—Low Oil Pressure E—Elevator Fault A—Auto Pilot Off C—Config Warning F—FWC Fault
