ACRONYMS Flashcards

1
Q

HYDRAULIC PTU Pump FAULT light

A

O-Overheated Reservoir
L-Low Reservoir Quantity
L-Low Reservoir Air Pressure

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2
Q

HYDRAULIC ENGINE Pump FAULT Light

A

P-Pump Low Pressure
O-Overheated Reservoir
L-Low Reservoir Quantity
L-Low Reservoir Air Pressure

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3
Q

HYDRAULIC Electric Pump FAULT light

A
P-Pump low pressure
O-Overheated Reservoir
L-Low Reservoir Quantity
L-Low Reservoir Air Pressure
O-Over heated Pump
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4
Q

Electrical Source Priority

A
G-Generator (Engine)
E-External power
A-APU
R-RAT
B-Batteries
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5
Q

Continuous Ignition Auto Operate

A
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

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6
Q

PACK FAULT Light

A

P- PACK Outlet overheat
C- Compressor outlet overheat
P- Position Disagree (Switch/Valve

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7
Q

ENG BLEED Auto Close (or FAULT Light)

A
A- APU BLEED ON (FAULT if no Bleed Auto close)
S- Start Valve Open (“ “)
O- Overpressure (“ “)
L- Leak (“ “)
O- Overtemp (“ “)
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8
Q

DITCHING pb Commands closed

A
O- Outflow Valve
C- Cargo Isolation Valves
R- Ram Air Inlet
A- Avionics Ventilation Inlet and Extract Valves
P- Pack Flow a Control Valves
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9
Q

Ventilation FAULT Lights (BLOWER & EXTRACT)

A

Blower and Extract:

S- Smoke
L- Low pressure (To/From Fan)
C-Computer power supply fail

Blower only:

D-Duct Overheat

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10
Q

IR Computer Information (AHRS Data)

A
F-Flight Path Vector
A-Attitude
A-Acceleration
T-Track
H-Heading
A-Aircraft position
G-Groundspeed
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11
Q

ADR Computer Information(Pitot Static Data)

A
B-Barometric altitude
O-Overspeed Warning
A-Angle of Attack
T-Temperature 
S-Speed/Mach
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12
Q

ELAC (Elevator and Aileron Computer)

A

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

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13
Q

SEC (Spoiler and Elevator Computer)

A

N-Normal Roll
A- Alternate Pitch
D- Direct Pitch and Roll
A- Abnormal attitude

(Sec)

S- Spoiler/Speed Brakes

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14
Q

FAC (Flight Augmentation Computer)

A

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

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15
Q

Normal Law Pitch Characteristic and Protection (Alternate*)

Note: * = normal and alternate

A
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
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16
Q

Normal Law Roll Characteristics and Protections

A
Characteristic:
P- Pitch Trim (Automatic)
B- Bank Angle Hold
R- Roll Rate
S- Spiral Stability

Protections:

67-Bank Angle Protection

17
Q

Normal Law Yaw Characteristics

A

T- Turn Coordination (Normal)
Y- Yaw Damping (Normal and Alternate)
R- Rudder Trim (Normal, Alternate, and Direct)
M- Manual Rudder (Normal, Alternate, and Direct
R- Rudder Limiting (Normal, Alternate, and Direct)

18
Q

Spoiler Inhibited

A
S- SEC 1 and 3 Failure
A- Alpha Prot or Floor activated
F- Flaps CONF FULL (or CONF 3 in A321)
E- Elevator L or R Failed
T- Thrust Above MCT
19
Q

Wing Tip Brakes (F.LOCK S.LOCK)

A

R- Runaway
O- Overspeed
A- Asymmetry
M- Movement Uncommanded

20
Q

Low Energy Warning Inhibited

A
F- Flaps 1 or 0
A- Alpha Floor
T- TOGA Selected
A- Attitude>2000RA, <100RA
N-Normal Law not Active
G-GPWS
R- RA Failure
21
Q

Switches Requiring Confirmation BEFORE Movement

A

I- IRS
B- Breakers
E- Engine Master Switches
G- Guarded Switches (Fire pbs, IDGs, etc…)