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Frontier Limitations > OVER HEAD PANEL > Flashcards

OVER HEAD PANEL Flashcards

(64 cards)

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1
Q

PTU (DARK)

A

Operates when GREEN & YELLOW pressure differs >500 psi

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2
Q

RAT MAN ON

A

Extends automatically when AC Bus 1 & 2 are lost

Do not need power to manually deploy

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3
Q

CAB FANS (OFF)

A

Stops the 2 cabin recirculation fans

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4
Q

DITCHING

A

5…
Closes the (1) outflow valve, (2) emergency ram air inlet, (3) avionics ventilation inlet, (4) extract valves, (5) pack flow control valve
…
Closes all valves below the water line

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5
Q

COMMAND (EVAC)

A

Activates the evacuation tone in the cabin and flashes the EVAC lights at the FWD and AFT attendant panels

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6
Q

CAPT + PURS/CAPT

A
  1. Evacuation alert may be activated from either the flight deck or the cabin
  2. Evacuation alert may be only activated from the flight deck
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7
Q

EMER GEN TEST

A

When pressed and held, the emergency generator is tested

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8
Q

GEN 1 LINE (SMOKE)

A

Smoke detected in avionics compartment and sheds 75% of its load and energizes one pump in each wing

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9
Q

RAT & EMER GEN

A

Loss of power to AC BUS 1 & 2 AND the emergency generator is not supplying power

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10
Q

MAN ON AUTO

A

AC BUS 1 & 2 are down AND aircraft speed is greater than 100 knots

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11
Q

AMBER

A

One or more IR(s) is supplied by aircraft battery

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12
Q

OFF

A

The respective IR is disconnected

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13
Q

FAULT (flashing)

A

Attitude and heading may be recovered using ATT mode

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14
Q
A

FAT HAAG

Flight vector
Aircraft position
Track
Heading
Attitude
Acceleration
Ground Speed

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15
Q
A

FAT HAAG

Flight vector
Aircraft position
Track
Heading
Attitude
Acceleration
Ground Speed

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16
Q
A

BOATS

Barometric altitude
Over speed
AoA
Temperature
Speed/Mach

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17
Q

FAULT

A

Fault is detected in the associated air data reference computer

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18
Q

FAULT

A

Fault is detected OR during the ELAC power up test

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19
Q
A

Elevator and Aileron Computer

PAR AAA
Pitch
Abnormal Attitudes
Roll
Autopilot acquisition
Aileron drop
Activates protections

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20
Q
A

Speed and Elevator Control

PAR SS
Pitch
Abnormal Attitudes
Roll
Speed brakes
Spoilers

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21
Q
A

Flight Augmentation Computer

BeSWiFt RATTY
Beta target
Speed
Wind shear reactive (1300 AGL)
~tail~
Rudder limiting
Alternate law yaw
Trim for THS
Turn coordination
Yaw dampening

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22
Q
A

When pressed and held, the emergency generator is tested

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23
Q

SMOKE

A

Smoke is detected in the avionics ventilation system

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24
Q

FAULT

A

Loss of power to AC Bus 1 and 2 if the emergency generator is not supplying power

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25
AC Bus 1 and 2 are not electrically supplied and Aircraft speed if greater than 100 knots
26
AUTO
Oxygen mask doors open automatically when cabin altitude exceeds 14,000 feet
27
OFF
Oxygen supply valves are closed
28
FIRE
2 - Silence CRC and arm squib 1 - Hydraulic pump valve closes 2 - Fuel valve closes and deenergizes FADEC 1 - IDG offline 2 - END bleed closes and pack valves closes
29
SQUIB
Associated halon bottles are armed
30
DISCH
Halon bottle has lost pressure
31
ENG TEST
CRC + Master Warning light ECAM ENG Fire pb light SQUIB light DISCH light FIRE light by ignition
32
FIRE
2 - Silences CRC and arms squib NONE 2 - Closes APU fuel valve and turns off APU pump 1 - Deactivates APU generator 2 - Closes APU bleed valve and closes cross bleed valve
33
DISCH
Halon bottle has lost pressure
34
TEST
CRC and Master warning light ECAM APU Fire pb light* SQUIB light* DISCH light* (*if only DC power)
35
BLUE SYSTEMS (pumps)
2 pumps
36
GREEN SYSTEM (pump)
1 pump
37
YELLOW SYSTEM (pumps)
3 pumps
38
Extends automatically when AC Buses 1 and 2 are lost
39
FAULT
Reservoir low level, low air pressure, overheat Pump low pressure
40
Reservior low level, overheat, low air pressure Pump low pressure, overheat
41
FAULT
GREEN or YELLOW Reservoir overheat, low air pressure, low level
42
FAULT
Low output pressure
43
FAULT
Wing tanks < 11,000lbs and center tanks > 500lbs
44
FAULT
Any generator load > 100%
45
FAULT
Battery charger current is out of limits
46
HOTLOP High Oil Temp Low Oil Pressure
47
FAULT
GCU trip Line contactor open
48
FAULT
GCU trip Line contactor open Inhibited at low speed
49
FAULT
AC ESS Bus not powered
50
FAULT
OD Overheat compressor outlet or pack outlet Disagree of valve position
51
FAULT
LOOSA Leak Overheat Over pressure Start in process & valve open APU bleed on & valve open
52
FAULT
Leak has been detected
53
FAULT
Overheat detected and closes: Hot air valve Trim air valve
54
ANTI ICE WING FAULT
Low pressure Uncommanded position Loss of electrical: valves closes
55
ANTI ICE ENG FAULT
Uncommanded position Loss electrical: valve opens
56
ON
EFFFE ECB power and self-test Flap opens Fuel valves opens (LP) Fuel pump on ECAM
57
FAULT
Auto shutdown for many reason Fire will only cause auto shutdown on the ground
58
UP
Opens the outflow valve to increase cabin altitude
59
DN
Closes outflow valve and decreases cabin altitude
60
FAULT
Fault is detected in BOTH automatic systems
61
ON
Closes the (1) outflow valve, (2) emergency ram air inlet, (3) avionics ventilation inlet, (4) extract valves, (5) pack control valves
62
FAULT
SOAC Smoke Overheat Air low pressure (horn on the ground + no engines running) Computer fault
63
FAULT
SAC Smoke Air low pressure (horn on the ground + no engines running) Computer fault
64
PTU Inhibit
1. Parking brake 2. Cargo door 3. Engines are split 4. By pin installed

Frontier Limitations (6 decks)

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