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Frontier Limitations > OVER HEAD PANEL > Flashcards

OVER HEAD PANEL Flashcards

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
Q
A

AC Bus 1 and 2 are not electrically supplied and
Aircraft speed if greater than 100 knots

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26
Q

AUTO

A

Oxygen mask doors open automatically when cabin altitude exceeds 14,000 feet

27
Q

OFF

A

Oxygen supply valves are closed

28
Q

FIRE

A

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
Q

SQUIB

A

Associated halon bottles are armed

30
Q

DISCH

A

Halon bottle has lost pressure

31
Q

ENG TEST

A

CRC + Master Warning light
ECAM
ENG Fire pb light
SQUIB light
DISCH light
FIRE light by ignition

32
Q

FIRE

A

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
Q

DISCH

A

Halon bottle has lost pressure

34
Q

TEST

A

CRC and Master warning light
ECAM
APU Fire pb light*
SQUIB light*
DISCH light*

(*if only DC power)

35
Q

BLUE SYSTEMS (pumps)

A

2 pumps

36
Q

GREEN SYSTEM (pump)

A

1 pump

37
Q

YELLOW SYSTEM (pumps)

A

3 pumps

38
Q
A

Extends automatically when AC Buses 1 and 2 are lost

39
Q

FAULT

A

Reservoir low level, low air pressure, overheat
Pump low pressure

40
Q
A

Reservior low level, overheat, low air pressure
Pump low pressure, overheat

41
Q

FAULT

A

GREEN or YELLOW
Reservoir overheat, low air pressure, low level

42
Q

FAULT

A

Low output pressure

43
Q

FAULT

A

Wing tanks < 11,000lbs and center tanks > 500lbs

44
Q

FAULT

A

Any generator load > 100%

45
Q

FAULT

A

Battery charger current is out of limits

46
Q
A

HOTLOP

High
Oil
Temp
Low
Oil
Pressure

47
Q

FAULT

A

GCU trip
Line contactor open

48
Q

FAULT

A

GCU trip
Line contactor open
Inhibited at low speed

49
Q

FAULT

A

AC ESS Bus not powered

50
Q

FAULT

A

OD

Overheat compressor outlet or pack outlet
Disagree of valve position

51
Q

FAULT

A

LOOSA
Leak
Overheat
Over pressure
Start in process & valve open
APU bleed on & valve open

52
Q

FAULT

A

Leak has been detected

53
Q

FAULT

A

Overheat detected and closes:
Hot air valve
Trim air valve

54
Q

ANTI ICE WING FAULT

A

Low pressure
Uncommanded position

Loss of electrical: valves closes

55
Q

ANTI ICE ENG FAULT

A

Uncommanded position

Loss electrical: valve opens

56
Q

ON

A

EFFFE

ECB power and self-test
Flap opens
Fuel valves opens (LP)
Fuel pump on
ECAM

57
Q

FAULT

A

Auto shutdown for many reason
Fire will only cause auto shutdown on the ground

58
Q

UP

A

Opens the outflow valve to increase cabin altitude

59
Q

DN

A

Closes outflow valve and decreases cabin altitude

60
Q

FAULT

A

Fault is detected in BOTH automatic systems

61
Q

ON

A

Closes the (1) outflow valve, (2) emergency ram air inlet, (3) avionics ventilation inlet, (4) extract valves, (5) pack control valves

62
Q

FAULT

A

SOAC

Smoke
Overheat
Air low pressure (horn on the ground + no engines running)
Computer fault

63
Q

FAULT

A

SAC

Smoke
Air low pressure (horn on the ground + no engines running)
Computer fault

64
Q

PTU Inhibit

A
  1. Parking brake
  2. Cargo door
  3. Engines are split
  4. By pin installed

Frontier Limitations (5 decks)

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