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Lights and Switches (OHP) Flashcards

(136 cards)

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1
Q

ADIRS: ADR Data
(BOATS)

A
  • Baro altitude
  • Overspeed warnings
  • AOA
  • Temperatures
  • Speed/Mach
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2
Q

ADIRS: Battery Power Endurance

A

ADIRU 1 - Until Battery 2 fails
ADIRU 2/3​ - 5​ mins

(#3 acts as #1 if ATT​ HDG​ CAPT​ 3 selected)

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3
Q

ADIRS: Can ADRs be turned off independent of the IRs?

A

Yes

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4
Q

ADIRS: Does turning the IR to OFF also turn off the ADR?

A

Yes

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5
Q

ADIRS: Fast Align

A

Each ADIRS OFF​ then NAV within​ 5 secs

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6
Q

ADIRS: Full Alignment Required

A
  • First Flight of the Day
  • Crew Change
  • International or Alaska
  • Class II
  • GPS Unavailable & NAVAID’s poor
  • GPS Unavailable and ETE > 3 hours
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7
Q

ADIRS: How would the Captain’s displays be affected with IR1 failed or OFF?

A
  • Att and Nav info lost
  • ATT and HDG flags on PFD
  • MAP NOT AVAIL on ND
  • Recover by switching to CAPT 3 ATT/HDG on EIS switching panel
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8
Q

ADIRS: IR Data
(FAT HAAG)

A
  • Flight path vector
  • Aircraft position
  • Track
  • Heading
  • Attitude
  • Acceleration
  • Ground Speed
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9
Q

ADIRS: Post-flight ADIRU accuracy check

A
  • DATA -> Position Monitor
  • Look for drift >5nm
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10
Q

ADIRS: [ADR]

A

FAULT:
Fault in Air Data

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11
Q

ADIRS: [IR]
(Split this card up)

A

[pb]
* Disconnects IR data output (new version)

ON BAT
* At least one IR is supplied by aircraft battery
* Illuminates briefly for full alignment

FAULT
* Steady: A fault affects the respective IR
* Flashing: ATT/HDG may be recovered in ATT mode (NAV lost)

ALIGN
* Steady: Normal during alignment
* Flashing: Poisiton error
* Also indications on E/WD

Position Errors
* No current position
* Incorrect position
* Aircraft movement

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12
Q

AIR COND: Describe how temperature is regulated.

A
  • Packs produce requested temp
  • Trim Air valves modulate to achieve zone temps
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13
Q

AIR COND: The pneumatic system is monitored and controlled by?

A

2 Bleed Monitoring Computers (BMC)

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14
Q

AIR COND: What causes the​ Pack Flow Control valve​ to automatically close?​

A
  • Engine start sequence
  • ENG FIRE pb pressed
  • Ditching pb
  • Faults:
    • Low pressure
    • Pack overheat​
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15
Q

AIR COND: What logic controls​ the​ X-Bleed valve​ when the​ X-BLEED switch is in​ AUTO?​

A
  • Matches the APU bleed valve​
  • X-Bleed​ also CLOSES for wing,​ pylon,​ or​ APU​ duct leak​ (except during​ engine​ start)
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16
Q

AIR COND: When does the Lav/Galley Extract Fan operate?

A

Continuously with electrical power available

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17
Q

AIR COND: When is Pack FLOW automatically HI?

A
  • APU Bleed
  • Single Pack
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18
Q

AIR COND: [APU BLEED]

A

FAULT:
* Bleed leak
* APU bleed valve closes

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19
Q

AIR COND: [ENG BLEED]

A

FAULT
(LOOSA)

  • Leak
  • Over pressure
  • Over temp
  • Starting engine with valve open
  • APU bleed open with valve open
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20
Q

AIR COND: [HOT AIR]

A

FAULT:
* Overheat
* Valve closure

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21
Q

AIR COND: [PACK #]

A
  • Overheat
  • Valve/Switch Disagreement
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22
Q

ANTI ICE: 3 elements to record after de-ice/anti-ice

A
  1. Brand and Type of Fluid
  2. Percentage of fluid in mix
  3. Anti-ice start time
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23
Q

ANTI ICE: Can the flight crew takeoff if the holdover time expires for Heavy Snow conditions?

A

No.
* No holdover time exists for Heavy snow.
* Pre-takeoff contamination check must be perfermed 5 mins prior to TO

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24
Q

ANTI ICE: In what position do the anti-Ice valves fail if electrical power is lost?

A
  • Wing valves CLOSED
  • Engine valves OPEN
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25
**ANTI ICE: What happens if the WING ANTI ICE switch is activated on the ground?**
Wing anti-icing valves open for a 30s test
26
**ANTI ICE: What part of the wing is heated?**
Outboard 3 slats
27
**ANTI ICE: What types/colors of anti-ice/de-ice fluid that Frontier F9 uses?** [update?]
Type 1 - De-ice Orange Type 2 - Anti-Ice Green Type 3 - F9 DOES NOT USE Type 4 - Anti-Ice Green.
28
**ANTI ICE: When do the wing anti-ice valves auto close?**
* On landing * Bleed leak detected * Loss of electrical power
29
**ANTI ICE: When is undiluted Type IV required?**
Heavy snow and Ice Pellets
30
**ANTI ICE: When must ENG ANTI-ICE be ON?**
* Ground and Flight Ops * Icing conditions exist/expect ( < 10ºC ) * Except climb and cruise SAT < -40ºC
31
**ANTI ICE: When should wing anti-ice be selected on?**
In flight with airframe icing indicated
32
**ANTI ICE: [ENG #]**
FAULT: Switch/anti-ice valve disagreement
33
**ANTI ICE: [WING]**
FAULT: * Switch/valve disagreement * Low pressure
34
**APU Master on Sequence** **(EFFFE)**
* ECB power and self-test * Flap opens * Fuel valve opens (LP) * Fuel pump on * ECAM
35
**APU: With the green AVAIL lights ON for both APU and EXT PWR, which system is powering the aircraft?**
APU
36
**APU: [APU BLEED]**
**FAULT:** * APU bleed leak
37
**APU: [MASTER SW]**
**FAULT** * ECB commanded an auto shutdown
38
**BLEED: Pneumatic Powered Items**
* Wing anti-ice * Eng start * Hydraulic pressurization * Air conditioning * Water pressure
39
**CABIN PRESS: [DITCHING]**
* Avionics Inlet and Extract valves * Ram air inlet * Pack Flow Control valves * Outflow valve (only if in AUTO mode)
40
**CABIN PRESS: From what source does the pressurization system obtain landing elevation?**
FMGC database
41
**CABIN PRESS: [MODE SEL]**
**FAULT:** * Both automatic pressure controllers are faulty
42
**CALLS: How do you call a mechanic stationed outside of the aircraft?**
MECH pb
43
**CALLS: How do you make a normal Flight Attendant call?**
* [FWD] and [AFT] or [ALL] call button * Listen and transmit on [CAB]
44
**CARGO: How many cargo smoke detectors are there?**
* 2 FWD Compartment * 4 AFT Compartment
45
**CARGO: How many fire extinguishers are provided for the cargo compartments?**
* 1 bottle * 2 bottles if ETOPS
46
**CARGO: [FWD] or [AFT]**
**SMOKE:** * Both channels detect smoke or * One channel faulty and the other detects smoke * Isolation Valve closes * Extract Fan stops
47
**CARGO: [HOT AIR]**
**FAULT** * Duct Overheat
48
**ELEC: How can an IDG be reset?**
On the ground by maintenance
49
**ELEC: Circuit Breaker Colors**
* Green – Monitored by ECAM * Black – Not monitored by ECAM * Red – Wing tip brake C/B
50
**ELEC: How is AC ESS​ FEED transferred​ from AC BUS 1 to AC BUS​ 2?**
* Manually: AC ESS​ FEED pb ALT * Automatically​: AC​ BUS​ 1 lost with pb normal
51
**ELEC: How is the BATTERY BUS normally powered?**
DC BUS 1
52
**ELEC: Min Battery Voltage (and how to charge batteries)**
* 25.5 V **[To charge:]** * EXT PWR - ON * BATT pbs - ON * Approx 20 mins
53
**ELEC: Power Source Priority** **(GEAR B)**
* Generators * EXT PWR * APU Generator * RAT * Batteries
54
**ELEC: What does​ the​ AC ESS​ FEED pushbutton white​ ALTN​ light indicate?​**
AC BUS​ 2 is powering the AC ESS​ BUS
55
**ELEC: What is​ the​ function of​ the​ AC ESS​ FEED​ pushbutton​ in the​ normal​ position?​**
Allows AC BUS​ 1​ to power the​ AC ESS​ BUS
56
**ELEC: What is​ the​ function of​ the​ BUS​ TIE in the​ AUTO position?​**
Allows the​ BUS​ TIE CONTACTORS​ to open and close​ automatically​ to maintain power to​ both AC ​BUS​ 1 &​ 2:​ ​ * Allows a single​ source​ to power the entire​ system ​ * Allows connection of​ the​ APU​ GEN​ or​ EXT​ PWR to the​ system ​ * Inhibits multiple​ sources​ to​ connect​ simultaneously
57
**ELEC: What is​ the​ purpose​ of the​ static inverter?​**
Ref: (FOM VOL. III-DSC-24-10-20)​ ​ To provide​ AC power to​ the​ AC ESS​ bus​ from the​ battery​ when​ the​ EMG GEN​ is not​ online when ​in the Emergency Electrical Configuration
58
**ELEC: What powers the Emergency Generator?**
Blue HYD pressure from the RAT
59
**ELEC: When are BATTs being used?**
* Sole source * Charging * APU start
60
**ELEC: Will the batteries completely discharge with BAT switches in AUTO and EXT PWR removed?**
No. Battery cut-off logic prevents this.
61
**ELEC: [COMMERCIAL]** **(GETCCD)**
* Galley * Entertainment other than live tv * Toilets and water * Cargo lights * Cabin lights * Drain masts x2
62
**ELEC: [GALY & CAB]**
**FAULT:** * GEN overload **AUTO:** * Sheds galley and IFE power with GEN loss
63
**ELEC: [GEN #]**
**FAULT** * Gen line contactor is open * Overload * Over/Under voltage * Short
64
**ELEC: [IDG]** **(HOTLOP)**
**FAULT:** * High Oil Temp * Low Oil Pressure
65
**EMER ELEC PWR: How long does it take the RAT to extend and provide power?**
**8 seconds** * RAT Extension - 3 s * B HYD PRES (EMER GEN) - 5 s
66
**EMER ELEC PWR: What buses are powered by the emergency generator?**
**Essentials** * AC ESS * AC ESS SHED * DC ESS * DC ESS SHED​
67
**EMER ELEC PWR: When will the RAT auto extend?**
* AC BUS 1 & 2 not powered * Airspeed > 100 kts
68
**EMER ELEC PWR: [GEN 1 LINE]**
**SMOKE:** * Smoke detected in avionics ventilation **[pb]:** * GEN 1 Line Contactor opens * OFF light illuminates * AC BUS 1 powered by GEN 2 * GEN 1 powers 1 fuel pump in each wing tank **Also:** * Extract and Blower fault lights * ECAM warning
69
**EMER ELEC PWR: [RAT & EMER GEN]**
**FAULT:** * AC Bus 1+2 power loss * EMER GEN not supplying power
70
**Emergency Power items available after landing** **(MAV)**
* Move outflow valve * APU Fire protection * VHF 1
71
**EVAC: How would the flight crew command an evacuation?**
* PA: “This is the Captain, EVACUATE, EVACUATE, EVACUATE!” * Press EVAC COMMAND pb
72
**EXT LT: Are the NAV 1/2 positions connected to a single bulb?**
No. Separate bulbs.
73
**EXT LT: When do the strobes flash in AUTO?**
Weight off of the main gear.
74
**FIRE: Does the APU have any automatic fire protection?**
Only when a fire is detected on the ground: * Auto shut down * Fire extinguisher discharge
75
**FIRE: How many fire extinguishers are provided for each engine?** **APU?**
2 per engine 1 per APU
76
**FIRE: What happens if both fire loops fail?**
If both loops fail within 5 seconds, a FIRE warning will be issued.
77
**FIRE: Where are the engine fire loops installed?**
* Pylon nacelle * Engine core * Fan section
78
**FIRE: [APU FIRE TEST] pb**
* CRC * MASTER WARN lights * APU FIRE light * SQUIB light * APU FIRE ECAM
79
**FIRE: [APU FIRE] pb**
* Silences the CRC * Arms the squib * Shuts down the APU (ECB) * Closes APU fuel valve * Shuts OFF the APU fuel pump * Deactivates the APU generator * Closes the APU bleed and X bleed valves
80
**FIRE: [ENG FIRE TEST] pb**
* CRC * MASTER WARN lights * ENG FIRE light * SQUIB lights * ENG FIRE ECAM * ENG pedastal FIRE light
81
**FIRE: [ENG FIRE] pb**
* Silences the CRC * Arms the squibs * Closes the hydraulic shutoff valve * Closes the fuel shutoff valve * Deactivates the IDG and FADEC * Closes the pack and engine bleed valves
82
**FLT CTL: ELAC Duties** **(PAR AAA)**
* **P**itch * **A**bnormal Attitudes * **R**oll * **A**ileron Droop * **A**/P Acquisition * **A**ctivates Protections
83
**FLT CTL: FAC Duties?** **(Be SWiFT RATTY)**
* **B**eta target * "**S**peed, speed, speed!” * **W**indshear * **F**light Envelope Protections * **T**ail: * **R**udder limiting * **A**lternate Law yaw * **T**urn coordination * **T**rim * **Y**aw damping
84
**FLT CTL: How are the flight control surfaces operated?**
**All Surfaces:** * Electrically controlled * Hydaulically actuated
85
**FLT CTL: If both FACs fail, is max rudder deflection available?**
Yes. After slat extension.
86
**FLT CTL: SEC Duties** **(PAR SS)**
* **P**itch * **A**bnormal Attitudes * **R**oll * **S**peed brakes * **S**poilers
87
**FLT CTL: [ELAC]**
**FAULT:** * Self test during power-up
88
**FLT CTL: [SEC]**
**FAULT** * SEC Fault detected **[pb]** * System off/on
89
**FUEL: How is the IDG cooled?**
Fuel, which is then pumped back to the same-side outer tank.
90
**FUEL: How many fuel pumps are installed?**
* 2 in each wing tank * 2 in center tank * 1 for APU
91
**FUEL: Normal in-flight fuel management scheme?**
Center tank first, then wing tanks.
92
**FUEL: When does the APU fuel pump run?**
* CTR TKs OFF * Battery power only
93
**FUEL: Why are the outer wing tanks drained last?**
Wing structural stress relief
94
**FUEL: [MODE SEL]**
**FAULT:** * Failure of AUTO mode * Center tank > 550# and a main tank < 11,000#
95
**FUEL: [PUMP]**
**FAULT** * Low fuel pressure
96
**GPWS: [SYS]**
**FAULT:** * Any failure of GPWS mode 1-5 * “Sink Rate” * “Terrain, Terrain” * “Don’t Sink” * “Too Low Flaps” * “Too Low Gear” * “Glideslope” **[pb]:** * Inhibits all EGPWS except TERR
97
**HYD: Can the aircraft be flown with a loss of all hydraulic systems?**
No. At least one required.
98
**HYD: Does the PTU transfer hydraulic fluid?**
No.
99
**HYD: How many hydraulic pumps are in the BLUE system?**
* 1 Electric * 1 RAT
100
**HYD: How many hydraulic pumps are in the GREEN system?**
* 1Engine * 1 PTU
101
**HYD: How many hydraulic pumps are in the YELLOW system?**
Ref: (FOM VOL. III-DSC-29-10-20)​ ​ * 1​ Engine ​ * 1​ Electric​ ​ * 1​ PTU ​ * 1 Hand​ pump
102
**HYD: Normal hydraulic system pressure?**
3,000 psi
103
**HYD: When does the BLUE ELEC PUMP operate?**
* After the first engine is started * In flight * [BLUE PUMP OVRD] pb w/no eng running
104
**HYD: Can the​ Y ELEC PUMP run​ the​ PTU?​**
Yes
105
**HYD: Does the​ RAT​ automatically​ deploy​ with the​ loss​ of​ BLUE hydraulic pressure?​**
No.
106
**HYD: If​ the​ ACCU PRESS​ indicator is​ low and​ an external​ walkaround​ is to be​ completed,​ what​ should you​ ​do?​**
Obtain ground​ clearance​ then turn​ ON​ the YELLOW​ ELEC PUMP to pressurize​ the​ accumulator
107
**HYD: If​ the​ ECAM actions​ lead​ you to​ turn OFF​ the​ PTU for a Reservoir Overheat, will​ the​ FAULT light go out?**​
No, not until temperature is restored
108
**HYD: If​ the​ FAULT light in the​ PTU pushbutton is​ ON,​ are​ there​ any​ other indications​ on the​ HYD Panel?​**
Yes​ –​ FAULT light illuminated in the​ respective​ ENG​ PUMP​ pushbutton
109
**HYD: Unique BLUE system item**
* Emergency generator
110
**HYD: Unique GREEN system items**
* Landing gear * Normal brakes * Engine 1 reverser
111
**HYD: Unique YELLOW system items**
* NW Steering * Alternate brakes * Parking brake * Cargo doors * Engine 2 reverser
112
**HYD: When does the PTU activate with the pb in AUTO mode?**
500 psi difference between Green and Yellow
113
**HYD: [ENG # PUMP]**
**FAULT:** * Low Pump Pressure * Low Air Pressure * Low Quantity * High Reservoir Temp
114
**HYD: [PTU]** **(LOL)**
* Low quantity * Overtemp * Low air pressure
115
**HYD: How do the hydraulic priority valves function?**
If HYD pressure drops, high demand items are isolated. (Flaps, Slats, Gear, Emer Gen)
116
**HYD: What is the purpose of the hand pump?**
To provide Y HYD pressure for cargo door operation
117
**HYD: [ELEC PUMP]**
**FAULT:** * Low Pump Pressure * Low Air Pressure * Low Quantity * High Reservoir Temp * High Pump Temp
118
**HYD: When is the PTU inhibited?**
* PTU pb * First engine start * PARK BRK set and only 1 ENG MASTER ON * NWS disc + PARK BRK released * Cargo door ops + 40 sec
119
**INTERIOR LIGHTS: What flight deck lighting is available if normal electrical power is lost?**
* Captain’s instrument panel * Right dome light * Standby compass
120
**OXYGEN: How long does the PAX oxygen last?**
Approximately 13 minutes
121
**OXYGEN: What does the PASSENGER SYS ON light mean?**
Signal sent to release oxygen mask doors
122
**OXYGEN: What displays on the DOOR ECAM with the CREW SUPPLY pb ON**
OXY data block changes from amber to green
123
**OXYGEN: When do the passenger masks auto-deploy?**
Cabin altitude > 14,000 ft
124
**PROBES: With the PROBE/WINDOW HEAT pb in AUTO, when are the probe and mast heaters activated?**
* LOW with at least 1 ENG running * (TAT not heated on ground) * NORMAL after takeoff
125
**RECORDER: When do the RCDR and DFDR operate?**
**Ground** * When elec power applied + 5 mins * When at least 1 engine is running **Flight** * Continuously until 5 mins after the last engine is shut down
126
**Switches to be Confirmed in Flight**
Engine master switches IR selector Guarded controls Thrust Levers* | Thrust levers during an Ecam or QRH procedure
127
**Takeoff in moderate and heavy freezing rain is prohibited.**
TRUE
128
**VENT: Normal Avionics Ventilation config with Extract and Blower pbs in AUTO**
**Ground** * OPEN configuration **Flight** * CLOSED configuration **INTERMEDIATE configuration** * High skin temp in flight * High skin temp after T/O CONFIG * High skin temp after T/L set for T/O
129
**VENTILATION: Is the skin heat exchanger ever bypassed in flight?**
Yes. During SMOKE configuration
130
**VENTILATION: What is the purpose of the CABIN FANS?**
To re-circulate cabin air to the mixing chamber and then back to the cabin
131
**VENTILATION: What is the status of the Blower and Extract fans with the Blower and Extract valves in OVRD?​**
* BLOWER fan OFF * EXTRACT fan ON
132
**VENTILATION: When is air conditioning introduced into the avionics compartment?**
* Abnormal operation​ ​ * SMOKE configuration
133
**VENTILATION: With both BLOWER and EXTRACT pushbuttons​ in OVRD (smoke​ configuration)​ what​ are​ the​ positions ​of​ the​ INLET​ and EXTRACT​ valves?​**
Ref: (FOM VOL. III-DSC-21-30-60)​ ​ * INLET​ valve​ CLOSED ​ * EXTRACT​ valve​ INTERMEDIATE
134
**VENTILATION: [BLOWER] and [EXTRACT]**
**FAULT** * SMOKE warning is activated * Computer power supply failure * Low pressure * Duct overheat **[pb]:** * Override mode
135
**When is the PTU inhibited?**
* Only 1 ENG master on, PRK BRK on * PRK BRK OFF, NW STRG DISC * 40 seconds after cargo door operation.
136
**RVSM Required Equipment** **(FFATPAD)**
* **F**CU (1 channel) * **F**WC * **A**DRs (2) * **T**XPDR (1) * **P**FDs (2) * **A**/P (1) * **D**MCs (2)

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