Lights and Switches (OHP) Flashcards
ADIRS: ADR Data
(BOATS)
- Baro altitude
- Overspeed warnings
- AOA
- Temperatures
- Speed/Mach
ADIRS: Battery Power Endurance
ADIRU 1 - Until Battery 2 fails
ADIRU 2/3 - 5 mins
(#3 acts as #1 if ATT HDG CAPT 3 selected)
ADIRS: Can ADRs be turned off independent of the IRs?
Yes
ADIRS: Does turning the IR to OFF also turn off the ADR?
Yes
ADIRS: Fast Align
Each ADIRS OFF then NAV within 5 secs
ADIRS: Full Alignment Required
- First Flight of the Day
- Crew Change
- International or Alaska
- Class II
- GPS Unavailable & NAVAID’s poor
- GPS Unavailable and ETE > 3 hours
ADIRS: How would the Captain’s displays be affected with IR1 failed or OFF?
- 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
ADIRS: IR Data
(FAT HAAG)
- Flight path vector
- Aircraft position
- Track
- Heading
- Attitude
- Acceleration
- Ground Speed
ADIRS: Post-flight ADIRU accuracy check
- DATA -> Position Monitor
- Look for drift >5nm
ADIRS: [ADR]
FAULT:
Fault in Air Data
ADIRS: [IR]
(Split this card up)
[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
AIR COND: Describe how temperature is regulated.
- Packs produce requested temp
- Trim Air valves modulate to achieve zone temps
AIR COND: The pneumatic system is monitored and controlled by?
2 Bleed Monitoring Computers (BMC)
AIR COND: What causes the Pack Flow Control valve to automatically close?
- Engine start sequence
- ENG FIRE pb pressed
- Ditching pb
- Faults:
- Low pressure
- Pack overheat
AIR COND: What logic controls the X-Bleed valve when the X-BLEED switch is in AUTO?
- Matches the APU bleed valve
- X-Bleed also CLOSES for wing, pylon, or APU duct leak (except during engine start)
AIR COND: When does the Lav/Galley Extract Fan operate?
Continuously with electrical power available
AIR COND: When is Pack FLOW automatically HI?
- APU Bleed
- Single Pack
AIR COND: [APU BLEED]
FAULT:
* Bleed leak
* APU bleed valve closes
AIR COND: [ENG BLEED]
FAULT
(LOOSA)
- Leak
- Over pressure
- Over temp
- Starting engine with valve open
- APU bleed open with valve open
AIR COND: [HOT AIR]
FAULT:
* Overheat
* Valve closure
AIR COND: [PACK #]
- Overheat
- Valve/Switch Disagreement
ANTI ICE: 3 elements to record after de-ice/anti-ice
- Brand and Type of Fluid
- Percentage of fluid in mix
- Anti-ice start time
ANTI ICE: Can the flight crew takeoff if the holdover time expires for Heavy Snow conditions?
No.
* No holdover time exists for Heavy snow.
* Pre-takeoff contamination check must be perfermed 5 mins prior to TO
ANTI ICE: In what position do the anti-Ice valves fail if electrical power is lost?
- Wing valves CLOSED
- Engine valves OPEN
ANTI ICE: What happens if the WING ANTI ICE switch is activated on the ground?
Wing anti-icing valves open for a 30s test
ANTI ICE: What part of the wing is heated?
Outboard 3 slats
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.
ANTI ICE: When do the wing anti-ice valves auto close?
- On landing
- Bleed leak detected
- Loss of electrical power
ANTI ICE: When is undiluted Type IV required?
Heavy snow and Ice Pellets
ANTI ICE: When must ENG ANTI-ICE be ON?
- Ground and Flight Ops
- Icing conditions exist/expect ( < 10ºC )
- Except climb and cruise SAT < -40ºC
ANTI ICE: When should wing anti-ice be selected on?
In flight with airframe icing indicated
ANTI ICE: [ENG #]
FAULT: Switch/anti-ice valve disagreement
ANTI ICE: [WING]
FAULT:
* Switch/valve disagreement
* Low pressure
APU Master on Sequence
(EFFFE)
- ECB power and self-test
- Flap opens
- Fuel valve opens (LP)
- Fuel pump on
- ECAM
APU: With the green AVAIL lights ON for both APU and EXT PWR, which system is powering the aircraft?
APU
APU: [APU BLEED]
FAULT:
* APU bleed leak
APU: [MASTER SW]
FAULT
* ECB commanded an auto shutdown
BLEED: Pneumatic Powered Items
- Wing anti-ice
- Eng start
- Hydraulic pressurization
- Air conditioning
- Water pressure
CABIN PRESS:
[DITCHING]
- Avionics Inlet and Extract valves
- Ram air inlet
- Pack Flow Control valves
- Outflow valve (only if in AUTO mode)
CABIN PRESS: From what source does the pressurization system obtain landing elevation?
FMGC database
CABIN PRESS: [MODE SEL]
FAULT:
* Both automatic pressure controllers are faulty
CALLS: How do you call a mechanic stationed outside of the aircraft?
MECH pb
CALLS: How do you make a normal Flight Attendant call?
- [FWD] and [AFT] or [ALL] call button
- Listen and transmit on [CAB]
CARGO: How many cargo smoke detectors are there?
- 2 FWD Compartment
- 4 AFT Compartment
CARGO: How many fire extinguishers are provided for the cargo compartments?
- 1 bottle
- 2 bottles if ETOPS
CARGO: [FWD] or [AFT]
SMOKE:
* Both channels detect smoke
or
* One channel faulty and the other detects smoke
- Isolation Valve closes
- Extract Fan stops
CARGO: [HOT AIR]
FAULT
* Duct Overheat
ELEC:
How can an IDG be reset?
On the ground by maintenance
ELEC: Circuit Breaker Colors
- Green – Monitored by ECAM
- Black – Not monitored by ECAM
- Red – Wing tip brake C/B
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
ELEC: How is the BATTERY BUS normally powered?
DC BUS 1
ELEC: Min Battery Voltage
(and how to charge batteries)
- 25.5 V
[To charge:]
* EXT PWR - ON
* BATT pbs - ON
* Approx 20 mins
ELEC: Power Source Priority
(GEAR B)
- Generators
- EXT PWR
- APU Generator
- RAT
- Batteries
ELEC: What does the AC ESS FEED pushbutton white ALTN light indicate?
AC BUS 2 is powering the AC ESS BUS
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
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
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
ELEC: What powers the Emergency Generator?
Blue HYD pressure from the RAT
ELEC: When are BATTs being used?
- Sole source
- Charging
- APU start
ELEC: Will the batteries completely discharge with BAT switches in AUTO and EXT PWR removed?
No.
Battery cut-off logic prevents this.
ELEC: [COMMERCIAL]
(GETCCD)
- Galley
- Entertainment other than live tv
- Toilets and water
- Cargo lights
- Cabin lights
- Drain masts x2
ELEC: [GALY & CAB]
FAULT:
* GEN overload
AUTO:
* Sheds galley and IFE power with GEN loss
ELEC: [GEN #]
FAULT
- Gen line contactor is open
- Overload
- Over/Under voltage
- Short
ELEC: [IDG]
(HOTLOP)
FAULT:
* High Oil Temp
* Low Oil Pressure
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
EMER ELEC PWR: What buses are powered by the emergency generator?
Essentials
* AC ESS
* AC ESS SHED
* DC ESS
* DC ESS SHED
EMER ELEC PWR: When will the RAT auto extend?
- AC BUS 1 & 2 not powered
- Airspeed > 100 kts
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
EMER ELEC PWR: [RAT & EMER GEN]
FAULT:
* AC Bus 1+2 power loss
* EMER GEN not supplying power
Emergency Power items available after landing
(MAV)
- Move outflow valve
- APU Fire protection
- VHF 1
EVAC: How would the flight crew command an evacuation?
- PA: “This is the Captain, EVACUATE, EVACUATE, EVACUATE!”
- Press EVAC COMMAND pb
EXT LT: Are the NAV 1/2 positions connected to a single bulb?
No.
Separate bulbs.
EXT LT: When do the strobes flash in AUTO?
Weight off of the main gear.
FIRE: Does the APU have any automatic fire protection?
Only when a fire is detected on the ground:
* Auto shut down
* Fire extinguisher discharge
FIRE: How many fire extinguishers are provided for each engine?
APU?
2 per engine
1 per APU
FIRE: What happens if both fire loops fail?
If both loops fail within 5 seconds, a FIRE warning will be issued.
FIRE: Where are the engine fire loops installed?
- Pylon nacelle
- Engine core
- Fan section
FIRE: [APU FIRE TEST] pb
- CRC
- MASTER WARN lights
- APU FIRE light
- SQUIB light
- APU FIRE ECAM
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
FIRE: [ENG FIRE TEST] pb
- CRC
- MASTER WARN lights
- ENG FIRE light
- SQUIB lights
- ENG FIRE ECAM
- ENG pedastal FIRE light
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
FLT CTL: ELAC Duties
(PAR AAA)
- Pitch
- Abnormal Attitudes
- Roll
- Aileron Droop
- A/P Acquisition
- Activates Protections
FLT CTL: FAC Duties?
(Be SWiFT RATTY)
- Beta target
- “Speed, speed, speed!”
- Windshear
- Flight Envelope Protections
-
Tail:
- Rudder limiting
- Alternate Law yaw
- Turn coordination
- Trim
- Yaw damping
FLT CTL: How are the flight control surfaces operated?
All Surfaces:
* Electrically controlled
* Hydaulically actuated
FLT CTL: If both FACs fail, is max rudder deflection available?
Yes.
After slat extension.
FLT CTL: SEC Duties
(PAR SS)
- Pitch
- Abnormal Attitudes
- Roll
- Speed brakes
- Spoilers
FLT CTL: [ELAC]
FAULT:
* Self test during power-up
FLT CTL: [SEC]
FAULT
* SEC Fault detected
[pb]
* System off/on
FUEL: How is the IDG cooled?
Fuel, which is then pumped back to the same-side outer tank.
FUEL: How many fuel pumps are installed?
- 2 in each wing tank
- 2 in center tank
- 1 for APU
FUEL: Normal in-flight fuel management scheme?
Center tank first, then wing tanks.
FUEL: When does the APU fuel pump run?
- CTR TKs OFF
- Battery power only
FUEL: Why are the outer wing tanks drained last?
Wing structural stress relief
FUEL: [MODE SEL]
FAULT:
* Failure of AUTO mode
* Center tank > 550# and a main tank < 11,000#
FUEL: [PUMP]
FAULT
* Low fuel pressure
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
HYD: Can the aircraft be flown with a loss of all hydraulic systems?
No.
At least one required.
HYD: Does the PTU transfer hydraulic fluid?
No.
HYD: How many hydraulic pumps are in the BLUE system?
- 1 Electric
- 1 RAT
HYD: How many hydraulic pumps are in the GREEN system?
- 1Engine
- 1 PTU
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
HYD: Normal hydraulic system pressure?
3,000 psi
HYD: When does the BLUE ELEC PUMP operate?
- After the first engine is started
- In flight
- [BLUE PUMP OVRD] pb w/no eng running
HYD: Can the Y ELEC PUMP run the PTU?
Yes
HYD: Does the RAT automatically deploy with the loss of BLUE hydraulic pressure?
No.
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
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
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
HYD: Unique BLUE system item
- Emergency generator
HYD: Unique GREEN system items
- Landing gear
- Normal brakes
- Engine 1 reverser
HYD: Unique YELLOW system items
- NW Steering
- Alternate brakes
- Parking brake
- Cargo doors
- Engine 2 reverser
HYD: When does the PTU activate with the pb in AUTO mode?
500 psi difference between Green and Yellow
HYD: [ENG # PUMP]
FAULT:
* Low Pump Pressure
* Low Air Pressure
* Low Quantity
* High Reservoir Temp
HYD: [PTU]
(LOL)
- Low quantity
- Overtemp
- Low air pressure
HYD: How do the hydraulic priority valves function?
If HYD pressure drops, high demand items are isolated. (Flaps, Slats, Gear, Emer Gen)
HYD: What is the purpose of the hand pump?
To provide Y HYD pressure for cargo door operation
HYD: [ELEC PUMP]
FAULT:
* Low Pump Pressure
* Low Air Pressure
* Low Quantity
* High Reservoir Temp
* High Pump Temp
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
INTERIOR LIGHTS: What flight deck lighting is available if normal electrical power is lost?
- Captain’s instrument panel
- Right dome light
- Standby compass
OXYGEN: How long does the PAX oxygen last?
Approximately 13 minutes
OXYGEN: What does the PASSENGER SYS ON light mean?
Signal sent to release oxygen mask doors
OXYGEN: What displays on the DOOR ECAM with the CREW SUPPLY pb ON
OXY data block changes from amber to green
OXYGEN: When do the passenger masks auto-deploy?
Cabin altitude > 14,000 ft
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
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
Switches to be Confirmed in Flight
Engine master switches
IR selector
Guarded controls
Thrust Levers*
Thrust levers during an Ecam or QRH procedure
Takeoff in moderate and heavy freezing rain is prohibited.
TRUE
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
VENTILATION: Is the skin heat exchanger ever bypassed in flight?
Yes.
During SMOKE configuration
VENTILATION: What is the purpose of the CABIN FANS?
To re-circulate cabin air to the mixing chamber and then back to the cabin
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
VENTILATION:
When is air conditioning introduced into the avionics compartment?
- Abnormal operation
- SMOKE configuration
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
VENTILATION: [BLOWER] and [EXTRACT]
FAULT
* SMOKE warning is activated
* Computer power supply failure
* Low pressure
* Duct overheat
[pb]:
* Override mode
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.
RVSM Required Equipment
(FFATPAD)
- FCU (1 channel)
- FWC
- ADRs (2)
- TXPDR (1)
- PFDs (2)
- A/P (1)
- DMCs (2)
