Recall the required pavement width for a 180 degree turn.

The theoretical minimum pavement width required is ___feet.

Recall the required pavement width for a 180 degree turn.

The theoretical minimum pavement width required is 75 feet.

Describe the minimum obstruction path during a turn.

The ___swings the largest arc, followed by the ___, then the ___.

Therefore, the ___determines the minimum obstruction clearance

path during a turn.

Describe the minimum obstruction path during a turn.

The wingtip swings the largest arc, followed by the tail, then the nose.

Therefore, the wingtip determines the minimum obstruction clearance

path during a turn.

Recall the location of Cabin Doors, Overwing Emergency Exits and Flight Deck emergency exits.

 There are ___(  __on each side of the cabin), identified as _________.

 There are 4 cabin doors (2 on each side of the cabin), identified as 1L, 1R, 2L, and 2R.

Recall the location of Cabin Doors, Overwing Emergency

Exits and Flight Deck emergency exits.

Cabin doors are each equipped with an ____________which allow for _________

from either the __________of the aircraft.

Recall the location of Cabin Doors, Overwing Emergency

Exits and Flight Deck emergency exits.

There are ____( __ on each side of the aircraft) which can

be opened from either __________.

There are 4 overwing exits (2 on each side of the aircraft) which can

be opened from either the interior or exterior of the aircraft.

Recall the location of Cabin Doors, Overwing Emergency

Exits and Flight Deck emergency exits.

Two (__) Flight deck ________can be used for emergency

egress, but ____be opened from the _____ of the aircraft.

Describe the ECAM DOOR/OXY page indications.

Cabin Entrance Doors:

o Green box – the door _____.

o Solid amber box with amber CABIN – door is ____.

Cabin Entrance Doors:

o Green box – the door is closed and locked.

o Solid amber box with amber CABIN – door is unlocked.

Describe the ECAM DOOR/OXY page indications.

Avionics Doors:

o Green box – door is _____.

o Solid amber box with amber ___ – door is _____.

Avionics Doors:

o Green box – door is closed and locked.

o Solid amber box with amber AVIONIC – door is unlocked.

Describe the ECAM DOOR/OXY page indications.

Overwing Exits:

o Green box – exit is ___and ___.

o Solid amber box with amber______– exit is ___or the ____________

has been ___.

Overwing Exits:

o Green box – exit is closed and locked.

o Solid amber box with amber EMER EXIT – exit is open or the cover of the exit

control handle has been removed.

Recall the ECAM DOOR/OXY page indications of emergency escape slides being armed.

The word ___  (_____) appears next to the respective ___ or _______.

NOTE: Only _________________________________.

The word SLIDE (white) appears next to the respective cabin door or overwing exit.

NOTE: Only one emergency escape slide is installed per wing.

Recall the emergency equipment stored on the flight deck.

• __ crew life vests (orange)

• __ halon fire extinguisher

• __ crash ax

• __ crew oxygen masks

• __ escape ropes

• __ Protective Breathing Equipment (PBE)

• 4 crew life vests (orange)

• 1 halon fire extinguisher

• 1 crash ax

• 4 crew oxygen masks

• 2 escape ropes

• 1 Protective Breathing Equipment (PBE)

Recall the emergency equipment stored on the flight deck.

• 4 ____

• 1 ____

• 1 ____

• 4 ____

• 2 ____

• 1 ____

Recall the emergency equipment stored on the flight deck.

• 4 crew life vests (orange)

• 1 halon fire extinguisher

• 1 crash ax

• 4 crew oxygen masks

• 2 escape ropes

• 1 Protective Breathing Equipment (PBE)

Explain the controls and indicators on the overhead

OXYGEN panel.

 _____________:

o Illuminates (SYS ON) when either an automatic or manual electrical signal has been sent to deploy the passenger masks.

o An automatic signal is generated whenever cabin altitude exceeds 14,000ft.

 PASSENGER SYS ON light:

o Illuminates (SYS ON) when either an automatic or manual electrical signal has been sent to deploy the passenger masks.

o An automatic signal is generated whenever cabin altitude exceeds 14,000ft.

Recall the oxygen system indications on the ECAM DOOR/OXY page.

o OXY (amber) – indicates _________________.

o OXY (amber) – indicates insufficient bottle pressure.

Recall the oxygen system indications on the ECAM DOOR/OXY page.

o REGUL LO PR (amber) – indicates ______________________.

o REGUL LO PR (amber) – indicates insufficient oxygen pressure is being delivered

to the crew oxygen masks.

o OXY and REGUL LO PR (amber) appearing together – indicates____________.

o OXY and REGUL LO PR (amber) appearing together – indicates oxygen system has been turned off via the Crew Supply pb.

Recall the flight deck’s emergency lights when in the

emergency electrical configuration or on battery power

alone.

Which lights?

NOTE: In order to provide illumination, these lights must be selected ______.

They will _______with _________________.

 CA's flood lights

 FO's dome light

 STBY COMPASS light

NOTE: In order to provide illumination, these lights must be selected on by the

pilot. They will NOT come on automatically with the loss of normal power.

Recall the results of the NO SMOKING switch placed in the AUTO position:

o NO SMOKING signs illuminate

o Cabin EXIT signs:

 Illuminates when the landing gear is extended.

 Extinguishes when the landing gear is retracted.

Recall the function of each position of the X BLEED selector.

o SHUT:

 Commands ____________________________________.

o SHUT:

 Commands crossbleed valve closed, overriding auto logic.

Recall the function of each position of the X BLEED selector.

o AUTO:

 Auto logic controls ___ nd ___ of the ___ ___ .

•___ ___ commanded ___ when the ___ ___ ___ is ___

•___ ___ commanded ___ when ___ ___ ___ is ___

•___ ___ commanded ___ when a ___ ___ ___ ___

o AUTO:

 Auto logic controls opening and closing of the crossbleed valve

•crossbleed valve commanded open when the APU bleed valve is open

•crossbleed valve commanded closed when APU bleed valve is closed

•crossbleed valve commanded closed when a bleed leak is detected

Recall the function of each position of the X BLEED selector.

o OPEN:

 Commands the _____ _____ _____ , overriding the _____ _____ .

o OPEN:

 Commands the crossbleed valve open, overriding the auto logic.

With no ___ ___ ___ being provided (i.e. ___ or ___ ___ ___ ), a ___ ___ is displayed on the left side of the ___ ___ page. By default the air source must be an ___ ___ ___ ___ ___ .

Recall the indications of external high pressure air being applied to the pneumatic system.

With no internal air source being provided (i.e. APU or engine bleed air), a PSI value is displayed on the left side of the ECAM BLEED page. By default the air source must be an external high pressure air cart.

Engine ___ ____ are depicted next to the respective ___ ____

on lower portion on the page.

Recall the indications of the Engine Bleed Valves and HP

(High Pressure) valves on the ECAM BLEED page.

Engine bleed valves are depicted next to the respective engine’s

number (1 and 2) on lower portion on the page.

__ ______are depicted on the ___ ____of the page next to the ___ HP designator.

Recall the indications of the Engine Bleed Valves and HP

(High Pressure) valves on the ECAM BLEED page.

HP valves are depicted on the lower portion of the page next to

the white HP designator.

NOTE: __ (____ ____) check valves are not specifically depicted

but are represented by a ___ __designator.

Recall the indications of the Engine Bleed Valves and HP

(High Pressure) valves on the ECAM BLEED page.

NOTE: IP (Intermediate Pressure) check valves are not specifically depicted

but are represented by a white IP designator.

Recall the indications when APU bleed air is in use.

___ ___is presented in ___(color) on the ___ section of the E/WD.

Recall the indications when APU bleed air is in use.

APU BLEED is presented in green on the memo section of the E/WD.

Recall the areas of the aircraft where a bleed air leak can be detected.

o Wings: ______

o Engine pylons: ______

o Aft fuselage: ______

Recall the areas of the aircraft where a bleed air leak can be detected.

o Wings: each wing’s bleed air duct

o Engine pylons: area from the engine to the respective wing bleed duct

o Aft fuselage: area surrounding the APU bleed air duct

o Primary channel failure:

 ______________

    ______________

o Secondary channel failure:

______________

o Primary and Secondary channel failure:

______________

______________

Recall the indications of a Pack Regulator failure.

o Primary channel failure:

-ECAM failure message appears on the E/WD memo section.

-All pack information presented on the BLEED page is still present.

o Secondary channel failure:

-All temperature indications for the corresponding pack will be replaced with amber Xs.

o Primary and Secondary channel failure:

-All temperature indications for the corresponding pack will be

replaced with amber Xs.

-ECAM failure message appears in the E/WD memo section.

Recall which cargo compartment is heated and ventilated.

- Only the _____is capable of having its temperature controlled, using the controls located on the ___ ____ ____ ____.

- Temperature of the ___ ____ ____ can be monitored by referencing the ___ ____or ____pages.

Recall which cargo compartment is heated and ventilated.

Only the aft cargo compartment is capable of having its temperature controlled, using the controls located on the overhead CARGO HEAT panel.

Temperature of the aft cargo compartment can be monitored by referencing the ECAM COND or CRUISE pages.

 There are ___ _______ __________installed.

 Designated as ___ and _____,  the current active system can be viewed on the

ECAM ___ _____page.

Recall how many pressurization controllers are installed on

the aircraft and where the active system is displayed on

ECAM.

 There are two pressurization controllers installed.

 Designated as SYS 1 and SYS 2, the current active system can be viewed on the ECAM CAB PRESS page.

Describe how the active and standby pressurization controllers switch roles.

o Automatically:

 ______________.

 ______________.

o Manually:

  ______________.

Describe how the active and standby pressurization controllers switch roles.

o Automatically:

 Shortly after landing.

 In the event the active controller fails.

o Manually:

 Placing the MODE SEL pb to MAN for 10 seconds, and then returning it back to the AUTO (lights out) mode.

Describe the function of the LDG ELEV selector.

o In AUTO (detent) position:

 _________________

o Outside of AUTO (turning clockwise):

 Landing field elevation is set manually.

 _________________

NOTE: Selector is calibrated in _____, not _____of feet.

Describe the function of the LDG ELEV selector.

o In AUTO (detent) position:

 FMGCs provide the pressurization system with the landing field elevation.

o Outside of AUTO (turning clockwise):

 Landing field elevation is set manually.

 Used when both FMCGs have failed or when landing airport is not in the FMS data base.

NOTE: Selector is calibrated in thousands, not hundreds of feet.

o MODE SEL pb:

 selecting ___(light on) enables the use of the

___ ___ ____toggle switch to manually control the ____valve.

 Deactivates the ____ ___________mode.

o MAN V/S CTL toggle switch:

 __ commands the _____valve ____, reducing cabin pressure – increasing cabin’s

altitude- "___ ___ ___".

 __ commands the ____ valve ____, increasing cabin pressure – decreasing

cabin’s altitude- "___ ___ ___".

NOTE: Pressurization system performance can be monitored on either ECAM

 ___ ___ or _____pages.

o MODE SEL pb:

 selecting MAN (light on) enables the use of the

MAN V/S CTL toggle switch to manually control the outflow valve.

 Deactivates the AUTO pressurization mode.

o MAN V/S CTL toggle switch:

 UP commands the outflow valve open, reducing cabin pressure – increasing cabin’s altitude- "taking the cabin up".

 DN commands the outflow valve close, increasing cabin pressure – decreasing cabin’s altitude- "taking the cabin down".

NOTE: Pressurization system performance can be monitored on either ECAM CAB PRESS or Cruise pages.

Recall, in the event the flight must return to the departure

airport immediately after takeoff, what pressurization

system action must be taken by the pilot.

_______________________. The pressurization system will

___ return the ____ to ____ the ___ _____

field elevation. This is referred to as the system’s ____ _______.

Recall, in the event the flight must return to the departure

airport immediately after takeoff, what pressurization

system action must be taken by the pilot.

No pilot action is required. The pressurization system will

automatically return the cabin to match the departure airport’s

field elevation. This is referred to as the system’s Abort Mode.

Describe the function of the DITCHING pb on.

Placing the DITCHING pb to ON commands the following openings to close:

______________

______________

______________ 

______________

______________

Describe the function of the DITCHING pb on.

Placing the DITCHING pb to ON commands the following openings to close:

 Outflow valve (if the MODE SEL pb is AUTO)

 Emergency ram air inlet

 Avionics ventilation inlet valve

 Avionics ventilation extract valve

 Pack flow control valves

NOTE: Each valve listed above is located below the aircraft’s flotation line.

Recall the Avionics Compartment’s venting and cooling

configuration which is not automatic and requires pilot

action.

The ____ _____configuration requires pilot action in order to ___ ____

within the ____ ____ overboard.

Placing the _______ and ______ pbs to ____ (_____):

•allows ____ ___ from the ___ _______system to enter the ___________

•forces all ___ within the __________ ______.

Recall the Avionics Compartment’s venting and cooling

configuration which is not automatic and requires pilot

action.

 The AVIONICS SMOKE configuration requires pilot action in order to vent smoke within the avionics compartment overboard.

 Placing the BLOWER and EXTRACT pbs to OVRD (white):

•allows additional air from the air conditioning system to enter the compartment

•forces all air within the compartment overboard

Recall the Avionics Compartment’s venting and cooling

configuration which is not automatic and requires pilot action.

NOTE: ____ (_____) appears on the _____ and _____pb as the result of

_____ being detected in the _____compartment.

Recall the Avionics Compartment’s venting and cooling

configuration which is not automatic and requires pilot action.

NOTE: FAULT (amber) appears on the BLOWER and EXTRACT pb as the result of smoke being detected in the avionics compartment.