ATA 32: Landing Gear Flashcards

1
Q

The landing gear is not down on approach (below 750 R.A) and full flap is selected. Warning lights appear and a continuous repetitive chime sounds. The chime can be cancelled by:

(a) Pressing Master Caution push button
(b) Pressing Master Warning push button
(c) Pressing the EMERG CANCEL push button

A

(c) Pressing the EMERG CANCEL push button

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2
Q

The disconnect button on the Captain’s steering hand wheel when depressed:

(a) Allows steering authority by rudder pedals
(b) Allows steering authority by Captain’s rudder pedals
(c) Disconnects the rudder pedal input to the Brake and Steering Control Unit (BSCU)

A

(c) Disconnects the rudder pedal input to the Brake and Steering Control Unit (BSCU)

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3
Q

LDGGR_01
Understand the control functions and indications on the LND GEAR panel.
1. UNLK Lights

  • Illuminates red if there is a __________ between the selected gear position and the actual position of the gear.

VOL II., 32.3.2-6

A

LDGGR_01
Understand the control functions and indications on the LND GEAR panel.
1. UNLK Lights

  • Illuminates red if there is a disagreement between the selected gear position and the actual position of the gear.

VOL II., 32.3.2-6

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4
Q

LDGGR_01
Understand the control functions and indications on the LND GEAR panel.
2. Green Triangles

  • Illuminates green when LGCIU 1 (LANDING GEAR CONTROL INTERFACE UNIT) detects that the respective gear is _____________\_

VOL II., 32.3.2-6

A

LDGGR_01
Understand the control functions and indications on the LND GEAR panel.
2. Green Triangles

  • Illuminates green when LGCIU 1 (LANDING GEAR CONTROL INTERFACE UNIT) detects that the respective gear is downlocked.

VOL II., 32.3.2-6

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5
Q

LDGGR_01
Understand the control functions and indications on the LND GEAR panel.
3. Landing Gear Lever

  • UP - The landing gear are selected up.
  • DOWN - The landing gear are selected down.
  • Red Arrow
    • Illuminates red if the gear are not ________ and either:
      • The aircraft is below [_____] ft. RA and flaps ________,
      • or
      • The aircraft is below [_____] RA with flaps __ or __, and engines not at ________ power,
      • or
      • Both ________ altimeters are failed and the flaps are selected to position __, __, or ______.
A

LDGGR_01
Understand the control functions and indications on the LND GEAR panel.
3. Landing Gear Lever

  • UP - The landing gear are selected up.
  • DOWN - The landing gear are selected down.
  • Red Arrow
    • Illuminates red if the gear are not downlocked and either:
      • The aircraft is below [750] ft. RA and flaps full,
      • or
      • The aircraft is below [750] RA with flaps 2 or 3, and engines not at TOGA power,
      • or
      • Both radio altimeters are failed and the flaps are selected to position 2, 3, or FULL.

VOL II., 32.3.2-6

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6
Q

LDGGR_01
Understand the control functions and indications on the LND GEAR panel.
4. LDG GEAR GRVTY EXTN Selector
• OFF - Landing gear gravity extension is not _______

• DOWN:

  • Isolates the landing gear from the ________ hydraulic system,
  • ________ unlocks the landing gear doors,
  • and allows the landing gear to extend by________.
  • ______ ______ is also lost.

• RESET (momentary action) - Resets the landing gear system.

If the malfunction that required the gravity extension is no longer present, selecting ________:

  • ________ the gear doors
  • Recovers normal gear ______ and ______
  • Recovers ______ ______

• Red Selector Guards -

  • Prevent inadvertent ________of the LDG GEAR GRVTY EXTN selector.
  • Hinged so they can be moved if landing gear gravity ________is desired.

VOL II., 32.3.2-6

A

LDGGR_01
Understand the control functions and indications on the LND GEAR panel.
4. LDG GEAR GRVTY EXTN Selector
• OFF - Landing gear gravity extension is not selected.
• DOWN:

  • Isolates the landing gear from the green hydraulic system,
  • electrically unlocks the landing gear doors,
  • and allows the landing gear to extend by gravity.
  • Nosewheel steering is also lost.

• RESET (momentary action) - Resets the landing gear system.

If the malfunction that required the gravity extension is no longer present, selecting RESET:

  • Closes the gear doors
  • Recovers normal gear extension and retraction
  • Recovers nosewheel steering

• Red Selector Guards -

  • Prevent inadvertent movement of the LDG GEAR GRVTY EXTN selector.
  • Hinged so they can be moved if landing gear gravity extension is desired.

VOL II., 32.3.2-6

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7
Q

LDGGR_01
Understand the control functions and indications on the LND GEAR panel.
5. DECEL Lights

  • • Illuminates green:
    • if the respective autobrake setting is ________
    • and actual aircraft deceleration reaches [____%] of the TARGET rate for LO or MED or a FIXED rate for MAX.
  • • ON Lights - Illuminates ________ when the respective setting has been ________

VOL II., 32.3.2-6

A

LDGGR_01
Understand the control functions and indications on the LND GEAR panel.
5. DECEL Lights

  • • Illuminates green:
    • if the respective autobrake setting is active
    • and actual aircraft deceleration reaches [80%] of the target rate for LO or MED or a fixed rate for MAX.
  • • ON Lights - Illuminates blue when the respective setting has been armed.

VOL II., 32.3.2-6

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8
Q

LDGGR_01
Understand the control functions and indications on the LND GEAR panel.

  1. A/SKID & N/W STRG Switch
  • ON - Both channels of the ______ ______ ______ ______ (BSCU) are available.
  • OFF - Both channels of the BSCU are off. As a result:
    • ________ braking is lost.
    • ________ is lost.
    • ______ ______ is lost.
    • ________ lost

VOL II., 32.3.2-6

A

LDGGR_01
Understand the control functions and indications on the LND GEAR panel.

  1. A/SKID & N/W STRG Switch
  • ON - Both channels of the Brake Steering Control Unit (BSCU) are available.
  • OFF - Both channels of the BSCU are off. As a result:
    • Normal braking is lost.
    • Antiskid is lost.
    • Nosewheel steering is lost.
    • Autobrakes lost

VOL II., 32.3.2-6

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9
Q

LDGGR_01
Understand the control functions and indications on the LND GEAR panel.

7. BRAKES Indicator

  • Provides indications of ________ hydraulic system brake pressure if ________ braking is unavailable or the ________ brake is set.
  • The top of the green arcs indicate the ________ recommended brake pressure of [________] psi to prevent locking the brakes if the ________ is inoperative.

VOL II., 32.3.2-6

A

LDGGR_01
Understand the control functions and indications on the LND GEAR panel.

7. BRAKES Indicator

  • Provides indications of blue hydraulic system brake pressure if normal braking is unavailable or the parking brake is set.
  • The top of the green arcs indicate the maximum recommended brake pressure of [1000] psi to prevent locking the brakes if the antiskid is inoperative.

VOL II., 32.3.2-6

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10
Q

LDGGR_01
Understand the control functions and indications on the LND GEAR panel.

8. ACCU PRESS Indicator

  • Provides indications of remaining ________ hydraulic accumulator pressure.
  • Normal accumulator pressure is indicated by the ________ band.
  • If the indicator is in the amber band, accumulator pressure is ______ ______.

VOL II., 32.3.2-6

A

LDGGR_01
Understand the control functions and indications on the LND GEAR panel.

8. ACCU PRESS Indicator

  • Provides indications of remaining blue hydraulic accumulator pressure.
  • Normal accumulator pressure is indicated by the green band.
  • If the indicator is in the amber band, accumulator pressure is critically low.

VOL II., 32.3.2-6

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11
Q

LDGGR_02
Understand the control functions of the Parking Brake Handle.
Parking Brake Handle

  • ON - Pull up while turning ________ to engage parking brake.
    • ______ and ______ braking systems are deactivated and braking pressure is applied by the ________ system or ______ ______.
    • PARK BRK memo message is displayed.
  • OFF - Parking brake is released.

VOL II., 32.3.2-6

A

LDGGR_02
Understand the control functions of the Parking Brake Handle.
Parking Brake Handle

  • ON - Pull up while turning clockwise to engage parking brake.
    • Normal and alternate braking systems are deactivated and braking pressure is applied by the blue system or brake accumulator.
    • PARK BRK memo message is displayed.
  • OFF - Parking brake is released.

VOL II., 32.3.2-6

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12
Q

LDGGR_03
Understand the control functions of the Steering Handwheels.

  • Steering handwheels are located on each pilot’s outboard side console.
  • The handwheels command a nosewheel angle that corresponds to the angles printed on their base.
  • Full authority is [____°] L/R and gradually ________ as ground speed increases.
  • As the angle of the handwheel increases, additional steering inputs result in a ______ ______ in nosewheel angle
    • (i.e., nosewheel steering using the handwheels is ______ ______ as the angle of the handwheel______).

VOL II., 32.1.7.1-4

A

LDGGR_03
Understand the control functions of the Steering Handwheels.

  • Steering handwheels are located on each pilot’s outboard side console.
  • The handwheels command a nosewheel angle that corresponds to the angles printed on their base.
  • Full authority is [72°] L/R and gradually decreases as ground speed increases.
  • As the angle of the handwheel increases, additional steering inputs result in a larger change in nosewheel angle
    • (i.e., nosewheel steering using the handwheels is more sensitive as the angle of the handwheel increases).

VOL II., 32.1.7.1-4

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13
Q

LDGGR_03
Understand the control functions of the Steering Handwheels.

  • The handwheels are not ____________
  • Inputs made with one handwheel do not affect the position of the other handwheel.
  • If an input is made with both handwheels simultaneously, the combined input is _______ by the _______ up to the _______ authority for one handwheel.

VOL II., 32.1.7.1-4

A

LDGGR_03
Understand the control functions of the Steering Handwheels.

  • The handwheels are not interconnected.
  • Inputs made with one handwheel do not affect the position of the other handwheel.
  • If an input is made with both handwheels simultaneously, the combined input is summed by the BSCU up to the maximum authority for one handwheel.

VOL II., 32.1.7.1-4

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14
Q

LDGGR_03
Understand the control functions of the Steering Handwheels.

The rudder pedals can be _______ from nosewheel steering (e.g., for checking rudder travel during taxi):

  • by pushing and holding the _____ _____ pushbutton in the center of the steering handwheel.
  • Releasing the pushbutton _______ steering control to the rudder pedals.

VOL II., 32.1.7.1-4

A

LDGGR_03
Understand the control functions of the Steering Handwheels.

The rudder pedals can be disconnected from nosewheel steering (e.g., for checking rudder travel during taxi):

  • by pushing and holding the PEDALS DISC pushbutton in the center of the steering handwheel.
  • Releasing the pushbutton returns steering control to the rudder pedals.

VOL II., 32.1.7.1-4

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15
Q

LDGGR_04
Discuss normal and abnormal indications on the ECAM WHEEL page.
1. Spoiler Indications

  • Indicates the __________ of the spoilers.

VOL II., 32.3.9

A

LDGGR_04
Discuss normal and abnormal indications on the ECAM WHEEL page.
1. Spoiler Indications

  • Indicates the position of the spoilers.

VOL II., 32.3.9

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16
Q

LDGGR_04
Discuss normal and abnormal indications on the ECAM WHEEL page.
2. Gear Door Indications
The door indications provide a graphical representation of the gear door position:

  • locked up (_______),
  • in transit or open (_______),

An _______ indication appears above the gear door if the uplock is engaged when the landing gear is ______._
VOL II., 32.3.9

A

LDGGR_04
Discuss normal and abnormal indications on the ECAM WHEEL page.
2. Gear Door Indications
The door indications provide a graphical representation of the gear door position:

  • locked up (green),
  • in transit or open (amber),

An UPLOCK indication appears above the gear door if the uplock is engaged when the landing gear is DOWNLOCKED.
VOL II., 32.3.9

17
Q

LDGGR_04
Discuss normal and abnormal indications on the ECAM WHEEL page.
3. Landing Gear Indications

  • Two _______ indicate the landing gear position.
    • The left triangle from_______,
    • the right triangle from _______.
  • _______ Triangle - Landing gear downlocked
  • Red Triangle - Landing gear __ _____
  • No symbol - Landing gear_____
  • XX (amber) - _____ _____

VOL II., 32.3.9

A

LDGGR_04
Discuss normal and abnormal indications on the ECAM WHEEL page.
3. Landing Gear Indications

  • Two triangles indicate the landing gear position.
    • The left triangle from LGCIU 1,
    • the right triangle from LGCIU 2.
  • Green Triangle - Landing gear downlocked
  • Red Triangle - Landing gear in transit
  • No symbol - Landing gear uplocked
  • XX (amber) - LGCIU failure

VOL II., 32.3.9

18
Q

LDGGR_04
Discuss normal and abnormal indications on the ECAM WHEEL page.
4. Brake Temperatures
Indicates brake temperature on the respective wheel.

  • Normally ______,_
  • minimum display temperature [____°]C.
  • Amber at ____°_ C and above.
  • An arc appears _______ the wheel with the _______ brakes (min temp [__\_°C]),
  • if that temperature is greater than _____°, the arc is _______

VOL II., 32.3.9

A

LDGGR_04
Discuss normal and abnormal indications on the ECAM WHEEL page.
4. Brake Temperatures
Indicates brake temperature on the respective wheel.

  • Normally green,
  • minimum display temperature [0°]C.
  • Amber at 300° C and above.
  • An arc appears above the wheel with the hottest brakes (min temp [100°C]),
  • if that temperature is greater than 300°, the arc is amber

VOL II., 32.3.9

19
Q

LDGGR_04
Discuss normal and abnormal indications on the ECAM WHEEL page.
5. Tire Pressures

  • Deactived.

6. Messages

  • _____ _____ (amber) - Normal braking is lost
  • ANTI-SKID (amber) - _______ function is lost
  • AUTO BRK
    • Green - Auto brake is _______, followed by selected setting LO, MED, or MAX
    • Amber - _______ is lost

VOL II., 32.3.9

A

LDGGR_04
Discuss normal and abnormal indications on the ECAM WHEEL page.
5. Tire Pressures

  • Deactived.

6. Messages

  • NORM BRK (amber) - Normal braking is lost
  • ANTI-SKID (amber) - Anti-skid function is lost
  • AUTO BRK
    • Green - Auto brake is armed, followed by selected setting LO, MED, or MAX
    • Amber - Auto brake is lost

VOL II., 32.3.9

20
Q

LDGGR_04
Discuss normal and abnormal indications on the ECAM WHEEL page.

7. Antiskid Indications
Vertical bars indicate the anti-skid system.

The “R” is permanently displayed to indicate the bars refer to the brake ______._

  • Green - Brakes are _____: (in flight with _____ _____, or released due to _______ activation during braking)
  • Amber - _______ brake pressure exists when a release command is given, or brake release _______ is detected.

VOL II., 32.3.9

A

LDGGR_04
Discuss normal and abnormal indications on the ECAM WHEEL page.

7. Antiskid Indications
Vertical bars indicate the anti-skid system.

The “R” is permanently displayed to indicate the bars refer to the brake release.

  • Green - Brakes are released: (in flight with gear extended, or released due to antiskid activation during braking)
  • Amber - Residual brake pressure exists when a release command is given, or brake release fault is detected.

VOL II., 32.3.9

21
Q

LDGGR_04
Discuss normal and abnormal indications on the ECAM WHEEL page.
8. N/W STRG

  • N/W STRG appears in amber if nosewheel steering is lost due to:
    • Failure detected by _______
    • A/SKID & N/W STRG switch _______
    • Failure of both _______ channels

VOL II., 32.3.9

A

LDGGR_04
Discuss normal and abnormal indications on the ECAM WHEEL page.
8. N/W STRG

  • N/W STRG appears in amber if nosewheel steering is lost due to:
    • Failure detected by BSCU
    • A/SKID & N/W STRG switch OFF
    • Failure of both BSCU channels

VOL II., 32.3.9

22
Q

LDGGR_05
Discuss the meaning of the ECAM memos as they relate to landing gear/brakes system.
N/W DISC

  • Displayed in green when the towing lever on the nose gear is in the _______ position.
  • It is displayed in _______ if an engine is running.

VOL II., 32.3.11

A

LDGGR_05
Discuss the meaning of the ECAM memos as they relate to landing gear/brakes system.
N/W DISC

  • Displayed in green when the towing lever on the nose gear is in the TOWING position.
  • It is displayed in amber if an engine is running.

VOL II., 32.3.11

23
Q

LDGGR_05
Discuss the meaning of the ECAM memos as they relate to landing gear/brakes system.
PARK BRK

  • Displayed in green when the parking brake is set.
  • It is displayed in amber if the parking brake is set in _______

VOL II., 32.3.11

A

LDGGR_05
Discuss the meaning of the ECAM memos as they relate to landing gear/brakes system.
PARK BRK

  • Displayed in green when the parking brake is set.
  • It is displayed in amber if the parking brake is set in flight.

VOL II., 32.3.11

24
Q

LDGGR_05
Discuss the meaning of the ECAM memos as they relate to landing gear/brakes system.

AUTO BRK LO

  • Displayed in green when autobrakes LO is armed and the aircraft is below [_____] feet.

VOL II., 32.3.11

A

LDGGR_05
Discuss the meaning of the ECAM memos as they relate to landing gear/brakes system.

AUTO BRK LO

  • Displayed in green when autobrakes LO is armed and the aircraft is below [800] feet.

VOL II., 32.3.11

25
LDGGR\_05 **Discuss the meaning of the ECAM memos as they relate to landing gear/brakes system.** **AUTO BRK MED** * Displayed in green when autobrakes MED is armed and the aircraft is below [_**\_\_\_**_] feet. VOL II., 32.3.11
LDGGR\_05 **Discuss the meaning of the ECAM memos as they relate to landing gear/brakes system.** **AUTO BRK MED** * Displayed in green when autobrakes MED is armed and the aircraft is below [**_800_**] feet. VOL II., 32.3.11
26
LDGGR\_06 Recall which hydraulic system is needed for the landing gear and nosewheel steering operations. * The _**\_\_\_\_**_ hydraulic system is required for all landing gear and nosewheel steering operations. VOL II, 32.1.3.1
LDGGR\_06 Recall which hydraulic system is needed for the landing gear and nosewheel steering operations. * The **_green_** hydraulic system is required for all landing gear and nosewheel steering operations. VOL II, 32.1.3.1
27
LDGGR\_07 Describe the autobrake system design. * The autobrakes are armed using the pbs on the center instrument panel. * The **\_\_\_\_\_e \_\_\_** light in the pb indicates that the respective setting has been armed. * The autobrakes can be armed provided all of the following conditions are met: * _**\_\_\_\_\_**_ hydraulic pressure is available. * _**\_\_\_\_\_**_ is available. * At least two _**\_\_\_\_\_**_ are available. * At least one _**\_\_\_\_\_**_ is available. * No _**\_\_\_\_\_**_ in the brake system. VOL II., 32.2.4.1-4
LDGGR\_07 Describe the autobrake system design. * The autobrakes are armed using the pbs on the center instrument panel. * The **_blue ON_** light in the pb indicates that the respective setting has been armed. * The autobrakes can be armed provided all of the following conditions are met: * **_Green_** hydraulic pressure is available. * **_Antiskid_** is available. * At least two **_PRIMs_** are available. * At least one **_ADIRU_** is available. * No **_failure_** in the brake system. VOL II., 32.2.4.1-4
28
LDGGR\_07 Describe the autobrake system design. When armed, each of the three settings activate at different times and provide different rates of deceleration. * The activation of the autobrakes is dependent on the deployment of the ground spoilers: * LO - Used for landing. * The brakes are applied starting **\_\_\_ \_\_\_\_\_** after **\_\_\_\_\_ _____ \_\_\_\_\_**. * MED - Used for landing. * The brakes are applied starting at **\_\_\_\_\_ _____ \_\_\_\_\_**. * The deceleration rate is higher than _**\_\_\_**_. * MAX - Used for takeoff only. * In case of an aborted takeoff, maximum antiskid braking is used starting when the **\_\_\_\_\_ _____ \_\_\_\_\_** signal is sent. * ground spoilers do not deploy if wheel speed is below _**\_\_**_ knots. VOL II., 32.2.4.1-4
LDGGR\_07 Describe the autobrake system design. When armed, each of the three settings activate at different times and provide different rates of deceleration. * The activation of the autobrakes is dependent on the deployment of the ground spoilers: * LO - Used for landing. * The brakes are applied starting **_one second_** after **_ground spoiler deployment_**. * MED - Used for landing. * The brakes are applied starting at **_ground spoiler deployment_**. * The deceleration rate is higher than **_LO_**. * MAX - Used for takeoff only. * In case of an aborted takeoff, maximum antiskid braking is used starting when the **_ground spoiler extension_** signal is sent. * ground spoilers do not deploy if wheel speed is below **_72_** knots. VOL II., 32.2.4.1-4
29
LDGGR\_07 Describe the autobrake system design. In order for MAX autobrakes to activate: * The **\_\_\_\_\_ \_\_\_\_\_** strut must be compressed. * An aborted takeoff must be initiated with wheel speed at least _**\_\_**_ knots * (ground spoilers do not deploy if wheel speed is below _**\_\_**_ knots). VOL II., 32.2.4.1-4
LDGGR\_07 Describe the autobrake system design. In order for MAX autobrakes to activate: * The **_nose gear_** strut must be compressed. * An aborted takeoff must be initiated with wheel speed at least **_72_** knots * (ground spoilers do not deploy if wheel speed is below **_72_** knots). VOL II., 32.2.4.1-4
30
LDGGR\_07 Describe the autobrake system design. If the autobrakes are active a green _**\_\_\_\_\_**_ light illuminates in the respective pb when: * actual aircraft deceleration reaches a _**\_\_\_\_\_**_ rate for LO and MED * and a _**\_\_\_\_\_**_ rate for MAX. If reverse thrust is added during deceleration while LO or MED is active, * _**\_\_\_\_\_**_ braking is applied resulting in the same _**\_\_\_\_\_**_ rate * and little change in _**\_\_\_\_\_**_ distance. Note: On a slippery runway, the _**\_\_\_\_\_**_ deceleration rate may not be reached due to antiskid operation. * In this case the _**\_\_\_\_\_**_ light will not illuminate. * This does not mean that the _**\_\_\_\_\_**_ are not working. VOL II., 32.2.4.1-4
LDGGR\_07 Describe the autobrake system design. If the autobrakes are active a green **_DECEL_** light illuminates in the respective pb when: * actual aircraft deceleration reaches a **_target_** rate for LO and MED * and a **_fixed_** rate for MAX. If reverse thrust is added during deceleration while LO or MED is active, * **_less_** braking is applied resulting in the same **_deceleration_** rate * and little change in **_stopping_** distance. Note: On a slippery runway, the **_predetermined_** deceleration rate may not be reached due to antiskid operation. * In this case the **_DECEL_** light will not illuminate. * This does not mean that the **_autobrakes_** are not working. VOL II., 32.2.4.1-4
31
LDGGR\_08 Discuss the normal, alternate, and parking brake operations. **_NORMAL_** Normal braking uses _**\_\_\_\_\_**_ hydraulic pressure and is available if all of the following conditions are met: * _**\_\_\_\_\_**_ hydraulic pressure is available. * The main landing gears are on the _**\_\_\_\_\_**_. * At least one channel of the _**\_\_\_\_\_**_ is available (A/SKID & NWS switch is _**\_\_\_\_\_)**_. * The PARK BRK is _**\_\_\_\_\_**_. When normal braking is active: * the alternate system is _**\_\_\_\_\_**_ * and the brake pressure gauge indicates **_zero._** In normal braking, **\_\_\_\_\_ and \_\_\_\_\_** are available. The loss of normal braking is indicated by an amber _**\_\_\_\_\_**_ message on the WHEEL page. VOL. II, 32.2.3.2
LDGGR\_08 Discuss the normal, alternate, and parking brake operations. **_NORMAL_** Normal braking uses **_green_** hydraulic pressure and is available if all of the following conditions are met: * **_Green_** hydraulic pressure is available. * The main landing gears are on the **_ground_**. * At least one channel of the **_BSCU_** is available (A/SKID & NWS switch is **_ON)_**. * The PARK BRK is **_OFF_**. When normal braking is active: * the alternate system is **_depressurized_** * and the brake pressure gauge indicates **_zero._** In normal braking, **_antiskid and autobrakes_** are available. The loss of normal braking is indicated by an amber **_NORM BRK_** message on the WHEEL page. VOL. II, 32.2.3.2
32
LDGGR\_08 Discuss the normal, alternate, and parking brake operations. **_ALTERNATE_** * The alternate brake system uses _**\_\_\_\_\_**_ hydraulic pressure. * The autobrakes are inoperative if the _**\_\_\_\_\_**_ system is active. * *If the _**\_\_\_\_\_**_ is available, antiskid may be available on the alternate system. NOT LOD* VOL. II, 32.2.3.3
LDGGR\_08 Discuss the normal, alternate, and parking brake operations. **_ALTERNATE_** * The alternate brake system uses **_blue_** hydraulic pressure. * The autobrakes are inoperative if the **_alternate_** system is active. * *If the **_BSCU_** is available, antiskid may be available on the alternate system. NOT LOD* VOL. II, 32.2.3.3
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LDGGR\_08 Discuss the normal, alternate, and parking brake operations. **_ALTERNATE_** The brake system will degrade to alternate braking, and antiskid may be available, if: * _**\_\_\_\_\_**_ hydraulic pressure is low and any of the following conditions are met: * _**\_\_\_\_\_**_ hydraulic pressure is available. * One channel of the _**\_\_\_\_\_**_ is available (A/SKID & NWS switch is _**\_\_\_\_\_**_). * The PARK BRK is _**\_\_\_\_\_**_. VOL. II, 32.2.3.3
LDGGR\_08 Discuss the normal, alternate, and parking brake operations. **_ALTERNATE_** The brake system will degrade to alternate braking, and antiskid may be available, if: * **_Green_** hydraulic pressure is low and any of the following conditions are met: * **_Blue_** hydraulic pressure is available. * One channel of the **_BSCU_** is available (A/SKID & NWS switch is **_ON_**). * The PARK BRK is **_OFF_**. VOL. II, 32.2.3.3
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LDGGR\_08 Discuss the normal, alternate, and parking brake operations. **_ALTERNATE_** The _**\_\_\_\_\_\_\_\_\_**_ indicator, installed on the center instrument panel, provides indications of current brake pressure if the _______ system is active. VOL. II, 32.2.3.3
LDGGR\_08 Discuss the normal, alternate, and parking brake operations. **_ALTERNATE_** The **_BRAKES_** indicator, installed on the center instrument panel, provides indications of current brake pressure if the **_alternate_** system is active. VOL. II, 32.2.3.3
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LDGGR\_08 Discuss the normal, alternate, and parking brake operations. **_ALTERNATE_** Antiskid will not be available if alternate braking is active due to either: * A failure of _**\_\_\_\_\_ \_\_\_\_\_**_ of the BSCU or the A/SKID & NWS switch selected _**\_\_\_\_\_**_. * Low **\_\_\_\_\_ and \_\_\_\_\_** hydraulic pressure (only accumulator pressure is available). The diagram below illustrates how the brake system is configured with the brakes applied in alternate braking as a result of a loss of both channels of the BSCU. VOL. II, 32.2.3.3
LDGGR\_08 Discuss the normal, alternate, and parking brake operations. **_ALTERNATE_** Antiskid will not be available if alternate braking is active due to either: * A failure of **_both_** **_channels_** of the BSCU or the A/SKID & NWS switch selected **_OFF_**. * Low **_green and blue_** hydraulic pressure (only accumulator pressure is available). The diagram below illustrates how the brake system is configured with the brakes applied in alternate braking as a result of a loss of both channels of the BSCU. VOL. II, 32.2.3.3
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LDGGR\_08 Discuss the normal, alternate, and parking brake operations. **_ALTERNATE_** A hydraulic accumulator, within the _**\_\_\_\_\_**_ brake system, provides a backup source of\_\_\_\_\_ hydraulic pressure to the alternate brake system in case of low _**\_\_\_\_\_**_ and _**\_\_\_\_\_**_ hydraulic pressure. * Antiskid is not available when _**\_\_\_\_\_**_ braking is in use. * This prevents premature exhaustion of _**\_\_\_\_\_**_ pressure. * The accumulator will provide a minimum of _**\_\_\_\_\_**_ full brake applications. * The **\_\_\_\_\_ \_\_\_\_\_** indicator, installed on the center instrument panel, provides indications of remaining accumulator pressure. VOL. II, 32.2.3.3
LDGGR\_08 Discuss the normal, alternate, and parking brake operations. **_ALTERNATE_** A hydraulic accumulator, within the **_alternate_** brake system, provides a backup source of **_blue_** hydraulic pressure to the alternate brake system in case of low **_green_** and **_blue_** hydraulic pressure. * Antiskid is not available when **_accumulator_** braking is in use. * This prevents premature exhaustion of **_accumulator_** pressure. * The accumulator will provide a minimum of **_seven_** full brake applications. * The **_ACCU PRESS_** indicator, installed on the center instrument panel, provides indications of remaining accumulator pressure. VOL. II, 32.2.3.3
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LDGGR\_08 Discuss the normal, alternate, and parking brake operations. **_PARKING BRAKE_** An _**\_\_\_\_\_**_ controlled parking brake, when set, applies brake pressure from the: * _**\_\_\_\_\_**_ hydraulic system * or the _**\_\_\_\_\_**_ to the brakes. * The parking brake is operated by a control handle located on the left side of the pedestal. The diagram below illustrates how the brake system is configured when the parking brake is set. VOL. II, 32.2.3.4
LDGGR\_08 Discuss the normal, alternate, and parking brake operations. **_PARKING BRAKE_** An **_electrically_** controlled parking brake, when set, applies brake pressure from the: * **_blue_** hydraulic system * or the **_accumulator_** to the brakes. * The parking brake is operated by a control handle located on the left side of the pedestal. The diagram below illustrates how the brake system is configured when the parking brake is set. VOL. II, 32.2.3.4
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LDGGR\_08 Discuss the normal, alternate, and parking brake operations. **_PARKING BRAKE_** Placing the PARK BRK handle to ON: * deactivates **\_\_\_\_\_ and \_\_\_\_\_e** braking modes and the _**\_\_\_\_\_**_ system. Parking brake pressure is supplied by: * _**\_\_\_\_\_**_ hydraulic system pressure * or the brake _**\_\_\_\_\_**_ and displayed on the _**\_\_\_\_\_**_ indicator. VOL. II, 32.2.3.4
LDGGR\_08 Discuss the normal, alternate, and parking brake operations. **_PARKING BRAKE_** Placing the PARK BRK handle to ON: * deactivates **_normal and alternate_** braking modes and the **_antiskid_** system. Parking brake pressure is supplied by: * **_blue_** hydraulic system pressure * or the brake **_accumulato_**r and displayed on the **_BRAKES_** indicator. VOL. II, 32.2.3.4