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A partir de los siguientes datos recogidos por la EPA, calcula la tasa de paro juvenil. (1)

DES page

The descent page provides the crew with access to descent planning

The descent page provides the crew with access to descent planning

and inormation. The DES page is selected by pressing the VNAV key

and inormation. The DES page is selected by pressing the VNAV key

on the FMC/MCDU keypad. The NEXT PAGE/PREV PAGE keys may

on the FMC/MCDU keypad. The NEXT PAGE/PREV PAGE keys may

need to be used

need to be used i the aircrat is still at i the aircrat is still at cruise altitude.cruise altitude.

E/D AT:

E/D AT: The End o Descent At inormation displayed in 1L describesThe End o Descent At inormation displayed in 1L describes

the altitude and waypoint at which the descent is planned to end.

the altitude and waypoint at which the descent is planned to end.

Speed Mode:

Speed Mode: Line 2L contains the descent speed mode inormation.Line 2L contains the descent speed mode inormation.

The current descent speed mode is displayed in small ont in the 2L

The current descent speed mode is displayed in small ont in the 2L

header line. The descent speed is

header line. The descent speed is displayed in large ont, in the CAS/ displayed in large ont, in the CAS/ 

Mach ormat. Descent speed modes

Mach ormat. Descent speed modes available are:available are:

ECON DES: The economy descent mode will yield the lowest aircrat

ECON DES: The economy descent mode will yield the lowest aircrat

operating cost based on the entered cost index. The ECON DES mode

operating cost based on the entered cost index. The ECON DES mode

will attempt to provide an idle thrust descent unless wind conditions

will attempt to provide an idle thrust descent unless wind conditions

encountered during the descent require thrust.

encountered during the descent require thrust.

MCP SPD DES: The MCP selected speed descent mode is a pilot

MCP SPD DES: The MCP selected speed descent mode is a pilot

selected descent speed mode. To initiate this mode, the pilot pushes

selected descent speed mode. To initiate this mode, the pilot pushes

the MCP speed select knob. The speed o the descent can then be

the MCP speed select knob. The speed o the descent can then be

adjusted by selecting the desired speed in the MCP speed

adjusted by selecting the desired speed in the MCP speed selectorselector

window.

LIM SPD DES: The

LIM SPD DES: The limit speed descent mode becomes active in caseslimit speed descent mode becomes active in cases

where the target descent speed exceeds the capabilities o the

where the target descent speed exceeds the capabilities o the

airrame in either the overspeed regime, or the stall buet margin. The

airrame in either the overspeed regime, or the stall buet margin. The

limit speed is own by the vertical guidance unction.

limit speed is own by the vertical guidance unction.

END OF DES: The prompt END OF DES is displayed in the descent

END OF DES: The prompt END OF DES is displayed in the descent

speed mode line when the aircrat has passed the programmed end o

speed mode line when the aircrat has passed the programmed end o

descent constraint waypoint.

descent constraint waypoint.

SPD TRANS:

SPD TRANS: Line 3L displays the speed transition altitude. The lineLine 3L displays the speed transition altitude. The line

contains the transition speed, ollowed by the transition altitude in a

contains the transition speed, ollowed by the transition altitude in a

SSS/AAAAA ormat. This feld may not be updated manually, but it may

SSS/AAAAA ormat. This feld may not be updated manually, but it may

be deleted by pressing the FMC/MCDU DELETE key, then pressing 3L.

be deleted by pressing the FMC/MCDU DELETE key, then pressing 3L.

SPD REST:

SPD REST: Line 4L provides the crew with the ability to enter anLine 4L provides the crew with the ability to enter an

altitude dependent speed restriction. The line contains transition

altitude dependent speed restriction. The line contains transition

speed, ollowed by the transition altitude in a SSS/AAAAA ormat. The

speed, ollowed by the transition altitude in a SSS/AAAAA ormat. The

altitude entry must be an altitude below the cruise altitude, but above

altitude entry must be an altitude below the cruise altitude, but above

the End o Descent altitude.

the End o Descent altitude.

Next Descent Constraint:

Next Descent Constraint: Line 1R contains the descent constraintLine 1R contains the descent constraint

waypoint as defned in the RTE LEGS page o the ight plan. The

waypoint as defned in the RTE LEGS page o the ight plan. The

header line contains ‘AT’ ollowed by the navigation fx identifer to

header line contains ‘AT’ ollowed by the navigation fx identifer to

which the descent constraint is assigned. The constraint is displayed in

which the descent constraint is assigned. The constraint is displayed in

the DES page exactly as it appears in the RTE LEGS page. The

the DES page exactly as it appears in the RTE LEGS page. The descentdescent

constraint cannot be updated or changed rom the DES page, but it

constraint cannot be updated or changed rom the DES page, but it

may be deleted. Deleting the constraint will remove it rom the lateral

may be deleted. Deleting the constraint will remove it rom the lateral

route.

route.

Descend Now Prompt (DES NOW):

Descend Now Prompt (DES NOW): When the aircrat is notWhen the aircrat is not

currently descending, but the MCP altitude selector is set below the

currently descending, but the MCP altitude selector is set below the

current altitude, the DES NOW prompt will be displayed at 6R. The

current altitude, the DES NOW prompt will be displayed at 6R. The

DES NOW> prompt deletes all climb/cruise constraints and commences

DES NOW> prompt deletes all climb/cruise constraints and commences

an early descent. The rate o descent will be approximately 1250 eet

an early descent. The rate o descent will be approximately 1250 eet

per minute until the aircrat intercepts the originally planned vertical

per minute until the aircrat intercepts the originally planned vertical

descent path which would have commenced at the top-o-descent

descent path which would have commenced at the top-o-descent

mark.

Descend Direct Prompt (DES DIR):

Descend Direct Prompt (DES DIR): When the aircrat is descendingWhen the aircrat is descending

and the MCP altitude selector is set below the current aircrat altitude,

and the MCP altitude selector is set below the current aircrat altitude,

the DES DIR> prompt will be displayed. Pressing the associated LSK will

the DES DIR> prompt will be displayed. Pressing the associated LSK will

delete all altitude constraints between the aircrat and the MCP

delete all altitude constraints between the aircrat and the MCP

selected altitude and the FMC will command a descent to reach the

selected altitude and the FMC will command a descent to reach the

MCP altitude. Upon reaching the MCP selected altitude, the vertical

MCP altitude. Upon reaching the MCP selected altitude, the vertical

guidance unction o the FMC will capture the originally computed

guidance unction o the FMC will capture the originally computed

vertical path or the remainder o the descent. Unless deleted or

vertical path or the remainder o the descent. Unless deleted or

modifed, all remaining descent constraints will be adhered to.

modifed, all remaining descent constraints will be adhered to.

Opath Descent Prompt (OFFPATH DES):

Opath Descent Prompt (OFFPATH DES): The opath descent pageThe opath descent page

provides access to “Clean” and speed brake direct descent profles i

provides access to “Clean” and speed brake direct descent profles i

the crew does not wish to use the FMC calculated descent path. This

the crew does not wish to use the FMC calculated descent path. This

page can be access through the <OFFPATH DES prompt in 6L o the

page can be access through the <OFFPATH DES prompt in 6L o the

DES page or DESCENT FORCASTS page.

DES page or DESCENT FORCASTS page.

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