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时间:2010-05-01 10:09来源:蓝天飞行翻译 作者:admin
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supplied by pressing in the external power (EXT PWR)
pushbutton.
After the safety test of the computers, the FCU and
the MCDU are energized and Flight Director is
automatically engaged.
The STATUS page is displayed.
TMUFM3301-T01 LEVEL 3
EFFECTIVITY 22-70-00 Page 2
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 218
ALL
FMGS COCKPIT PREPARATION - STATUS
TMUFM3301-P01 LEVEL 3
EFFECTIVITY 22-70-00 Page 3
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
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FMGS COCKPIT PREPARATION
INITIALIZATION
INIT page A is obtained by pressing the INIT key on
the MCDU.
The number of the company route is entered onto the
scratchpad of the MCDU by using the alphanumeric
keyboard.
The company route can be defined by up to 10 characters.
In our example, it is KMSPKLGA01 from KMSP to KLGA
(ICAO codes for Mineapolis St Paul and New-York La
Guardia airports).
Once the company route has been inserted, the departure
and destination airports appear on the display
automatically.
Note also, that the ALIGN IRS prompt has appeared.
The flight plan being defined, NAV is armed and
indicated on the Flight Mode Annunciator (FMA) of the
PFD and the LAT light comes on on the FCU.
NOTE: If the pilot wants to insert a route, which does
not belong to the data base, he must give the
origin and destination identifier in the FROM/TO
boxes. He must then build up his route waypoint
by waypoint.
The flight number (FLT NBR) is entered and inserted
by using the alphanumeric keyboard and the appropriate
Line Select Key.
The alignment process is completed by sending the
departure airport coordinates to the Inertial
Reference Systems. This is done by pressing the Line
Select Key adjacent to the ALIGN IRS prompt.
NOTE: The tropopause (TROPO) altitude default value
is 36090 ft, but may be changed if necessary.
TMUFM3301-T02 LEVEL 3
EFFECTIVITY 22-70-00 Page 4
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 220
ALL
FMGS COCKPIT PREPARATION - INITIALIZATION
TMUFM3301-P02 LEVEL 3
EFFECTIVITY 22-70-00 Page 5
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_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 221
ALL
FMGS COCKPIT PREPARATION
INITIALIZATION (CONTINUED)
INIT page B is obtained from INIT page A by pressing
the NEXT PAGE key on the MCDU.
A Zero Fuel Weight (ZFW) of 55 tons is entered and
inserted.
A BLOCK fuel of 10 tons is entered and inserted.
The BLOCK entry initiates a fuel prediction
computation.
TMUFM3301-T03 LEVEL 3
EFFECTIVITY 22-70-00 Page 6
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
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FMGS COCKPIT PREPARATION - INITIALIZATION (CONTINUED)
TMUFM3301-P03 LEVEL 3
EFFECTIVITY 22-70-00 Page 7
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
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ALL
FMGS COCKPIT PREPARATION
RUNWAY CHANGE
The active runway is different from the one included
in the company route. Therefore, the designated origin
runway needs to be changed before inserting the
critical speeds for Take-Off.
The runway included in the company route is 11L and
the active one is 29L.
To change the runway in the flight plan, the F-PLN key
is pressed first on the MCDU.
Flight plan page A is then displayed.
On this page, the Line Select Key, adjacent to the
runway (KMSP11L) contained in the company route, is
pressed.
This selection, called a lateral revision, from the
current runway gives you access to the LAT REV page
at origin.
From it, and by pressing the Line Select Key adjacent
to the DEPARTURE prompt, you get access to the
departure data.
TMUFM3301-T04 LEVEL 3
EFFECTIVITY 22-70-00 Page 8
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
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ALL
TMUFM3301-P04 LEVEL 3
FMGS COCKPIT PREPARATION - RUNWAY CHANGE
EFFECTIVITY 22-70-00 Page 9
 
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