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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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RADIO NAVIGATION
A radio navigation aids check must be performed on the
RADIO NAV page before departure.
This page is accessed by pressing the RAD NAV key on
the MCDU.
The FMGC has automatically selected the first
encountered VOR/DME for NAV updating purposes, and the
ILS associated with the selected runway for guidance
purposes.
The FMGS cockpit preparation is completed.
TMUFM3301-T08 LEVEL 3
EFFECTIVITY 22-70-00 Page 16
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 232
ALL
FMGS COCKPIT PREPARATION - RADIO NAVIGATION
TMUFM3301-P08 LEVEL 3
EFFECTIVITY 22-70-00 Page 17
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 233
ALL
SELF EXAMINATION
Thrust reduction and acceleration altitudes have:
A - a common default value but may be
modified.
B - a common default value but can not be
modified.
C - no default values and may be modified.
Runway changes should be performed:
A - on the TAKE OFF page.
B - only by re-aligning the Inertial
Reference Systems to the new runway
coordinates.
C - by making a lateral revision from the
currently displayed runway on the flight
plan page.
V2 speed is entered on the:
A - FCU.
B - MCDU TAKE OFF page.
C - MCDU flight plan page.
If no company route exists in the data base for
your flight, what must be done on INIT page A?
A - Insert the LAT and LONG values of your
present position and the identifier in
the TO box.
B - Give the origin and destination
identifiers in the FROM/TO boxes.
C - Insert the origin identifier in the FROM
box and the LAT and LONG values of your
destination.
Pressing the ALIGN IRS Line Select Key on INIT page
A?
A - speeds up the alignment process of the
three Inertial Reference Systems.
B - initializes the alignment process of the
three Inertial Reference Systems.
C - completes the alignment process of the
three Inertial Reference Systems using
the coordinates of the origin airport.
Zero Fuel Weight is entered:
A - on the PERF page.
B - on INIT page A.
C - on INIT page B.
TMUFM3301 LEVEL 3
EFFECTIVITY 22-70-00 Page 18
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 234
ALL
22 - AUTO FLIGHT SYSTEM
22-00-00 FMGS WARNINGS
CONTENTS:
AP Off
Failure of both FDs
A/THR Off
A/THR Limited
Capacity Change
FCU 1 (or 2) Fault, FCU 1 and 2 Fault
MCDU Failure
Altitude Alert
Decision Height (DH)
Autoland
TMUFGCN01 LEVEL 1
EFFECTIVITY 22-00-00 Page 1
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 235
ALL
FMGS WARNINGS
TMUFGCN01-P01 LEVEL 1
EFFECTIVITY 22-00-00 Page 2
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 236
ALL
THIS PAGE INTENTIONALLY LEFT BLANK
TMUFGCN01 LEVEL 1
EFFECTIVITY 22-00-00 Page 3
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 237
ALL
FMGS WARNINGS
ALTITUDE ALERT
The altitude alert takes into account the difference
between the aircraft altitude and the reference
altitude selected on the FCU.
It has an effect on the altitude window of the PFD and
can trigger the C-chord aural warning.
Altitude alert is inhibited by glide slope capture.
Altitude alert is cancelled by turning the FCU altitude
knob, or by setting the landing gear lever to DOWN
with slats extended or when the landing gear is
downlocked.
DECISION HEIGHT (DH)
This warning corresponds to an audio call out by a
synthetic voice, depending on the aircraft radio
altitude and the Decision Height (DH).
X is equal to 15ft if DH is greater or equal to 90ft.
X is equal to 5ft if DH is less than 90ft.
"HUNDRED ABOVE" and/or "MINIMUM" warnings can be
inhibited by pin programming.
TMUFGCN01-T02 LEVEL 1
EFFECTIVITY 22-00-00 Page 4
Oct 31/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
 
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