曝光臺(tái) 注意防騙 網(wǎng)曝天貓店富美金盛家居專(zhuān)營(yíng)店坑蒙拐騙欺詐消費(fèi)者

TMUFGCJ02-T03 LEVEL 3
EFFECTIVITY 22-00-00 Page 8
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 280
ALL
AUTO FLIGHT SYSTEM COMPONENTS - MULTIPURPOSE CONTROL AND DISPLAY UNITS (MCDUs)
TMUFGCJ02-P03 LEVEL 3
EFFECTIVITY 22-00-00 Page 9
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 281
ALL
AUTO FLIGHT SYSTEM COMPONENTS
FAC PUSHBUTTON SWITCHES
IDENTIFICATION
FIN: 12CC1, 12CC2
LOCATION
ZONE:
23VU (12CC1), 24VU (12CC2)
COMPONENT DESCRIPTION
The FAC pushbutton switch monitors the status of the
computer in a general way.
The FAULT indication comes on when a failure occurs
affecting the normal operation of the different FAC
functions.
The FAC pushbutton switch, when used, either disables
the related FAC operations (OFF light on - pressed
out) or enables the reset of the computer if pressed
in again (OFF light off).
TMUFGCJ02-T04 LEVEL 3
EFFECTIVITY 22-00-00 Page 10
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 282
ALL
AUTO FLIGHT SYSTEM COMPONENTS - FAC PUSHBUTTON SWITCHES
TMUFGCJ02-P04 LEVEL 3
EFFECTIVITY 22-00-00 Page 11
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 283
ALL
THIS PAGE LEFT BLANK INTENTIONALLY
TMUFGCJ02 LEVEL 3
EFFECTIVITY 22-00-00 Page 12
Jul 31/00
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 284
ALL
22 - AUTO FLIGHT SYSTEM
22-00-00 CFDS SPECIFIC PAGE PRESENTATION
CONTENT:
Nota
Last Leg Report
Previous Legs Report
Trouble Shooting Data
Ground Scan
Windshear Test
TMUAFPG02 LEVEL 3
EFFECTIVITY 22-00-00 Page 1
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 285
ALL
CFDS SPECIFIC PAGE PRESENTATION
NOTA
- LRU ident is not a specific option.Refer to
ATA chapter 31 ("CFDS Reports").
- AFS TEST and LAND TEST functions are
respectively described in dedicated modules
("Operational test of the AFS and Operational
test of the LAND CAT III capability").
LAST LEG REPORT
The philosophy of the LAST LEG REPORT is the same as
the one described in ATA chapter 31 ("CFDS REPORT"),
but additional information is presented:
- FAIL NO : Number of presented fault. This
counter is reset at the start of each flight.
- OCCURENCE : Number of times the same failure
occurs within the same flight.
- ISSUED BY : Designates the computer which
detected the fault. By selecting this function
you have access to the primary data of the
analysis (TROUBLE SHOOTING DATA page).The
information presented on this page is the same
as that accessible by selecting the TROUBLE
SHOOTING DATA function from the AFS MAIN MENU
page.
NOTE: The last fault presented occured first during
the last flight (FAIL NO 01).
TMUAFPG02-T01 LEVEL 3
EFFECTIVITY 22-00-00 Page 2
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 286
ALL
CFDS SPECIFIC PAGE PRESENTATION
TMUAFPG02-P01 LEVEL 3
EFFECTIVITY 22-00-00 Page 3
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 22 AUTO FLIGHT SYSTEM
UF94200
EFFECTIVITY Page 287
ALL
CFDS SPECIFIC PAGE PRESENTATION
PREVIOUS LEGS REPORT
The philosophy of the PREVIOUS LEGS REPORT is the same
as the one described in ATA chapter 31 ("CFDS REPORT"),
and additional information presented is identical to
that presented in the LAST LEG REPORT.
TROUBLE SHOOTING DATA
From the AFS/TROUBLE SHOOTING BITE SELECTION page
generated by the Fault Isolation and Detection System
(FIDS) you can select the BITE that you wish to examine.
NOTE:
- FAC: Flight Augmentation Computer.
- FG: Flight Guidance.
- FM: Flight Management.
- COM: Command side.
- MON: Monitor side.
When the BITE has been selected, the Fault Isolation
　
中國(guó)航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：ATA 22 AUTO FLIGHT SYSTEM(48)