曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

3 occurences.
TMUMCDU03-T04 LEVEL 3
EFFECTIVITY 31-00-00 Page 8
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 494
ALL
CFDS SPECIFIC PAGE PRESENTATION - EIS 1 GENERAL/PREVIOUS LEGS REPORT
TMUMCDU03-P04 LEVEL 3
EFFECTIVITY 31-00-00 Page 9
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 495
ALL
CFDS SPECIFIC PAGE PRESENTATION
EIS 1 ENGINES
The DMC connected to the upper ECAM DU monitors primary
parameter indications of both engines (N1, N2, EGT).
N1E1
N1 red line gives the N1 limit depending on the engine
type and equipment.
N1E1 (E1 means engine 1): The DMC stores, in its BITE,
the maximum value reached during the last flight.
N2E1
N2 red line gives the N2 limit depending on the engine
type and equipment.
N2E1 (E1 means engine 1): The DMC stores, in its BITE,
the maximum value reached during the last flight.
EGTE1
EGT red line gives the EGT limit depending on the
engine type and equipment.
EGTE1 (E1 means engine 1): The DMC stores, in its BITE,
the maximum value reached during the last flight.
GENERAL RESET
This key resets the values stored for overlimit
parameters. The reset is also performed automatically
at each take-off.
TMUMCDU03-T05 LEVEL 3
EFFECTIVITY 31-00-00 Page 10
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 496
ALL
CFDS SPECIFIC PAGE PRESENTATION - EIS 1 ENGINES
TMUMCDU03-P05 LEVEL 3
EFFECTIVITY 31-00-00 Page 11
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 497
ALL
CFDS SPECIFIC PAGE PRESENTATION
EIS 1 DUMP BITE MEMORY
The DUMP BITE MEMORY gives a CFDS level 3 information
(Engineering maintenance). When required, the TSM has
to be used for decoding the messages.
INTERNAL FAULTS
INTERNAL FAULTS means faults detected inside the DMC.
A maximum of 3 failures can be recorded for each flight
leg. 27 legs may be stored. NEXT PAGE is used to see
the other legs.
TMUMCDU03-T06 LEVEL 3
EFFECTIVITY 31-00-00 Page 12
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 498
ALL
CFDS SPECIFIC PAGE PRESENTATION - EIS 1 DUMP BITE MEMORY
TMUMCDU03-P06 LEVEL 3
EFFECTIVITY 31-00-00 Page 13
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 499
ALL
CFDS SPECIFIC PAGE PRESENTATION
EIS 1 DUMP BITE MEMORY (Cont’d)
EXTERNAL FAULTS
EXTERNAL FAULTS are the result of no information or
no valid information received by the DMC. 7 failures
can be recorded for each flight leg. 27 legs may be
stored. NEXT PAGE is used to see the other legs.
FAULT ON GROUND
Faults which may occur on ground shall be recorded in
the zone 3 of the BITE memory and will not be
transmitted in plain english language to the CFDIU.
The only access to this zone is by the memory dump. A
maximum of 4 failures can be stored.
FAILURE COUNTER RESET
The FAILURE COUNTER RESET key resets the failure
counters inside DMC 1.
TMUMCDU03-T07 LEVEL 3
EFFECTIVITY 31-00-00 Page 14
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 500
ALL
CFDS SPECIFIC PAGE PRESENTATION - EIS 1 DUMP BITE MEMORY (Cont’d)
TMUMCDU03-P07 LEVEL 3
EFFECTIVITY 31-00-00 Page 15
Nov 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 31 INDICATING/RECORDING SYSTEMS
UF94200
EFFECTIVITY Page 501
ALL
CFDS SPECIFIC PAGE PRESENTATION
EIS 1 TEST
SYSTEM TEST
SYSTEM TEST enables the DMC to operate with the full
fault detection possibilities available in flight.
After selection of this test, the DMC will leave the
MENU mode.
After selecting the START TEST key, the result of this
test can be read by selecting the SYSTEM TEST RESULT
key.
DISPLAY TEST
When DISPLAY TEST is selected, the 3 DUs connected to
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：ATA 31 INDICATING AND RECORDING SYSTEM(67)