曝光臺 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

flight legs and shows NONE.
INFLIGHT FAULTS Engineering Page
This page shows the A/T system failure information. The
display shows the flight number and the date when the problem
occurred. The faulty LRU shows on the left of the display and the
flight deck effect shows on the right. The diagnostic is under the
flight deck effect. The repeat indicator shows if the problem
occurred more than once during the flight.
Push LSK 6R to see problems on the next flight.
To go back to the A/T BITE main menu, push LSK 6L.
A/T SYSTEM - TRAINING INFORMATION POINT - A/T BITE PAGES - A/T INFLIGHT FAULTS
EFFECTIVITY
SHZ ALL 22-31-00
Page 86
D633A101-SHZ1 Jun 10/2003
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
22-31-00-029
A/T SYSTEM - TRAINING INFORMATION POINT - A/T BITE PAGES - A/T INFLIGHT FAULTS
A/T SYSTEM - TRAINING INFORMATION POINT - A/T BITE PAGES - A/T INFLIGHT FAULTS
EFFECTIVITY
SHZ ALL 22-31-00
Page 87
D633A101-SHZ1 Jun 10/2003
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
22-31-00-029
INTERACTIVE Page
You select the INTERACTIVE page from the A/T BITE TEST
menu when you push LSK 4L. The INTERACTIVE page lets you
do interactive tests that are not in current status test. These
tests are done one at a time and are selectable from a menu.
MODE ANNUNCIATION Page
From the INTERACTIVE page, push LSK 1L to start the MODE
ANNUNCIATION test.
The first page of the MODE ANNUNCIATION test gives you the
initialization instructions. Push the NEXT PAGE key to continue
with the test.
Page 2 shows mode annunciations that you can see on the
common display system. Push the LSK next to the annunciation
to see the display.
Page 3 shows modes you can set but there is no annunciation
on the common display system. You must connect test
equipment to monitor these signals. You push the LSK next to
the annunciation to set the mode.
A/T SYSTEM - TRAINING INFORMATION POINT - A/T BITE PAGES - INTERACTIVE TEST 1
EFFECTIVITY
SHZ ALL 22-31-00
Page 88
D633A101-SHZ1 Jun 10/2003
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
22-31-00-030
A/T SYSTEM - TRAINING INFORMATION POINT - A/T BITE PAGES - INTERACTIVE TEST 1
A/T SYSTEM - TRAINING INFORMATION POINT - A/T BITE PAGES - INTERACTIVE TEST 1
EFFECTIVITY
SHZ ALL 22-31-00
Page 89
D633A101-SHZ1 Jun 10/2003
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
22-31-00-030
INPUT DISCRETES Page
You select the INPUT DISCRETES page from the INTERACTIVE
test menu when you push LSK 2L. The INPUT DISCRETES page
lets you do interactive tests of the discrete inputs.
The first page shows general instructions for the input discretes
page.
Other pages shows the current state of the input discretes.
DISENGAGE/WARNINGS Page
You select the DISENGAGE/WARNINGS test from the
INTERACTIVE test menu when you push LSK 3L. The
DISENGAGE/WARNINGS test lets you do interactive tests of
the disengage/warning circuits.
The first page shows general instructions for the disengage/
warning test.
Other pages shows methods of A/T disengagement and
methods to reset the A/T disengage warning lights.
A/T SYSTEM - TRAINING INFORMATION POINT - A/T BITE PAGES - INTERACTIVE TEST 2
EFFECTIVITY
SHZ ALL 22-31-00
Page 90
D633A101-SHZ1 Jun 10/2003
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
22-31-00-031
A/T SYSTEM - TRAINING INFORMATION POINT - A/T BITE PAGES - INTERACTIVE TEST 2
A/T SYSTEM - TRAINING INFORMATION POINT - A/T BITE PAGES - INTERACTIVE TEST 2
EFFECTIVITY
SHZ ALL 22-31-00
Page 91
D633A101-SHZ1 Jun 10/2006
BOEING PROPRIETARY - Copyright#- Unpublished Work - See title page for details.
737-600/700/800/900 AIRCRAFT MAINTENANCE MANUAL
22-31-00-031
CTM/POR Page
The Cycle Time Monitor/Power On Reset (CTM/POR) is an
internal timing function that enables the A/T computer to reset
itself in case an A/T malfunction is detected. A computer
malfunction that manifests itself as an invalid CTM will cause
the A/T computer to reset and re-initialize, causing it to
disengage so as to power up again. The effect of POR is the
same as starting from power off, but without the need to reset
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737NGAMM2(7)