(7)
GROUND REPORT After the key 5R has been pushed the page DMCx GROUND REPORT is presented to show all the internal faults of class 1, 2 or 3 recorded on ground during the last leg. (Ref. Fig. 013) No fault has been recorded (Ref. Fig. 014) some faults have been recorded and trouble shooting data of a given fault
(8)
GROUND SCANNING After the key 4L has been pushed the page DMCx GROUND SCANNING presented to show all the internal and external faults of class 1, 2 or 3 as soon as they occur. (Ref. Fig. 015)
(A)
No fault has been recorded
(B)
= some faults have been recorded
(Ref. Fig. 016)
Several pages may be necessary to display all the faults (2 per
page).
(Ref. Fig. 017)
The trouble shooting data of a given fault is displayed by pressing
the related key.
R 1EFF : 106-149, 303-399, 401-499, 1 31-69-00Page 24 1 1 Aug 01/05 1 1 1CES 1
Last leg class 3 fault
Figure 011
R 1EFF : 106-149, 303-399, 401-499, 1 31-69-00Page 25 1 1 Aug 01/05 1 1 1CES 1
Last leg class 3 fault
Figure 012
R 1EFF : 106-149, 303-399, 401-499, 1 31-69-00Page 26 1 1 Aug 01/05 1 1 1CES 1
Ground report Figure 013
R 1EFF : 1 1 1CES 106-149, 303-399, 401-499, 1 111 31-69-00 Page 27 Aug 01/05
Ground report Figure 014
R 1EFF : 1 1 1CES 106-149, 303-399, 401-499, 1 111 31-69-00 Page 28 Aug 01/05
Ground scanning Figure 015
R 1EFF : 1 1 1CES 106-149, 303-399, 401-499, 1 111 31-69-00 Page 29 Aug 01/05
Ground scanning Figure 016
R 1EFF : 1 1 1CES 106-149, 303-399, 401-499, 1 111 31-69-00 Page 30 Aug 01/05
Ground scanning Figure 017
R 1EFF : 1 1 1CES 106-149, 303-399, 401-499, 1 111 31-69-00 Page 31 Aug 01/05
(9) SYSTEM TEST After the key 2R has been pushed the page DMCx SYSTEM TEST is presented. This test, which allows to find out an EIS system misbehaviour needs some action from the operator to initialize the test. These actions are described on two pages under the subtitle "INITIAL CONDITIONS" (Ref. Fig. 018)
(A)
= first page of initial conditions
(B)
= second page of initial conditions
On this second page the key 5L is used to start the test which do not
require any action from the operator, at this stage.
(Ref. Fig. 019)
Display (C) = the test is in progress
Display (E) and (F)
This is the step 1 = the operator is asked to check that a colour
pattern is displayed on the DUs driven by the DMC1 and to press the
key 4L when the patterns are correct.
(Ref. Fig. 020)
Display (G) and (H)
This is the step 2 = the operator is asked to check that a black and
white pattern is displayed on the DUs driven by the DMC1 and to press
the key 4L when the patterns are correct.
Display (J) and (K)
This is the step 3 = the operator is asked to check that a black and
white pattern is displayed on the DUs driven by the DMC1 and to press
the key 4L when the patterns are correct.
(Ref. Fig. 021)
Display (L)
This is the step 1 for the DMC2: the operator is asked to check that
a coloured pattern is displayed on the DUs driven by the DMC2 and to
press the key 4L when the patterns are correct.
Display (M)
This is the step 2 for the DMC2: the operator is asked to check that
a black and white pattern is displayed on the DUs driven by the DMC2
and to press the key 4L when the patterns are correct.
Display (N)
This is the step 3 = the operator is asked to check that a black and
white pattern is displayed on the DUs driven by the DMC1 and to press
the key 4L when the patterns are correct.
Display (P)
This page is displayed when the operator pressed another key: 4R or
5L or 5R during step 1, 2 or 3. The related trouble shooting data is
then displayed on display (Q) after the key in front the fault has
been pressed.
(Ref. Fig. 022)
When the operator, only pressed the 4L key the result is TEST OK like
on display (R).
R 1EFF : 106-149, 303-399, 401-499, 1 31-69-00Page 32 1 1 Aug 01/05 1 1 1CES 1
System test Figure 018
R 1EFF : 1 1 1CES 106-149, 303-399, 401-499, 1 111 31-69-00 Page 33 Aug 01/05
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM 指示/记录系统 8(175)
