(d)
Push the LSK adjacent to <CONTINUE.
(e)
Make sure the CDU shows:
~.............
| INTERLOCK |
...............
| L | C | R |
...............
| 0 | 0 | 0 |
2....…....…...1
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(f)
(g)
(h)
(i)
(j)
(k)
(l)
(m)
(n)
(o)
A
747-400
MAINTENANCE MANUAL
Push the LSK adjacent to <CONTINUE
Make sure the CDU shows:
Make sure the CDU shows:
~................
| OPTION GROUP 1 |
..................
| L | C | R |
..................
| 6 | 6 | 6 |
2....…....…......1
Push the LSK adjacent to <CONTINUE.
Make sure the CDU shows:
~................
| OPTION GROUP 2 |
..................
| L | C | R |
..................
| 5 | 5 | 5 |
2.....…....….....1
Push the LSK adjacent to <CONTINUE.
Make sure the CDU shows: ~................ | OPTION GROUP 3 | .................. | L | C | R | .................. | 55| 55| 55 | 2......…...….....1
Push the LSK adjacent to <CONTINUE.Make sure the CDU shows:
~................
| OPTION GROUP 4 |
..................
| L | C | R |
..................
| 2 | 2 | 2 |
2.....…....….....1
Push the LSK adjacent to <CONTINUE.
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A
747-400 MAINTENANCE MANUAL
(p) Make sure the CDU shows:
~................ | PARITY | .................. | L | C | R | .................. | OK| OK | OK | 2....….....….....1
G. Put the Airplane in Its Usual Condition
S 865-217
(1) Remove the electrical power if it is not necessary (AMM 24-22-00/201).
TASK 22-10-00-745-300
13. Ground Test - FCC Instrument____________________________
A. General
(1) This test is for a check of these functions:
(a)
FCC to EIU Interface
(b)
FMC Switching Interface to the FCCs
(c)
Magnetic/True Heading Switch Interface to the FCCs
(d)
Flight Director Source Select Switch inputs to the FCCs.
B. References
(1)
AMM 22-11-01/401, Flight Control Computer
(2)
AMM 24-22-00/201, Manual Control
(3)
AMM 34-12-01/401, Air Data Computer
(4)
AMM 34-21-00/201, Inertial Reference System
(5)
AMM 34-61-00/501, Flight Management Computer System
(6)
AMM 34-61-02/401, Control Display Unit
(7)
AMM 45-10-00/501, Central Maintenance Computer System
C. Access
(1) Location Zones
221 Control Cabin, LH
222 Control Cabin, RH
D. Preconditions
S 865-455
(1) These conditions are necessary for this task:
(a) Electrical Power On (AMM 24-22-00/201).
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A
747-400 MAINTENANCE MANUAL
(b)
Control Display Unit (CDU), serviceable (AMM 34-61-02/401).
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