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ú 03 Page 101
ú Feb 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A04451
A
747-400
FAULT ISOLATION/MAINT MANUAL
TOP OR BOTTOM ATC ANTENNA,
P7 PANEL
ATC CONTROL PANEL, B37
NOT INSTALLED ON THE TOP ANTENNA
Air Traffic Control (ATC) System - Component Location Figure 102 (Sheet 1)
A41685
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A
747-400
FAULT ISOLATION/MAINT MANUAL
RIGHT ATC
TRANSPONDER, B100
(E2-2)
SEE D
TOP OR BOTTOM
ATC ANTENNA
RF TRANSFER
RELAY,
B872 OR B871
(E2-3)
SEE E
FWD
LEFT ATC
TRANSPONDER,
B99 (E2-3)
SEE D
MAIN EQUIPMENT CENTER ACCESS DOOR, 117AL
MAIN EQUIPMENT CENTER C FROM SHT 1
TRANSPONDER PASS LIGHT (GREEN)
TRANSPONDER FAIL LIGHT (RED)
CONTROL PANEL-INPUT FAIL LIGHT (RED)
TOP ANTENNA FAIL LIGHT (RED)
BOTTOM ANTENNA FAIL LIGHT (RED)
ALTITUDE-INPUT FAIL LIGHT (RED)
TEST SWITCH
FWD
TOP OR BOTTOM
LEFT OR RIGHT ATC TRANSPONDER, ATC ANTENNA RF TRANSFER RELAY,
B99 OR B100
B872 OR B871 D
E
Air Traffic Control (ATC) System - Component Location
Figure 102 (Sheet 2)
G33088
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A
747-400 MAINTENANCE MANUAL
ATC SYSTEM - ADJUSTMENT/TEST
____________________________
1. General_______
A. The adjustment test procedure for the Air Traffic Control (ATC) system contains two task. The first task is an operational test. The second task is a system test. The operational test is a fast check of the system. The system test uses a ramp test set to examine the ATC system. To fully examine the ATC system, do the operational test and the system test.
B. Two ATC systems are installed in the airplane. Each ATC system is made of a transponder, two antennas (top and bottom), two RF transfer relays, and a dual ATC control panel.
TASK 34-53-00-715-001
2. ATC System - Operational Test_____________________________
A. General
(1) This test examines the ATC system for correct operation. It uses only the system's BITE functions, and no special test or ground equipment is necessary. The TEST switch on the front panel of the ATC transponder starts the operational test.
B. References
(1)
AMM 24-22-00/201, Manual Control
(2)
AMM 31-61-00/501, Integrated Display System (IDS)
(3)
AMM 32-09-02/201, Air/Ground Relay System
(4)
AMM 34-12-00/501, Air Data Computing (ADC) System
(5)
AMM 34-61-00/501, Flight Management Computer System (FMCS)
(6)
AMM 34-61-02/401, Control Display Unit (CDU)
(7)
AMM 45-10-00/201, Central Maintenance Computer System (CMCS)
C. Access
(1) Location Zones 221 Control Cabin, LH 222 Control Cabin, RH 117/118 Electrical and Main Equipment Center
D. Prepare for the Operational Test.
S 865-002
(1) Make sure these circuit breakers are closed:
(a) P7 Overhead Circuit Breaker Panel
1) 7B10, NAV RADIO ATC L
2) 7B22, NAV RADIO ATC R
3) 7B23, NAV RADIO ATC ANTENNA SW
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