K89529
Selcal System Component Location 5C8
23-28-0 Figure 1 Jun 20/85
Page 2
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.
D. With the decoder relay energized, three sets of contacts are actuated. One set causes the relay to latch closed as described. A second set of contacts applies power to an oscillator relay circuit. The third set of contacts complete power to the selcal indicator light on the selcal control panel. The oscillator relay receives power through the decoder relay and thus becomes energized. When energized, two sets of contacts are operated. One set closes a circuit to the selcal system chime. The second set of contacts grounds the capacitor and transistor oscillator circuit connected to the relay coil. Since the relay is in a time delay circuit, it will remain closed momentarily and then open. After it opens, the capacitor will charge and the relay coil will again receive power. The close-open cycle will repeat until the decoder is reset.
E. A reset circuit is completed whenever the toggle switch on the selcal panel is held to RESET. When the reset circuit is operated, power to the decoder relay is grounded causing the decoder relay to open. When the decoder relay opens, the oscillator relay is de-energized and the system is reset.
4. Aural Warning Unit
A. An electrical chime is in the aural warning unit with other aural warning components. The chime will emit a two-tone signal each time the oscillator relay of a decoder unit closes. The chime is connected in parallel with decoder unit No. 1 and decoder unit No. 2 oscillator relays; therefore, it will operate whenever either decoder unit receives the proper tone combination through the respective VHF communication receiver (Ref Chapter 31, Aural Warning and Call Devices).
5. Operation
A. Operation of the selcal systems is dependent upon the fact that each airplane is assigned a particular four-tone audio combination for identification purposes. A decoder is installed in the airplane to detect only the identification tones assigned to the airplane. Whenever a ground station attempts to communicate with a particular aircraft on VHF, they will transmit the proper identification tone combination for that airplane. Provided the proper frequency is selected on the HF or VHF system for the area in which the pilots expect to receive communications, the airplane selcal decoder will detect the tones and operate a chime and a green selcal alert light to indicate to the crewmembers that communication on VHF is desired from a ground station.
B. The selcal system may be reset by pressing the RESET button located on the Selcal control panel. The selcal light will then go out and the chimes will stop.
5C8
Jun 20/85 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 23-28-0 Page 3
EFFECTIVITY
Selcal System Schematic 5C8
23-28-0 Figure 2 (Sheet 1) Jun 20/85
Page 4
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.
EFFECTIVITY
5C8 Selcal System Schematic
Jun 20/88 Figure 2 (Sheet 2) 23-28-0
Page 5
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.
EFFECTIVITY
GJ ALL EXCEPT B-2501 thru
B-2503, B-2509 thru
B-2510, and B-2524
Selcal System Schematic 5C8
23-28-0 Figure 2 (Sheet 3) Jun 20/88
Page 6
SELCAL SYSTEM - TROUBLE SHOOTING
1. General
A. Since both SELCAL decoder units are housed in a single case, failure of either SELCAL system requires the entire decoder to be replaced in electronic equipment rack E2. The SELCAL tones may be monitored with the flight interphone system headphones and associated HF and VHF systems to verify whether the decoder is receiving the tones. The SELCAL indicator light comes on and the chime sounds when a SELCAL transmission is received. If the chime sounds but the light does not come on, replace the control panel. If the light comes on but the chime does not sound, replace the aural warning unit. If the light does not come on and the chime does not sound when SELCAL tones are received, replace the decoder.
5C8
Jun 20/85 23-28-0 Page 101
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.
SELCAL SYSTEM - ADJUSTMENT/TEST
1. Test Selcal System
A. General
(1)
The following test is in tended to check for proper operation of the selcal decoders and connected lights and chime whenever a coded signal is received over the respective HF or VHF system.
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