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port is below the left instrument panel shelf.
WARNING: DO NOT USE THE GPS WITH AN OUT-OF-DATE DATA BASE. AN
OUT-OF-DATE DATA CAN CAUSE A FLIGHT SAFETY HAZARD.
Refer to the manufacturers Operator’s Handbook provided with the equipment for operating
data. (Bendix\King part number 006-08791-0000).
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Figure 7: KLX 135\135A GPS COMM
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F. Bendix\King KLX 135\135A GPS COMM
Figure 5 shows the KLX 135\135A GPS COMM. The KLX 135\135A is a VHF communications
transceiver and a GPS receiver. Refer to Chapter 23-10 for data about the VHF COMM part of
the equipment.
The avionics bus supplies power to the KLX 135\135A. The GEN/BAT switch and the
AVIONICS MASTER switch must be ON to supply power through the circuit breaker to the
equipment. The DIM/BRIGHT switch (located in the instrument panel) controls the brightness of
the display.
The GPS part of the KLX 135\135A receives signals from an active antenna. The antenna is
located behind the battery box.
The blind altitude encoder provides data to the KLX 135\135A. Refer to Chapter 34-20 for data
about the altitude encoder. You can up-date the KLX 135\135A data base though a data loading
port. The port is below the left instrument panel shelf.
WARNING: DO NOT USE THE GPS WITH AN OUT-OF-DATE DATA BASE. AN
OUT-OF-DATE DATA CAN CAUSE A FLIGHT SAFETY HAZARD.
Refer to the manufacturers Operator’s Handbook provided with the equipment for operating
data. (Bendix\King part number 006-08751-0000 for the KLX 135, 006-08789-0000 for the KLX
135A).
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Figure 8: KT 76A Transponder
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G. Bendix\King KT 76A Transponder
(1) Description
Figure 6 shows the KT 76A Transponder. The KT 76A transponder is a receiver/transmitter.
It transmits transponder code and attitude data to the Air Traffic Control Radar Beacon
System (ATCRBS).
The Transponder replies to interrogation signals from the ATCRBS mode A secondary
surveillance radar (SSR). The reply signal gives the code which can be set on the cockpit
display. A reply lamp comes on when the equipment is transmitting.
The transponder can also give altitude data in reply to mode C interrogation. The
transponder transmits data from the blind encoding altimeter to the ATCRBS. See Chapter
34-20 for data about the blind encoding altimeter.
The transponder has an IDENT button. Push the IDENT button to transmit a special
identification pulse. The IDENT pulse identifies the airplane to the air traffic controller.
(2) Operation
The avionics bus supplies power to the transponder. The GEN/BAT switch and the
AVIONICS MASTER switch must be ON to supply power through the circuit breaker to the
transponder. Turn the function selector switch clockwise from the OFF position to set the
transponder on. There is a 45 second delay after setting the unit ON from OFF to let the
transmitter tube warm-up. The function selector switch has these positions:
− SBY. The transponder receives signals but does not transmit.
− ON. If the transponder receives a mode A interrogation, it transmits the mode A code
set by the code selector knobs. You can set any code between 0000 and 7777.
− ALT. If the transponder receives a mode C interrogation, it transmits the altitude data
from the blind encoder.
− TST. This uses a momentary contact switch to operate the transmitter. The reply
lamp comes on. The reply lamp shows the operator that the unit is transmitting.
The reply lamp also shows that the IDENT button has been pressed. If you press the IDENT
button once, the unit transmits a special identification pulse for each interrogation over the
next 15 to 30 seconds.
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Figure 9: GARMIN GNS430W NAV
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H. GARMIN GNS430W
The GNS430W is a VHF communications transceiver and a GPS receiver (see Figure 9). Refer
to Chapter 23-10 for the COMM functions. It also includes the a TSO’d airborne VOR/Localizer
and Glideslope receivers. It has two removable data cards, one with a Jeppesen database
(inserted in the left-most card slot) and the other the Terrain database (inserted in the right-most
card slot). See Figure 9.
The GNS430W has these controls:
　
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