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connectors of the unit.
B. Install the Bendix\King KLX 135/135A GPS COMM
Detail Steps/Work Items Key Items
(1) Remove the protective covers from the
connectors on the rear of the unit.
(2) Slide the unit into the rack. Engage the
locking screw so that the latch front lobe
touches the rack.
Refer to Figure 3
(3) Turn the locking screw clockwise so that the
rear lobe engages the mounting rack.
CAUTION: DO NOT OVER-TIGHTEN THE LOCKING SCREW. YOU CAN
DAMAGE THE LOCKING MECHANISM.
(4) Continue to turn the screw until the unit is
fully installed in the mounting rack.
(5) Close the GPS COMM circuit-breaker.
(6) Do a function test. See below.
Communications
DA20-C1 AMM
Page 204
19 Dec 1997 23-10-00 Doc # DA201-C1
Rev. 0
C. Adjustment/Test KLX 135/135A GPS COMM
If possible, do an operational flight check after the radio has been replaced. Alternatively, use a
NAV COMM test set to make sure that the system operates correctly. Refer to the Bendix\King
Installation manual #006-10500-0003 for performance specifications.
Refer to the Bendix\King Pilot’s Guide (#006-08751-0000 for the KLX 135, #006-08789-0000 for
the KLX 135A) which gives start-up and operating procedures.
WARNING: DO NOT OPERATE THE GPS USING AN OUT-OF-DATE DATA BASE.
OUT-OF-DATE DATA CAN CAUSE A FLIGHT SAFETY HAZARD.
Detail Steps/Work Items Key Items
(1) Do a test of each control function. See this Chapter and chapter 34-50.
(2) Make sure that the data base is date valid.
(3) Move the airplane clear of buildings and
ground equipment.
(4) Bring the unit to the NAV READY status. If the unit does not reach NAV READY
status in 5 minutes, refer to the
Bendix\King Pilot’s Guide section 3.6:
Initialization and Time to First Fix.
(5) At a sufficient altitude, contact a ground
station at least 50 miles away and another
close by.
If possible use frequencies at both the low
and high ends of the VHF band.
D. Data Base Loading
You load the data base with an IBM compatible lap-top computer with a 3.5 in disk drive and an
open COM1 or COM 2 port. Use interface kit Bendix\King part number 050-03213-0000.
Detail Steps/Work Items Key Items
(1) Connect the PC to the data loading port
below the left instrument panel.
(2) Set the KLX 135/135A to the SET 0 page.
(3) Put the diskette in the PC.
(4) Cycle the power of the PC. Follow the menu
instructions.
DA20-C1 AMM
Communications
Doc # DA201-C1
Rev. 15 23-10-00 Page 205
30 Apr 2009
4. Remove Install the Garmin GNS430W
A. Remove the Garmin GNS430W
Detail Steps/Work Items Key Items
(1) Open the related GPS COMM circuitbreaker.
(2) Put a 3/32 allen wrench into the access hole
for the locking screw. Engage the screw.
See Figure 4
(3) Turn the screw counter-clockwise until the
unit disengages from the mounting rack.
CAUTION: DO NOT PULL ON THE KNOBS. DO NOT PRY THE FACE-PLATE.
YOU CAN DAMAGE THE UNIT.
CAUTION: DO NOT TOUCH THE CONNECTOR CARD AT THE REAR OF THE
UNIT. THE ELECTROSTATIC CHARGE ON YOUR BODY CAN
DAMAGE THE UNIT.
(4) Pull gently on the sides of the unit to remove
it from the mounting rack.
(5) Install the protective covers on the rear
connectors of the unit.
B. Install the Garmin GNS430W
Detail Steps/Work Items Key Items
(1) Remove the protective covers from the rear
connectors on the unit.
(2) Slide the unit into the rack. Engage the
locking screw so that the latch front lobe
touches the rack.
See Figure 4
(3) Turn the locking screw clockwise so that the
rear lobe engages the mounting rack.
CAUTION: DO NOT OVER-TIGHTEN THE LOCKING SCREW. YOU CAN
DAMAGE THE LOCKING MECHANISM.
(4) Continue to turn the screw until the unit is
fully installed in the mounting rack.
(5) Close the GPS COMM circuit-breaker.
(6) Do a functional test. See paragraph C.
Communications
DA20-C1 AMM
Page 206
30 Apr 2009 23-10-00 Doc # DA201-C1
Rev. 15
C. Garmin GNS430W Adjustment/Test
If possible, do an operational flight check after the radio has been replaced. Alternatively, use a
GPS COMM test set to make sure that the system operates correctly. Refer to the GNS430W
installation manual for performance specifications.
WARNING: DO NOT OPERATE THE GPS USING AN OUT-OF-DATE DATABASE.
OUT-OF-DATEDATA CAN CAUSE A FLIGHT SAFETY HAZARD.
Detail Steps/Work Items Key Items
(1) Do a test of each control function. Refer to Chapter 34-50.
(2) Make sure that the database date is valid. Once the database has been
acknowledged, the instrument panel selftest
　
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