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400W Series 

190-01226-04 Rev. 2 

Instructions for Continued Airworthiness Bell 206B 

Page 7 of 22 

2.3 Control, Operating Information 

See the Pilot’s Guides or the 400W Rotorcraft STC Installation Manual for system operation and self-test 
information. The 400W Rotorcraft STC Installation Manual is listed under the reference documentation in 
paragraph 2.1 of this document, and the Pilot’s Guides are listed in the related documents section of the 
400W Rotorcraft STC Installation Manual.    

2.4 Servicing  Information 

None.  In the event of system failure, troubleshoot the 400W Series unit in accordance with Section 2.6. 

2.5 Periodic Maintenance Instructions 

The 400W Series units are designed to detect internal failure. A thorough self-test is executed 
automatically upon application of power to the units, and built-in test is continuously executed. Detected 
errors are indicated on the equipment via failure annunciations.  

Maintenance of the components installed by this STC is on condition, except as noted in the following 
table. 

Table 1 Periodic Maintenance Inspections 

Item Interval 

Description/Procedure 

400W Series 
Unit 

12 Months 

Conduct a visual inspection (look for signs of wear, deterioration, 
or damage to wires, backshells, or connectors) of the 400W 
Series unit and wiring harnesses to ensure installation integrity: 

1.  Inspect the unit for security of attachment. 
2.  Inspect all knobs and buttons for legibility. 
3.  Inspect condition of wiring, routing and 

attachment/clamping. 

4.  Inspect related antennas for proper sealing and 

attachment. 

5.  Inspect integrity of shield terminations. 
6.  Inspect for signs of corrosion on equipment, racks and it’s 

backplates and rack mounting. 

400W Series 
Mounting Rack 

12 Months

 

Inspect the mounting rack for any signs of excessive wear, 
corrosion, or damage. Check mounting rack corners for cracks. 
Check integrity of connector plate attachment to the back of 
mounting rack. 

400W Series 
Mounting Rack 

Every 2000 
flight hours or 
ten (10) 
years, 
whichever is 
first 

Perform an electrical bonding test: 

1.  Remove 400W Series unit from mounting rack 
2.  Measure the resistance between the mounting rack and a 

nearby exposed portion of aircraft metallic structure and 
verify it is less than 10 milliohms. 

Reinstall the 400W Series unit in the mounting rack 

Avionics 
Cooling Fan 

12 Months 

Conduct a visual inspection (look for signs of wear, deterioration, 
or damage to wire harness and connector) of the cooling fan to 
ensure installation integrity. Inspect for signs of corrosion on 
equipment and mounting brackets. 

Содержание 400W Series

Страница 1: ..._________ Dwg Number 190 01226 04 Rev 2 Garmin International Inc 1200 E 151st Street Olathe Kansas 66062 USA Record of Revision Rev Date Description of Change 1 7 16 10 Initial Release 2 8 11 10 Updat...

Страница 2: ...ol Operating Information 7 2 4 Servicing Information 7 2 5 Periodic Maintenance Instructions 7 2 6 Troubleshooting Information 8 2 7 Removal and Installation Information 19 2 8 Diagrams 20 2 9 Special...

Страница 3: ...t control system When this document is revised refer to Section 2 15 for information on how to gain FAA acceptance or approval and how to notify customers of changes 1 4Permission to Use Certain Docum...

Страница 4: ...m units Definition of Abbreviations See Section 1 5 Precautions None Units of measurement None Referenced publications Garmin 005 00610 03 Rev 1 Equipment List 400W 500W Series Installation Bell 206B...

Страница 5: ...ricted to VFR only including rotorcraft that may not have previously been restricted to VFR To clarify this operation limitation a placard with the text APPROVED FOR DAY NIGHT VFR is required to be in...

Страница 6: ...5 5 GNS 430W Unit Only 5 1 GNS 430W Installed with rack and back plate 011 01060 XX 6 2 GNS 430AW Unit Only 5 1 1 GNS 430AW Installed with rack and back plate 011 01061 XX 6 2 39 7 0 1 2 GCF 3XX 3 Por...

Страница 7: ...for signs of wear deterioration or damage to wires backshells or connectors of the 400W Series unit and wiring harnesses to ensure installation integrity 1 Inspect the unit for security of attachment...

Страница 8: ...isplay a low battery message when replacement is required Once the low battery message is displayed the battery should be replaced within 1 to 2 months If the battery is not replaced and becomes total...

Страница 9: ...nnector P4002 11 and 12 and ground to P4002 21 and 22 The 400W Series unit does not transmit The input voltage is too low Increase input supply voltage to 12VDC 24VDC for 430AW models The sidetone lev...

Страница 10: ...not updating DME Wiring connections are incorrect Check wiring 400W Series unit ARINC 429 output not configured correctly Check ARINC 429 output port setting for port that device is connected to ARIN...

Страница 11: ...ontinued Airworthiness Bell 206B Page 11 of 22 Problem Possible Cause Solution CDI scaling on EFS 40 50 is not correct On EFS 40 50 FMS 1 2 configuration is not set to KLN 90 GPS Reconfigure EFS 40 50...

Страница 12: ...s not solve the problem replace the card Basemap database integrity error The 400W Series unit has detected a failure in the built in basemap land data database Land data does not appear on the Map Pa...

Страница 13: ...sing the switch again to cycle its operation COM transfer key stuck 420W and 430W only The COM flip flop key is stuck in the enabled or pressed state If the message persists contact Garmin technical s...

Страница 14: ...ceiver has failed Operational status of the glideslope receiver is unknown Contact Garmin technical support G S needs service 420W and 430W only The unit has detected a failure in its glideslope recei...

Страница 15: ...OM Move GPS antenna further from the COM antenna Add a 1575 42 MHz notch filter in COM coax Fix or replace the COM Disconnect the ELT antenna coax to check for possible re radiation Low Battery Unit N...

Страница 16: ...the Terrain data card The data is not usable Try reloading the information onto the card If that does not solve the problem replace the card RAIM position warning Although sufficient GPS satellite cov...

Страница 17: ...he information onto the card If that does not solve the problem replace the card VLOC has failed 420W and 430W only The GNC 420 GNS 430W has detected a failure in its VLOC receiver Contact Garmin tech...

Страница 18: ...X 500 Check for proper configuration Check the wiring WX 500 device has failed The WX 500 is reporting a system failure Refer to the WX 500 installation manual for additional troubleshooting informati...

Страница 19: ...he installation configuration and user settings are stored internally in the 400W Series unit and will be lost when the 400W Series is replaced with a new unit Original 400W Series unit is Reinstalled...

Страница 20: ...e cover plate 2 Remove copilot side LH side center console cover plate 3 Disconnect cooling fan electrical connector located under cooling ports on fan 4 Extract the three 3X cooling fan mounting scre...

Страница 21: ...Fasteners FASTENER TYPE AND TORQUE Location see Installation Drawing 6 32 Screw 12 15 inch pounds 8 32 Screw 12 15 inch pounds 10 32 Screw 22 25 inch pounds 400W Unit Mounting Rack X GPS Antenna X Co...

Страница 22: ...mer assistance may be contacted during normal business hours via telephone 913 397 8200 or email from the Garmin web site at www garmin com 2 17 Implementation and Record Keeping Modification of an ro...

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