![]() The electronics unit was also accompanied by an FAA Form 8130-3, Airworthiness Approval Tag, also dated. Unit passes all ATE tests and is operating within normal limits. Confirmed all applicable hardware modifications are installed. Master cleared unit to restore all factory default settings. ![]() Updated software to the latest version and aligned unit to optimum performance. Replaced memory battery to correct non-related issue found while testing. Replaced snap dome to correct the return issue. ![]() The following excerpt from the Garmin factory work order, dated, summarizes the refurbishment effort performed: Following refurbishment, this unit was retained as the spare and never subsequently reinstalled into an aircraft. The defective unit was removed from the aircraft, replaced with a spare unit, and subsequently sent to Garmin’s Olathe Kansas facility for factory refurbishment. At approximately 1,200 hours aircraft TTAE, the “CLR” and “ENT” buttons on the GNS430 began to fail intermittently. This particular Garmin GNS340 (S/N: 97119850) was installed in an aircraft as original factory equipment. The standard GNS 430 features a 10-watt comm as well as navigational capabilities. The GNS 430 leads the industry with multitasking, integrated avionics. ![]()
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