In my experience as an Avionics Tech Rep, unless I am talking to the person who witnessed the squawk, I go under the assumption that there is always more to the story than what I am told.
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In an FAA Reduced Vertical Separation Minimum (RVSM) Notam dated March 9, 2011, operators of aircraft authorized to use RVSM airspace must conduct monitoring every two years or within 1,000 flight hours per aircraft, whichever period is longer.
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How to troubleshoot both systems when the Flight Director (FD) computer and Autopilot computer are combined into one.
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Due to the report of missing locking clips, Embraer has just released two Service Bulletins that require the inspection of the turnbuckles installed on the control cables throughout certain S/N Embraer Phenom 100/300 model aircraft.
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Duncan Aviation strongly recommends complying with Service Bulletin 196 or 024 to prevent the potential of severe corrosion of the Group 2 Fuel Tank.
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In addition to SB560XL-27-34, Cessna now offers a new pulley for the aft elevator trim cables that will enhance the Flight Control System.
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If you are planning on flying in EASA airspace, there are several important items you need to keep in mind about FANS and Link 2000+.
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The FAA has issued AD 2012-06-03 due to reports that the horizontal stabilizer trim actuator (HSTA) no-back and the number 1 motor brake assembly (MBA) on the Challenger 300 can both fail dormant.
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December 31, 2012 is the deadline to replace the rear compressor spool in certain CF34-3A engines.
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The first step to troubleshooting an inoperable NAV is to identify the NAV source the pilot was using at the time of the failure.
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