Honeywell RNZ-850/851 AD Deadline Approaching
November 3, 2012, is the date that operators are required to be in compliance of AD 2010-07-02. It addresses possible erroneous glide slope or localizer display indications.
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November 3, 2012, is the date that operators are required to be in compliance of AD 2010-07-02. It addresses possible erroneous glide slope or localizer display indications.
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TCAS 7.1 is being offered as an upgrade by all of the major TCAS manufacturers and makes two important safety enhancements.
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It was determined that the epoxy ramp installed to prevent water accumulation could deteriorate with time. A dry ice blasting machine removes the epoxy ramp efficiently without collateral damage.
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Now, through a Securaplane STC, Citation 500, 550 and 560 operators are able to enjoy the benefits of the thin plate, pure lead (TPPL) technology that improves discharge and recharge capacity.
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Bombardier has issued a recommended SB 45-56-3 that calls for the inspection of the windshield coupe rails on all Learjet 45 models.
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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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Dassault requires that after discharge of a fire bottle, whether by accident or intention, the rubber silicone nipple must be replaced.
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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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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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How to troubleshoot both systems when the Flight Director (FD) computer and Autopilot computer are combined into one.
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Because of the high probability of future corrosion around the fasteners of the front center panel ahead of frame 10, Duncan Aviation strongly recommends to comply with SB 392.
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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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Six guidelines to assist in prolonging the service life of your business aircraft's maintenance laptop.
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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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The wiring harnesses for nose wheel anti-skid transducers are known to break down internally which can cause intermittent anti-skid issues.
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