Staying Connected And Informed At Any Altitude With Airtext
To continue conducting business, operators need to stay connected to their contacts on the ground while at any altitude, anywhere in the world. Here is a low-cost alternative.
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To continue conducting business, operators need to stay connected to their contacts on the ground while at any altitude, anywhere in the world. Here is a low-cost alternative.
We urge a thorough inspection of this specific area during all future maintenance, especially as part of a pre-purchase evaluation, to detect and address cracks early.
Not sure why the engine computer light begins to flash after several flights and the only fault you can see is fault code 237, ECTM Buffer Filled? Keep reading to learn more.
Many factors will cause a low or high oil pressure indication on TFE731 engines. One of the more common causes is a faulty Breather Pressurizing Valve (BPV).
The unit requires to be function tested every 1200 hours or 36 Months, whichever occurs first. However, we have often witnessed that these actuators do not make it between function tests.
TCAS 7.1 is being offered as an upgrade by all of the major TCAS manufacturers and makes two important safety enhancements.
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.
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.
Dassault requires that after discharge of a fire bottle, whether by accident or intention, the rubber silicone nipple must be replaced.
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.
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.
Duncan Aviation strongly recommends complying with Service Bulletin 196 or 024 to prevent the potential of severe corrosion of the Group 2 Fuel Tank.
How to troubleshoot both systems when the Flight Director (FD) computer and Autopilot computer are combined into one.
December 31, 2012 is the deadline to replace the rear compressor spool in certain CF34-3A engines.
Six guidelines to assist in prolonging the service life of your business aircraft's maintenance laptop.