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.
Recently, Dassault Aviation released several service bulletins and Falcon Service Advisories announcing the installation of ‘wing tank modifications’ for all of the Falcon 50/900/2000 series aircraft.
Hawker 800 series aircraft equipped with SPZ-8000 were required to designate an RVSM critical zone forward of the static ports. This included the nose avionics bay doors.
Communiqué #HK-0017 advises service centers and owner/operators of an information only kit, part number 238-0002, being made available to replace portable fire extinguishers.
Avoid unexpected scheduling and planning headaches by remembering to replace the Lear 40 Series Aft Quadrant at its 10 Year Life Limit.
When you are considering upgrading the MFD to a later model, keep in mind the effect that modification will have on the aircraft’s type certification.
Don't let your engines end up on the DERB list! Some operators are experiencing the unfortunate effects of long-term storage when proper engine preservation procedures have not been followed.
If you have not completed PW SB 26243R2, then P&W recommends Part A of the SB be completed at the next convenient opportunity.
At Duncan Aviation, we have recently come across a number of Temperature Control Valves or Low Limit Control Valves on Challenger aircraft with cracked housings.
The wing leading edge upper removable panels on Falcon 50, 900 and 2000s are installed with differing length screws depending on location.
We recently serviced a Hawker 900XP experiencing recurring hydraulic pressure and a hydraulic overheat issue that could not be readily duplicated on the ground.