Bombardier Learjet Horizontal Stabilizer Actuator
There should never be a time during installation, testing, or adjustment when the potentiometer rods on the actuator are adjusted.
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There should never be a time during installation, testing, or adjustment when the potentiometer rods on the actuator are adjusted.
Sulfation of the plates and damaged terminal studs are common warranty claims that can be prevented or lessened by following simple operational and maintenance procedures.
Troubleshooting an autopilot altitude hold INOP squawk involves a complicated decision tree that includes several steps and scenarios. Here are three questions to get started.
Maintaining the integrity of your weather radar antenna is vital for accurate hazard detection and flight safety. From inspecting physical warpage to ensuring correct system strapping, precise maintenance prevents the false returns and signal smearing that can compromise a pilot’s view of the sky.
When valuing an aircraft, you either have complete, consecutive, and original logs or you do not. During a pre-purchase evaluation, the logbook plays a major role, and vague or incomplete statements can be troublesome and delay closing.
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.
TCAS 7.1 is being offered as an upgrade by all of the major TCAS manufacturers and makes two important safety enhancements.
Bombardier has issued a recommended SB 45-56-3 that calls for the inspection of the windshield coupe rails on all Learjet 45 models.
SB 72-0175 changes the compliance date from January 1, 2013, to the next shop visit.
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.