Due to a small number of turbine blade separations related to stress ruptures, Honeywell issued SB TFE731-72-3494 to significantly increase the reliability of the turbine blades and reduce the risk of sudden inflight failures and the maintenance costs associated with them.
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Failure to allow your gyros to fully spool down before moving the aircraft can cause severe damage. This video demonstrates what happens to a gyro when it is moved too soon.
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Rolls Royce issued a recent News Flash about the potential for nuisance T2.5 Faults occurring following engine starts on AE 3007C Series engines on Citation X aircraft.
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It is common for a CRT to experience burn-in caused by the continual bombardment of electrons from the CRT’s guns on one spot of the CRT screen. However, it doesn’t take a huge effort to extend the useful life of a DU-870.
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Recent revisions to the Learjet Replacement Schedule have installed an ultimate life on the MLG Strut Torque Links. Keep reading for the stipulations required for each model of aircraft.
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Removing the leading edges prior to painting an aircraft will prevent a thick line of paint from building up along the tape lines behind those edges.
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Is it normal for outboard slats not to retract fully after winglet installation on a Falcon 900? Keep reading for the answer.
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The light alloy brackets and levers in the center wheel well area and wing rear spar are susceptible to severe corrosion if the protective coating is compromised and remedial action is not taken promptly.
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Don’t overlook inspecting the phenolic bushing in the top mount of the APU exhaust. It is commonly broken or missing.
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Because of our long history and experience with the Falcon aircraft, we know the most commonly exchanged parts and keep an inventory available to meet customer needs.
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