Squawk Solution: Learjet 35A Autopilot Disengaging
The autopilot disengaged immediately when the pitch servo tried to drive the elevator.
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The autopilot disengaged immediately when the pitch servo tried to drive the elevator.
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The incorporation of SB 72-5194 will extend to the TFE731-40 and -60 engines to the 3000 hour MPI and 6000 hour CZI intervals. MSP will pay for this bulletin at the next MPI.
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Duncan Aviation technicians have found the V-Band Clamp installed incorrectly on a Falcon 50B and 50EX.
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During the next nose gear strut corrosion inspection, our technicians recommend evaluating the centering torsion spring.
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Learjet has recently discovered the potential for cracks developing in the ballscrew and nut assembly of the Learjet 45 flap actuator.
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There is a new Chapter 5 requirement for the Astra/SPX/G-100 to overhaul the horizontal stabilizer trim actuator at 10 years.
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For intermittent faults from thrust reversers to autopilot and everything in between, don’t overlook a very important part of the system—Weight on Wheels (WOW).
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We recently repaired several Lear 45 MLG actuators suspected of bypassing fluid due to poor performance on the aircraft.
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Our Challenger Tech Reps recommend two new areas for CL600 corrosion inspection.
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I recently ran across an issue with a Pratt & Whitney engine oil leak and felt it would be to everyone’s benefit to clarify my findings.
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