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Landing gear issue
Update on the landing Gear issue:
A thorough review of all components of the landing gear system has been completed. This inspection included the following: • Examination of all landing gear Up and Down indicator switches. • Examination of all landing gear circuits including power pack and gear/stall warning circuits. • Thorough inspection of the landing gear mechanical systems. o Up locks. o Down locks. o Push rods. o Hydraulic cylinders. o Hydraulic hoses and connections. o Power Pack. o Power Pack solenoid. o Gear control handle and linkage. o Hydraulic fluid. • The plane was jacked and the gear was: o Retracted using the emergency had pump. o Extended using the emergency had pump. o Gear doors opened and closed (without cycling the gear) using the hand pump as per the POH. o Landing gear was cycled ten (10) times using a hydraulic slave pump. o Landing gear retraction and extension was stopped at various points in the cycle and examination of all of the mechanical and electrical components was performed. Results: • Negative. No detectable anomaly of the gear system was found. Conclusion: • Cause unknown. Possible Causes: • Defective circuit breaker. • It may be possible that the (green) gear down indicator light/gear horn test switch malfunctioned resulting in excess load on the gear indicator circuit tripping the breaker. Subjectively, the gear/stall warning horn sounds much loader than before. Action taken: • Replacement of the gear indicator circuit breaker. • Lubrication of the landing gear system. • All electrical connections tested and verified secure. Any other ideas??? Thanks for your input. It made a big difference in the level of confidence I had approaching this issue. Best to all, Mark |