One of the aims of LOBO OZ has always been to provide a place for sharing discussions and investigations which Lancair Owners and Builders have experienced. In the linked article, Fred Moreno and Chris Howden outline their method of problem solving a landing gear issue:
Lancair IV VH-YFM has over several years experienced failures to retract the main landing gear after takeoff. Sometimes two green lights would remain illuminated, sometimes only one. Incidents were intermittent and widely separated in time, but began to occur more frequently. In all cases, slowing the aircraft to below 120 knots and recycling the landing gear (select down, then up again) would raise both main landing gear and the trip could be completed.
For those who are interested, they have written in extensive detail about how they approached the whole process – complete with photo and diagrams – Lancair IV Main Landing Gear Investigation.
The article also illustrates how collaboration and discussion on the Lancair Mailing List assisted in the investigation process:
After another occurrence a request for ideas and insights was broadcast on Lancair Mail News which resulted in several notes that others have experienced the same difficulties. The finger of suspicion was pointed to the shuttle valve which could malfunction and block the escape of fluid from MLG cylinders when they move to the retract position. This would explain why both gear would stay extended, but not why one gear would stay extended (green light on) while the other did not (green light off).
In such precision machines, the value of questioning, discussion and sharing of problems and their solutions cannot be underestimated, so we hope this ‘holiday weekend’ reading is valuable to you. Let us know if there is something you too could share.