Planning continues for our Devonport TAS conference being held from 2nd to 4th March 2018.
WE have some exciting announcements as far as guest presenters and speakers. Our program is taking shape along the lines of feedback from members who attended Goolwa.
Devonport is a beautiful part of the world so please come and join us. Save the date now.
If you are planning any sort of Avionics upgrade including ADSB, or an upgrade to IFR, we will cover that. LOBO Oz is pleased to announce that Patrick Coleman, our Australian and New Zealand Sales Manager from Garmin, will be presenting at Devonport. An ideal opportunity to see the Garmin gear first hand and ask questions specific to us here in Oz.
Feedback from Oshkosh and from the joys of fault finding new avionics like the G3X etc. When you ring Garmin Support with your problem, the first question they ask now is: Do you have a fast stack hub installed. If yes they will ask you to call back when the hub is removed.
The McCraken Country Club has now pretty much locked in our catering requirements, we will be well fed and I look forward to a wonderful weekend. If you are planning to attend and have not yet registered please let me know ASAP.
We have organised some good weather, even though Goolwa is starting to get cooler you can see our arrival day is advertised as being “Mostly sunny and pleasant”.
The new AD applies to certain Continental Motors, Inc. including TSIO-550-K, TSIOF-550-K, TSIO-550-C, TSIOF-550-D, and TSIO-550-N reciprocating engines.
Prompted by a report of an un-commanded in-flight engine shutdown, resulting in injuries and significant airplane damage, the AD requires replacing the oil cooler cross fitting assembly. All AD-required action must be completed within 12 months or 100 flight hours after the effective date of Nov 18,2016.
At our Mudgee LOBO Oz Fly-in, one of our attendees drew attention to a couple of Lancair Service Bulletins, and noted that my Legacy had not been modified in accordance with SB023.
I am not certain how I missed it, and given that this SB was dated 1994, I expected it would have been incorporated into the build book.
Please note that this SB023 is applicable to all Lancair models.
The forward rivets have now been replaced with pan head screws and nuts as noted in SB023.
This SB066 is for all of the Lancair IV/ES/and IVPT to ensure the rear access panel on the left side of the rear fuselage is not attached with latches or hinges. The panel is a structural part of the airframe and must be attached using a minimum of -6 screws. Note that new build IVs are now using -8 screws, but there is no requirement to replace existing -6 screws, as used on most of the Lancair IV/ES and IVPT’s that have been flying for some time.
Small things like this is what LOBO Oz is all about.
Learning as a group, we have an amazing pool of expertise and knowledge when it comes to building, flying and maintaining our Lancair aircraft.
Was there something you learnt at our Mudgee fly-in that might need further discussion? Please share.