FIKI

Flew myself and 2 coworkers to Chicago yesterday for a business meeting. Weather at 6am had icing forecast for 60 miles along our direct route of flight. We were flying a FIKI airplane and departed due south so that we could get out of the area of clouds in closer to 15-20 miles. Airliners that departed ahead of us had no pireps for ice and it turned out that the clouds were only 2,000 feet thick, clear sunny skies above and no ice.

For our flight home, we had to stop in the upper penninsula of Michigan to drop off one of the guys. Picked up a trace of ice, but it was mostly just light snow showers. Departed for Duluth and again just light snow showers and no ice enroute until we descended through about 2,000 feet of clouds in Duluth and we picked up some ice. Weather below was clear and made an uneventful landing.

It was my first icing experience in a FIKI airplane, and a trip I could not have made otherwise. Despite having been part of the FIKI certification program, I have not had much opportunity to fly one. It worked as expected, and I was happy to have it.
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Amsafe Inflater Replacement Time

We recently released Service Advisory SA12-01 that clarifies the inflator assembly replacement interval for the Amsafe inflatable air bags. The replacement interval for the inflators has been increased from 7 years to 10 years. The electronic module assembly remained unchanged and must be refurbished at 7 years and replaced at 14 years.
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Alt 2 Winter Update

Recently looking back, I noticed that I haven't updated the blog about our Alt 2's since this post in October.

As I mentioned in that post, In late 2010, the alternator vendor made several changes. Those were all implemented in the 'k' (2011) date code alternators. Those alternators hit our factory floor and field replacements in the march time frame.

About a month ago, we went through the data, and to date we have had 3 failures of these new 'k' alternators. The picture shown is a graph of serial number versus hours for the SR22 (SR22T is graphed separately). The vertical line on the graph shows where the new alternators were implemented into the line.

This is a VAST improvement over previous model years, and reason for continued optimism that we might be on to a solution.

As I also mentioned in that post, there are 2 additional improvements coming. The new rotor bonding process is now online and those parts are now being produced. The new diode is scheduled to be in place in a couple of months. We will continue to monitor the reliability of these parts, and keep you updated.
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Tires and Tubes Cont.

Over the past few years we have received reports of tires going flat. The reports are sporatic with seemingly no common theme. I blogged about it back in this June 2010 post. We have been working with Goodyear to try to understand what might be causing this, and have tried some of their new tires.


More explanation has come from the FAA via a revision to a Special Airworthiness Information Bulletin (SAIB) published today. CE-11-47R1 explains how Goodyear has been working with different compounds to try and eliminate the various tube failures they have seen in cold and warm weather. Cirrus continues to be active in discussions with Goodyear and help in any way we can.



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"Orbits" Part 2

In my previous post I described some of the technical hurdles we encountered during the development and certification of the Garmin GSR56 Iridium Transceiver. The story continues with the new Garmin GMA350 audio panel. We had been evaluating some prototypes of this new audio panel and wanted to put it into production, but we also wanted to be able to offer a GSR56 Iridium transciever retrofit kit for existing users to install in their airplanes that have the existing GMA347 audio panel. This meant we had to test the Iridium system with both the existing GMA347 audio panel and the new GMA350 audio panel.


What this means for us is that we had to install and test this in an airplane twice. The wiring for the two audio panels is completely different which complicates things. We had to take one of our experimental airplanes which has the GMA347 audio panel and  install the Iridium box and associated structural modifications, hardware and new antenna. We then did all the testing with that version of the installation. Then we took out the old audio panel, rewired the airplane for the new audio panel and repeated all the testing for that installation.

Software is another area where people tend to think it is an easy change, but we spend a lot of time doing enough testing, in many different conditions and scenarios, to ensure that there are no bugs in the software. This involves not only on-aircraft testing, but also installing it in a "bench" installation in our lab. We can simulate a lot of different warnings and other scenarios on the bench before actually doing the flight testing.


But real world results come from the extensive ground and flight testing we do. Every flight test program ends up with some interesting stories and this project is no different. One interesting bug we discovered was that a phone call would not terminate when you clicked hang-up on the aircraft but the guy on the other end of the phone didn't hang up (like when dialing into your voice mail.) This has since been fixed.

Another instance occurred when we were proofing out the voice service. From the ground we called the test aircraft and the guy talking from the plane then sat through a 45 minute teleconference. What we didn't know was that when we dialed the aircraft from our land line it was being considered an international call by our company phone service which racked up quite a charge. Oops.


So after all this testing we finally got a solution that we were happy with and began the process of creating all the various drawings (wire harnesses, installations, structural changes etc), and summarized all of our testing through plans and their test reports, along with a couple of certification reports and submitted that to the FAA.

While that was going on, we sent an airplane down the production line to act as a "pilot build" aircraft. We use this aircraft to proof out our drawings, any new processes, parts and installations. It also provides a chance to give the factory technicians training if necessary. We then feed back any information we learn to correct drawings or re-orient the line flow prior to the need to build these airplanes at rate.

With all of that complete, and final approval from the FAA we are able to confidently move forward with production knowing that there will be a few minor changes needed but overall production will proceed smoothly.
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Child Safety and the NTSB

We are quite honored that Debbie Hersman, the Chairwoman of the NTSB took note of our new LATCH system installation in the 2012 model rear seats by writing about it in her official blog called the NTSB Safety Compass.

We pride ourselves, and work very hard to make our airplanes as safe as possible, this new rear seat is just another step in our always ongoing process of continous improvement.

http://safetycompass.wordpress.com/2012/01/20/improving-child-safety-on-airplanes-one-seat-at-a-time/
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Perspective Global Connect Retrofit

We have received a lot of inquiries about whether the GSR56 Iridium transceiver will be retrofittable for existing Perspective airplanes and the answer is yes. The engineering team is working on the retrofit kit that would go out to the field. It is not a simple installation as there are structural modifications to the CAPS bulkhead and wiring harness changes, and installations of racks and antennas. These changes are quite different than the changes we make for production.

For example there are things we can do to the bulkhead during the initial lay up of the part like add hard points that cant be as easily done in the field or at least not in the same way. So it requires developing special instructions, and parts to complete the retrofit properly.

My intention is to have that kit available for the field in the first half of 2012.
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