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tom connor
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NTSB Misses the Point
from tom connor
wrote 3 years 9 weeks ago
I went to the Cessna TAA course on the C-182 Nav III for CAP and then tried to teach it to others under their guidelines. I thought they made it a lot harder than necessary and many pilots said no thanks. Personally, I don't see much difference from a similarly equipped steam gage aircraft. Having said that, there are few similarly equipped steam gage aircraft.
IMHO, a VFR pilot could care less if the panel is glass or steam, in fact for the person who falls in love with the pretty screens I think it is a detriment. But for the IFR pilot, the data fusion, geo-referenced presentation and synthetic vision is worth a lot of peeks out the window. Just as important is the elimination of the vacuum pump and associated instruments, or at least their demotion to second or third string.
I also own an aircraft and installed a JP instruments EDM-800, a Rocky Mountain microencoder and numerous digital engine instruments from Electronics International and use a G-496 for weather and sports. I lust for a Dynon D10 or higher to replace the Micro-encoder so I have a backup to the vacuum driven widgets. The in-flight and post-flight data analysis from the EDM-800 data recording has saved me many an unpleasant surprise, and I am also lusting after the JPI 830/930 so I can record more data and look in one place for it. Therein is the downfall of lots of data at various locations in the cockpit: Either something useful goes undetected or it's a bit busy. Keeping all the balls in the air between setting up a localizer/Glideslope and programming the G-496 for '[situational awareness' can be a handfull, and therein is the beauty of the tight integration in modern glass systems.
The FAA has redesigned almost all Montana ILS approaches by replacing marker beacons/NDBs with DME fixes or named waypoints. Hence a G-430W will soon replace a perfectly good Collins microline com/nav. Tied to the ancient Century I wing leveler with nav tracking I suppose that classifies the plane as TAA. It may not be as pretty as a G1000, but some say I can afford it.
FAA Knowledge Test Failures Skyrocket
from tom connor
wrote 2 years 10 weeks ago
How can anyone be for or against the changes without specifics? Did they change the KT questions to similar but related topics and problems or items unrelated to the topics mandated by the FAA.? It matters. It also matters if the questions are of a complexity unnecessary to that of the license in question or relevant to reality: Does the instrument test still cover the MLS? ADF?
Personally, my opinion of the private and instrument knowledge tests is that they cover darn little regarding how to fly a plane, decision making and the stuff an instructor and evaluator look for in a flight student.
Maybe we should be asking what the KT contributes to student safety and proficiency rather than how to keep a good stick with bad study habits from carrying a license.
Stay Out of the Clouds
from tom connor
wrote 1 year 8 weeks ago
I think that doing a 180 with indvertent IMC is a great way to experience vertigo, graveyard spirals and other dandy experiences best avoided. Instead, GO ON THE GAGES and maintain control. Us the autopilot's wing leveler if available. Then add power to climb above obstacles without touching trim. Once that's done and solidly on the gages then make a 180 or get a clearance.
I have good reason for that recommendation. I've searched for numerous aircraft that crashed in the Montana mountains, and I have a theory that most of them died trying to comply with the rules by scud running into the rocks. That's sad when there's safety in altitude and getting on the gages and wing leveler. Combine that with the reality that MEAs are well above the rock tops and there's a lot of room for the IFR into IMC guy and IFR traffic packing TCAS. Legal? No. Smart? Smarter than dying to stay legal.
New Cessna ADs Surrounded by Suspicion
from tom connor
wrote 51 weeks 4 days ago
Cessna's mandatory what?!? MSEBs and MSBs? For part 91?
What's wrong with ADs? Read this one and you'll see the feds leave themselves access to our checkbooks 'based on reports from the field.' As reported on the CPA and avweb sites, the AD is apparently based on Australian service difficulty reports submitted on aircraft that - like the T-34 Mentor fiasco - weren't used in the usual manner.
Where's the data? the suspect aircraft are unavailable to engineers who might be able to tell the difference between a crack and a stain. If the AD ends up based on one mechanic angry at a C-210 owner, will the FAA retract the AD?
Was an eddy current test done on the subject aircraft to confirm cracks per SEL-57-01, or are we over-reacting to stains? I'd sure like to see some data, pictures or tea leaves that support the AD.
The FAAs arrogance is palpable. Comments from the hoi poloi are welcome but their minds are made up and the AD will be effective 5 June 12 regardless, so why bother?
If you read SEL-57-01, it narrows the inspection to WS 25 and 45 and not the whole wing spar cap. I don't have the C210 repair manual, but I assume this is 25 to 45 inches from aircraft centerline and coincident with the spar fitting ( see SEL-57-01 page 4). Are there enough inspection holes? If not, and this has to be done every 100 hrs, adding more holes would be helpful.
Where are the bodies? C-210s are known for in-flight breakups. Is this a known cause? The C-177 has the same design and AFAIK there has never been an in-flight breakup.
All low wing aircraft have cantilever wings. Why do high-wing Cessnas with that feature get the attention?
New Cessna ADs Surrounded by Suspicion
from tom connor
wrote 51 weeks 1 day ago
ict-cfi suggests we should think of airplanes as cars and consider the miles they cover as a determinant of the age of retirement. How many properly maintained cars have been banned from US roads because they are too old or have too many miles?
The whole concept of age and TBO was abandoned by the airlines and military years ago. http://www.avweb.com/news/savvyaviator/savvy_aviator_45_how_risky_is_going_past_tbo_195241-1.html
A few years ago Richard Collins' last flight in his pampered C-210T was to the dismantler. It would be good to know more about what drove that decision. Oh Dick! http://www.airfactsjournal.com/about/
Corrosion: most engines die today because they rust out, not wear out. Is that true for airframes? I suspect Cessna's real concern is aircraft that fly a few hours and sit on the ramp in hail, rain,snow or salt fog.
Cessna has bumbled thru an 'aging aircraft' presentation to get a few on board. Good for them. But the feds have made zero effort to present their case or get me on board with this AD. That is just arrogance and it pisses me off.
The sad part is that a plane that has been routinely hangared, treated with CorrosionX and rarely mistreated could meet the same fate as a rust bucket that spent 30 years dancing on a tiedown in the wind, rain, hail and snow.
Compliance with 'Emergency Service Bulletins - SBs - is voluntary for part 91 operators. Airworthiness directives - ADs - are mandatory for everyone affected. So perhaps the spar cap issue is an attempt to collect data from the field at owner expense, so I have mixed emotions about it. Data is good. creating a red herring based on no data is not.
Elevating this spar cap SB to an AD without convincing the operators that there is data to support the need is flat wrong but not unheard of: Manufacturers can claim their data 'proprietary.' By doing so the feds can herd us off a cliff without explaining why, but it's still wrong.
Lets look at the T34 mentor in- flight breakups for a clue how this could go and how it should go. The involved aircraft were all used for mock combat. But it threatened to affect thousands that were in no way involved because the T-34 shares many structures with the Beech Bonanza. Avweb's John Deakin wrote a superb article about it in 2005 called "Pelican's Perch #20: Ground all Bonanzas? http://www.avweb.com/news/pelican/182086-1.html.
The salient point John makes is this:
""Why should you care about any of this? True, right now only the T-34s are at risk, but we all need to pay attention -- now! I believe that if events run their course in the current direction, it is very possible that most aircraft in "the Bonanza family" may be subject to another FAA-mandated fiasco that makes the V-Tail crisis of the '80s look tame by comparison. It is possible the entire fleet could be grounded while a "fix" is designed and approved, and that the fix could be so expensive that many Bonanza owners would simply have to junk their airplanes because the fix would be economically disastrous. Others would be burdened with costs in lost time, money, and useful load.
At this point, it is all too easy for the alphabet groups and owner associations to sit back and say, "Well, the investigation isn't complete, and we don't even know what happened, yet, so let's wait and see."
True, the investigation is not complete. The NTSB ain't talking, and the fat lady hasn't sung. But there are some frightening signs that lead me to believe the investigation is badly off track, and may never get back on. Many of the current participants have "mixed motives" at best, and the key players appear to be rushing ahead with a fix that isn't. ""
The similarities between the wing spar cap AD and the T-34 AD are not accidental, and to say 'aw shucks, wouldn't you want to know if your plane has cracks' avoids the real issue, which is this: Now we have the government mandating we collect and submit data to them for further 'decision making.' Cessna should be doing that, not the feds. Cessna has a vested interest in seeing that the fleet survives. The feds clearly have no such concern. That the feds are making this mandatory without sharing data and getting owners/operators on board is simple arrogance. That's the real problem.
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