http://www.youtube.com/watch?v=uYAVLfuU ... ed&search=
-istp

Moderators: lilfssister, North Shore, sky's the limit, sepia, Sulako, I WAS Birddog



Correct on some injuries and the cabin mess. The wings were disassembled, closely measured and inspected and re-skinned. But the same tortured fuselage and empennage...Hedley wrote:Holy Crap! You're saying -5G and +10G?! There must have been quite a few serious injuries and an incredible mess in the cabin afterwards.I have flown transport aircraft whos G meters exceed -5-+10 in heavy turbulence
I don't care if it was inspected, I ain't flying in an aircraft who's ultimate G limit has been exceeded. Metal has memory, and someone's going to pay down the road.
I put the AWD reference out there... Did I say anything that you are saying I said?North of You wrote: Then to lend credence to your argument you bring out an example of an AD on an AC with over 17,000 hours on it and say that these cracks in the spar will happen when you do said role. Your day to day operations are far more stressful then what these folks put their AC through on this particular day.
 
 
Are you sure that they do not have a company IFR approach that they are useing? Just a thouhgt.North of You wrote:As I have stated before, rules are broken all of the time in the north on a day to day basis. Example: a very reputable company had a northern destination on it’s sked which had no published approach. Yet the guys routinely flew there every day. Both IFR and VFR, breaking the rules every time they went in, when the weather was below sector.




And the dreaded thought police makes itself heard. What does this have to do with the argument in question? Sounds like the reaction of a person running out of ideas to me. "I'm telling your mommy"!Cat Driver wrote: " However stress paths and loading can be completely different. "
Exactly.
So North of You, if you fly for a company would you want them to read your ideas on how to fly airplanes here on Avcanada?
My point was so obvious that I didn't think I had to spell it out either. So lets try this again. This roll was done in such a way that there was less stress placed on the AC then it would experience on a typical day flying through weather or that hard landing where you leave a trench 6 feet long and deep enough to plant crops in. I am not talking about flying inverted. I am not talking about making a mess out of the roll and either falling out of it and having to pull to hard to pull it back out, or going into positive Gs'. I am not talking about the legalities of this either. I can't, cause if you get caught doing this you have nothing in the CARS that will help you save your job. I am talking about the very nice roll the guys did on this video.
I thought I was dealing with some more experience pilots out here instead I find myself dealing with you people that seem to have a copy of the CARS in the bathroom. Obviously you are all too law abiding and sanctimonious that none of you have ever flown down low on an empty leg back home up north, or flown over gross to get that last bag in. I think this also qualifies for taking the AC outside of it’s certified flight envelope. Or gone bellow minimums on the last leg of the day to places such as YTH. Let alone have naked strumpets walking around the top of the wing. So good luck to all of you, and may I suggest you apply to work for Transport Canada enforcement so you can keep the world safe from dangerous ramp rats such as myself.



Can't recall the last time I heard of a KA/1900 flying along when the wing just fell off...

 
  in that not everybody here is not a highly experienced pilot.  I fall into that category.  Only if you could count run-up time would I probably have close to the hours you have under your belt.
 in that not everybody here is not a highly experienced pilot.  I fall into that category.  Only if you could count run-up time would I probably have close to the hours you have under your belt.   I am sure you have caught on now..but in case others haven't... I am an AME of numerous years experience.
 I am sure you have caught on now..but in case others haven't... I am an AME of numerous years experience.
 
 The FAA received recent reports of cracks found in the wings of two RAC 1900D airplanes. During routine maintenance, the wing rear spar lower caps and rear spar web were found to have significant cracks.
The RAC Structural Inspection Manual requires a thorough inspection of the wing rear spar at 17,500 hours time-in-service (TIS) with repetitive inspections at intervals of 3,000 hours TIS.
One airplane had 19,126 hours TIS when cracks were found. The cracks were in the lower aft spar cap flange, but the cracks extended upward into the web and terminated at the lightening hole in the spar web. Fasteners were also found missing in the spar cap and wing cove splice plate. There were no discrepancies recorded from the initial inspection at 17,500 hours TIS on this airplane.
Early indications show similar cracking on the other airplane. We continue to gather information on this airplane.
Analysis shows that similar cracks could also develop in the wings of the Models 1900 and 1900C airplanes.