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Piper Meridian Review

Last post 06-14-2008, 11:10 AM by TPGUY. 14 replies.
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  •  01-30-2008, 11:29 AM 397

    Piper Meridian Review

    I recently posted a review of the new Piper Meridian on the blog section.  If you have comments or want to discuss the review please do so here.
  •  01-31-2008, 2:48 PM 416 in reply to 397

    Re: Piper Meridian Review

    Joe:  A good review.  I fly a 2001 Meridian and really enjoy the plane.  It has a couple of short comings that should be known:

    The real world range is 800 miles- you need at least 200 lbs of reserve, even in good weather.  I has 380 lbs predicted at my destination, which used the ASOS of a field 12 miles away.  All through my flight the ASOS showed 12,000' ceilings.  I flew the approach and had to execute a miss due to local fog.  I diverted to a field 20 miles away which was clear and landed with only 170 lbs- turbines really burn fuel down low!

    The P&W engine has a magnesium cast inlet housing. My aircraft was kept by San Francisco Bay for 7 years and corrosion was discovered in the inlet while Sun Aviation was replacing the engine mount under a warrenty program.  Several other engines have been found to have this problem by Sun and I was told that Beachcraft had the same problems in King Airs and changed to an aluminum casting.

    A great flying plane but with limited range and payload.

    Turboprop_Pilot
  •  01-31-2008, 6:24 PM 427 in reply to 397

    Re: Piper Meridian Review

    JoeN:
    I recently posted a review of the new Piper Meridian on the blog section.  If you have comments or want to discuss the review please do so here.


    After a comment on my blog about structural considerations, I did some research on the NTSB accident database with some disturbing results.  I limited my query to PA-46-500TP (Meridian) and excluded the Malibu since there are airframe differences including a larger tail on the Meridian.  There were multiple fatal accidents attributed to in flight structural break ups.  The part that really bothers me though is that there were even more non fatal incidents that resulted in airframe deformation and consequent wing replacements.  In one case it was due to a bird strike, in another it was due to turbulence, and another to an uncommanded autopilot roll.  In my mind, these are not events that should be deforming airframes to a point where they require completely new wing structures.  In addition, there seems to be a trend of incidents involving nose gear collapsing even when the gear down indicator was green.  It is one thing to offer an opinion about the way the airframe feels when flying and compare that with the cold reality of NTSB statistics.
  •  01-31-2008, 6:55 PM 429 in reply to 416

    Re: Piper Meridian Review

    Turboprop_Pilot:
    Joe:  A good review.  I fly a 2001 Meridian and really enjoy the plane.  It has a couple of short comings that should be known:

    The real world range is 800 miles- you need at least 200 lbs of reserve, even in good weather.  I has 380 lbs predicted at my destination, which used the ASOS of a field 12 miles away.  All through my flight the ASOS showed 12,000' ceilings.  I flew the approach and had to execute a miss due to local fog.  I diverted to a field 20 miles away which was clear and landed with only 170 lbs- turbines really burn fuel down low!

    The P&W engine has a magnesium cast inlet housing. My aircraft was kept by San Francisco Bay for 7 years and corrosion was discovered in the inlet while Sun Aviation was replacing the engine mount under a warrenty program.  Several other engines have been found to have this problem by Sun and I was told that Beachcraft had the same problems in King Airs and changed to an aluminum casting.

    A great flying plane but with limited range and payload.

    Turboprop_Pilot


    Interestingly, the plane that I flew was a 2006, had been in FL one year and had significant corrosion to a point where P&W sent the engine back to the factory and essentially conducted a hotsection. 
  •  02-04-2008, 10:42 AM 531 in reply to 429

    Re: Piper Meridian Review

    Inspired by Joe's public PIREP on his Meridian flight, I published to my blog my Meridian PIREP back in Nov.

    http://davidwihl.blogspot.com/



    -David, KBED, Mustang #165
  •  02-05-2008, 3:19 PM 565 in reply to 531

    Re: Piper Meridian Review

    wihl:
    Inspired by Joe's public PIREP on his Meridian flight, I published to my blog my Meridian PIREP back in Nov.

    http://davidwihl.blogspot.com/




    David,



    Enjoyed the review.  Good data on the noise levels. It really does seem like a decent plane.  I wish I had not seen the Meridian NTSB data.  I suppose if one never flies in turbulence, near convective activity, or icing everything should be fine. 
  •  02-05-2008, 4:09 PM 566 in reply to 565

    Re: Piper Meridian Review

    Joe,

    The Malibu/Mirage/Meridian is THE most reviewed GA design in history, more than even the much maligned MU-2.  Like the MU-2, the Meridian (and Malibu/Mirage) IS a safe plane, but like all planes it has limits - the difference is you fly closer to those limits in high performance aircraft like the Meridian, or almost any other turbine powered aircraft.

    Pilot competence is the most important factor.  Know what you are doing, pay attention to what the plane is doing, monitor and manage the systems effectively and you can fly anything.  Most breakups are due to the autopilot doing something the pilot did not notice and when he did finally notice his reaction was inappropriate for the situation/circumstance and overstressed the airframe.

    Training is always very important, but even more so when we move out of Bonanza's and into faster, more capable aircraft.


    Yeah, I said it.
  •  02-05-2008, 5:26 PM 567 in reply to 566

    Re: Piper Meridian Review

    ColdWetMackarelofReality:

    Joe,

    The Malibu/Mirage/Meridian is THE most reviewed GA design in history, more than even the much maligned MU-2.  Like the MU-2, the Meridian (and Malibu/Mirage) IS a safe plane, but like all planes it has limits - the difference is you fly closer to those limits in high performance aircraft like the Meridian, or almost any other turbine powered aircraft.

    Pilot competence is the most important factor.  Know what you are doing, pay attention to what the plane is doing, monitor and manage the systems effectively and you can fly anything.  Most breakups are due to the autopilot doing something the pilot did not notice and when he did finally notice his reaction was inappropriate for the situation/circumstance and overstressed the airframe.

    Training is always very important, but even more so when we move out of Bonanza's and into faster, more capable aircraft.



    You are right.  It is a safe plane within limits.  So is every plane that is certified by the FAA.  Even the Eclipse is safe within limits.  My problem after looking at the data is that those limits are not broad enough for me to feel safe flying in it with my family.  In comparison, the TBM in 17 years since certification has had nothing even remotely close to a structural failure that I could find.  In 7 years the Meridian alone not including all the Mirage data, shows numerous examples of fatal in flight strucural failure and non fatal structural failures. The last example of fatal in flight breakup was within the last 6 months. Both TBM and Meridian have had pilots who have made critical errors in judgement and have died as a consequence.  Every pilot is capable of a critical error in judgment.  I do not want to be defined by a mistake that costs me my life or someone else's because I was a cheap *** and bought a plane that can break up in severe turbulence or one of the other flight conditions that have resulted in structural failure for a Meridian.  Probably one of the reasons it bothered me so much to see that NTSB data is how much flying I do in the mountains.  I have had more than one encounter with unforecast turbulence meeting the technical definition of severe.  Since max manevering speed is just about what my Cirrus is, but it is capable of going 30% faster, that is an awful lot of slowing down to do to stay within limits.  The last thing I want to be thinking about as I am motoring along with my head banging the ceiling is whether the plane is going to fall apart.  Am I paranoid? Perhaps a little, but it is just not worth it to me to worry about it or my family.  The TBM has a 270 kt VMO and offers an easy choice as an alternative.   Flame away
  •  02-05-2008, 7:55 PM 570 in reply to 566

    Re: Piper Meridian Review

    ColdWetMackarelofReality:

    Joe,

    The Malibu/Mirage/Meridian is THE most reviewed GA design in history, more than even the much maligned MU-2.  Like the MU-2, the Meridian (and Malibu/Mirage) IS a safe plane,

    The Meridian has the SLOWEST Vmo (188kts) of ANY presurized TP airplane. Vno/Va can be as low as 127kts at light weights. Every Meridian pilot while flying low is constantly having to pull the power back to avoid busting the Vmo. Even in cruise flying in the 20s you are pressing right up against Vmo.

    That puts the pilot and plane in a trick position. Any upset (such as CAT, autopilot roll) or pilot innatention (such as failure to reduce power on descent) immediatelly puts excessive stress on the airframe. There is no buffer. Few of us would be operating our planes right against redline. However, the Meridian pilot has no choice if he wants to enjoy the speeds.

    That is the difference ColdWet. Yes, the Meridian is safe if operated within its envelope, HOWEVER, normal Meridian operation puts the pilot and the airframe right against that envelope limit most of the time. THAT is NOT safe.

    In addition, it is clear that some airframes have a much, much higher margin above and beyond the certification limits. And it shows on accident records. Mooneys (M20J and later) for example are very clean and easy to overspeed/overstress, yet there is no in-flight-breakup issue on those airframes. Malibus, despite being flown by better trained pilots have a substantial issue. Is it due to presurization and flying high - I don't think so. I'm willing to bet that the Piper Matrix will have a substantially worse IFB record than the Mooneys.

    FAA requirements should be the minimum, not the optimum safety margins. Malibus and Meridians simply cut it too closely to the minimuns.

  •  02-05-2008, 8:52 PM 572 in reply to 570

    Re: Piper Meridian Review

    B95,

    I believe we are in violent agreement.  In the part of my original post that you did not snip I said essentially the same thing you did - you are flying closer to the limits in the Malibu/Mirage/Meridian than in say a Mooney as you pointed out.

    Altitude and pressurization DO have an impact on IFSB both in terms of the potential energy and also in terms of the stresses on the airframe.

    I can accept that it is too close for comfort for Joe, or for you - and I am not an advocate for the Malibu/Mirage/Meridian, I have not flown it, do not own one.

    Just pointing out that like other ships that are operated close to the limit like the MU-2, these types of aircraft are less tolerant of pilot error and inattention.

    I would also suggest that for the piston versions especially but also the Meridian, the PA-46 has a price point that attracts a different quality pilot/owner than does a TBM or especially the Pilatus - theses are not the same kind of pilots - like comparing a C-150 pilot to a P-210 pilot - simply not the same class. 

    This is actually one of my primary concerns about the VLJ class in general and the Eclipse 500 in particular, it seems to open up access to a class of performance which used to have a certain barrier to entry that helped keep less qualified/capable pilots out of harms' way.  Look at the introduction of other performance changing aircraft, the Bonanza, the Malibu, the LearJet, even the Citation - in the hands of poorly qualified or poorly trained pilots they are dangerous.

    It is my belief that we each have the responsibility to set equipment minimums, and training/experience minimums, just like weather minimums - and those decisions should be made on good info.  Good info is that the Malibu/Mirage/Meridian are safe designs when flown within limits, just like every other plane out there - yes the margins may be different than other aircraft but different is not bad.


    Yeah, I said it.
  •  02-06-2008, 2:03 PM 580 in reply to 572

    Re: Piper Meridian Review

    JoeN,

    You put the problem clearer than I have heard before.  The Meridian is nearly always flown at Vmo and its maneuvering speed is quite slow, so if unexpected turbulence is encountered, the airframe is stressed to a higher level than other turbine aircraft, whose maneuvering speed is closer to their Vmo.  If yu have the data, it would be interesting to see how many breakups and wing bends have occured vs flight hours.  Since the TBM has been around longer and has more flight hours with NO problems of structural over stress or breakup, it is clearly a safer plane.  When training in my TBM, I was told that the Vmo for the same aircraft as used by the French Air Force was 305 kts!

    I saw the PiperJet wing on a factory tour- it is a couple of feet longer in span, built beefier and has a larger fuel capacity.  If Piper replaced the present Meridian wing with the PiperJet wing, they would acquire several major benefits:  Lower stall speed, higher useful load, more fuel and much better strength in the wing!

    Turboprop_Pilot
  •  02-06-2008, 2:35 PM 582 in reply to 580

    Re: Piper Meridian Review

    Turboprop_Pilot:
    JoeN,

    You put the problem clearer than I have heard before.  The Meridian is nearly always flown at Vmo and its maneuvering speed is quite slow, so if unexpected turbulence is encountered, the airframe is stressed to a higher level than other turbine aircraft, whose maneuvering speed is closer to their Vmo.  If yu have the data, it would be interesting to see how many breakups and wing bends have occured vs flight hours.  Since the TBM has been around longer and has more flight hours with NO problems of structural over stress or breakup, it is clearly a safer plane.  When training in my TBM, I was told that the Vmo for the same aircraft as used by the French Air Force was 305 kts!

    I saw the PiperJet wing on a factory tour- it is a couple of feet longer in span, built beefier and has a larger fuel capacity.  If Piper replaced the present Meridian wing with the PiperJet wing, they would acquire several major benefits:  Lower stall speed, higher useful load, more fuel and much better strength in the wing!

    Turboprop_Pilot


    I did a quick search and could not find anything relative to accidents/indidents per flight hour, but that data may be available only through Piper. 
    It would be interesting to see if Piper chose to share components from the Piper Jet with the Mirage line.  They are obviously aware of the reputation of the airframe.  The sales rep. mentioned something offhand about it.  His words were dismissive making the suggestion that anyone who had a structural issue had done something stupid like fly into a category 5 thunderstorm. 
  •  02-07-2008, 12:08 AM 591 in reply to 572

    Re: Piper Meridian Review

    ColdWetMackarelofReality:

     Look at the introduction of other performance changing aircraft, the Bonanza, the Malibu, the LearJet, even the Citation - in the hands of poorly qualified or poorly trained pilots they are dangerous.

    It is very true that certain airplane introductions with a step in performance in the past, the Bonanza being a great example as you pointed out, have caused problems. It is also true that others have not - the citation 500/501 for instance had a great safety record at first.

    I am hoping that in this day and age, where we know so much more about pilot training, have full motion simulations, mentor/transitioning programs, insurance underwriters, and an ATP-standard checkride, that few, if any, un-euiped pilots will squeak through the cracks into the cockpit of say an EA500. I actually feel pretty good about the prospects. Note that any joe-smoe with a private pilot ticket can buy a used King Air B200 for $500K and go flying with no insurance, no additional training, etc. The regs are all screwed up. A type rating would be required to fly a 25K-limitted, 5,000lbs diamond jet, but not to fly a 30K-capable 12,500lbs King Air B200. I don't know anyone who thinks that B200 (particularly the older models) is easier to handle.

  •  02-18-2008, 12:45 PM 649 in reply to 397

    Re: Piper Meridian Review

    reposting a comment from Bill on the blog:

     

    Bill said:

    I owned a Meridian for 4 years and 900hrs.  Nice transitional airplane but it broke a lot and the airframe is light for its power.  I had 11 AOG  (aircraft on the ground) issues during that period including smoke in the cockpit.  I've owned a TBM C2 model for 2.5 yrs and it's fabulous.  Doesn't break and I've never had an AOG issue in 400+hrs of flying.  It is built like a tank- it's VNE is 266kts all the way to FL310 compared to 188 on the Meridian.  I have a new 850 coming in August with the G1000.  I chose it over the Mustang after careful consideration and a test flight.  I should let you let you know that I have an SP type rating in a Cessna CJ2.  The Mustang is a nice airplane but has a very limited fuel/payload range compared to the TBM 850, CJ1+ or CJ2.  It also burns 30 to 40% more fuel depending on altitude, routing, and distance compared to the 850 and typically saves less then 5 minutes.  The TBM will actually beat it in a strong headwind in both time and fuel over a stage length greater than 600nm when the Mustang is forced to go up high into the stronger wind.  

    The VLJs are compelling and everybody, including me, prefers them over turboprops but what people don't realize is the penalty in fuel burn for short flights or being held down.  Another issue with all jets is performance when the air is warmer then standard atmosheric conditions (ISA) which typically occurs 9 months out of the year.  I asked Cessna for the ISA +10, +20, +30 charts for the Mustang and they suggested I buy a CJ1+.  Interesting.  This means that the Mustang may not be able to climb directly to FL410 when it is warmer then ISA (I didn't get the charts but the Eclipse cannot climb directly to FL410 above ISA) which will have a noticable impact on range and ATC may not want a 340kt airplane sitting in the mid to high 30s with the airliners doing 470kts.  

    High altitude take-off performance is another consideration for those who plan to operate out of mountain airports.  For example, at approximately (it was 6 months ago when I did the calculation) 52F in Aspen you have to start trading either fuel or payload since you can't takeoff at max gross.  Want to takeoff with 4 people on a summer 75F day out of ASE?  You will have only enough fuel to make it to Grand Junction (80nm).

    Clearly there is a substantial market for VLJs but it seems to me that most of the depositers are new to turbines.  What they don't realize is the much higher costs of flying a jet especially for trips less than 700nm.  When I compare the CJ2 to the TBM850, the CJ2 costs 2x to operate and more than 2x to buy but only goes 20% further, 20% faster and carries 20% more.   The used market, the ultimate barometer of how successful an aircraft is, is really strong for both the CJ2 and TBM.  In fact, if you bought a CJ2 in 2001 you could sell it today for more than you bought it.  Why?  Good combination of performance and operating cost.  This is not true with the original CJ which I've also flown and didn't climb well above FL370.  It is considered a dog or a "slowtation" by most jet pilots.  A used one today can be bought for as little as $2.2M.  

    When I flew the Mustang 4 months ago I was shocked that it burned 120 gallons during the 1 hour demo.  To be fair we had a 15 minute wait to takeoff but we also went to FL280 and stayed for a while to examine flying characteristics.  That's a lot of fuel for an hour flight.  For the CJ2 I typically use 1000lbs (150gallons) for the first hour and 700lbs (105g) for every hour at FL450 for flight planning.  If I am flying out of the Northeast or SoCal then I'll use 1200hrs for the first hour.  I just figured there would be a bigger difference between a CJ2 and a Mustang in fuel burn based on their capabilities.  

    With the rising cost of jet fuel I think a lot of pilots who are new to jets are going to be dissappointed with their new VLJ once they realize how expensive and limited it is.  The real question is once the VLJ market settles how will the used market value them?  How many Mustang owners will want to move up to a CJ1+ (IMO a real jet) in order to carry more and go further, faster?  Or move down to a TBM, Pilatus, or Meridian because they realize that for short trips of less than 600nm the time difference isn't significant but the fuel burn is.  People have been predicting the demise of the turboprop for 20 years but sales have never been better especially for the singles.  Why?  You just can't beat them for the ability to carry people and stuff out of small airports and in efficiency - especially on short trips.    

  •  06-14-2008, 11:10 AM 3845 in reply to 649

    Re: Piper Meridian Review

    Bill, I think you've hit the nail on the head about the new generation of VLJ's.  It sounds like a great idea until the chips are down and the fuel runs out due to a missed approach at a close alternate or some other unforeseen malady.  The truth is that jet engines burn lots of fuel, no matter how small they are.  And they burn even more at low altitude.  We all have to come down some time and if we move slower than other traffic then we will probably come down even earlier because of ATC.  High bypass is a great technology to make an engine that burns 2000lbs per hour only burn 1500lbs or so per hour; but that is a very different matter than trying to make a Williams FJ44 or a small PW engine burn 35 or 40 gallons per hour for an aircraft that only holds 250 gallons total to begin with.  And remember, there are two thirsty ones out there.  Just try to tell the boss man that he shouldn't invest in a new VLJ because it is too light duty and too short on fuel to be practical and it's an impossible uphill battle after the salesman gets done brainwashing him with sales hype.  Granted, jets are quieter than props and if you don't have to face headwinds, a slow jet will get you there 10 minutes earlier with a much higher fuel bill.  But as the little old lady at Wendy's always said, "Where's the Beef?"  It just isn't safe to build high tech wonder aircraft that substitute technology and gadgets for beefy airframes and fuel.  The sky is a harsh environment and it is easy for a boss who is thinking nice weather and sunny days to be sucked into spending his money on a dainty little airframe that could come apart in the harsh conditions that aviation reality brings from one day to the next.  We now have the technology available to make the cockpit of a single engine piston look more professional than the Boeing products of yesteryear.  Clip a few wires together with a mass produced microchip circuit format, add color weather capabilities, a cheap autopilot and updatable software and "bang" you can get people to lay down big bucks for a machine that will have airframe cracks within the first 100 hours of flight.  They may have enough engine to get to high altitude, but it's like the dog that loved to chase cars.  One day he finally caught one and it was his undoing.  Expensive Piper pistons also fall in this category.  We are having major problems getting our Avidyne MFD to quit scrambling and tell us how much fuel we have and what the oil pressure is and Avidyne doesn't even have any spares or loaners while ours is in the shop. Avidyne finally returned our calls but didn't even offer to help us and the service center tells us it might get fixed with 10 days of down time on this new Matrix which cost us the better part of a million dollars.  Maybe I'm old school, but mark my words, "High tech, combined with low beef and low fuel is going send many to their graves when it comes to airplanes."
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