Yingling Aviation maintenance review

po1212

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po1212
I recently had engines installed on my twin Cessna at Yingling Aviation in
Wichita Kansas. I am leaving this review because of the bad management
and poor workmanship I received at Yingling. The total cost was more than
the aircraft is worth. I just do not see how general aviation can survive the
current pricing. Yingling charged a premium price, but had substandard quality
of work and customer service. I would recommend looking elsewhere for
maintenance.

Yingling was acquired by a private equity firm in 2023 and has had high
turnover of personnel since then, as normally happens in this situation.
In the end I was left feeling it was Yingling in name only. It is not the same
company it once was. It is sad to see a once reputable shop go downhill
like this.

Below is a list of items I noted during the process. Items 1 thru 12 were
from before I paid the invoice and 13 thru 28 where after the invoice was
paid and taking delivery of the aircraft. This list was provided to Yingling
and their response was that my aircraft was old.

1) Both of the project managers I dealt with were not very organized, they
often did not respond to emails to answer my questions and did not keep
me informed of the progress. I had to specifically ask to get updates,
only sometimes would an update be provided.

2) Initially and multiple times I requested that new hose kits be
installed, but over a month into the project they still had not ordered
them, which caused further delays.

3) Initially and multiple times I requested that the silicone baffle seals
be replaced, they did not order these soon enough causing delays.

4) Initially and multiple times I requested that new SCAT tubing be
installed, but the old was reused and some of it had holes in it.

5) I was charged over Ram's list price on the hoses and baffle kits. Ram
gives the FBO a discount and normally the FBO would then charge the end
customer the list price. The price of $9,275 seems very high and when I
asked how many hours it was for, I never got a response.

6) There was a lot of confusion over the exhaust stacks and they asked
about this three different times, both project managers asked at
different times. I had provided all of the exhaust except both LH
stacks as they were recently replaced. They thought one stack was
missing and that both outboard stacks were the same part number and
both inboard another part number. I had to explain to them that while
some of the 400 series Twin Cessna's might be like that, the Cessna
T310/320 use the same part number on the LH stack on both engines and
the RH stack on both engines share another part number. I had to send a
diagram showing this. It appears that Yingling does not do many Twin
Cessna engine installs anymore.

7) They broke one of the alternators and never informed me of this, I saw
the replacement on the invoice, but was not charged for it directly.

8) I was charged $1,228.89 for shipping. I assume this was for next day
shipping, but if they had ordered the parts when I requested them the
first time, next day shipping would not have been needed.

9) The invoice shows, customer requested prop overhauls, I only agreed to
it because I was told it was a safety of flight issue. I requested pictures of the
damaged parts, but no pictures were provided to me. The props only had
800 hours on them since new and have a 2000 hour TBO. It is hard to believe
they had this much damage to the bearing races and piston.

10) After having the aircraft for a month they said there was a crack in
the LH throttle body bracket, this caused further delays. They should
have inspected everything on engine removal.

11) They broke a hose fitting p/n 0850695-1 in the right engine throttle
body, which caused further delays. They were unable to find one so I
had to find one and since the fitting was not available I got the
whole 632855-1A6 throttle body from a shop parting out a C310Q. A day
later I was able to find new surplus fittings. They knew this was broke
for at least a week, but never told me, given more notice I could have
gotten a new fitting. This caused a couple more days of delay.

12) My first choice of a shop to install the engines was Continental
Services, but Yingling quoted about $11,000 less. In the end it cost
much more to have Yingling do the work. Assuming the props had
worn/damaged parts that needed replacing, Continental would still have
cost less. The Continental quote included: prop overhauls, prop
governor overhauls, remove inspect install exhaust, new Teflon fluid
hoses with integral fire sleeve, new engine mounts, new SCAT hoses,
baffle seal, ducts, hardware, and supplies, engine oil fill, dynamic
prop balance, and flight test. Yingling's quote only included removal
and install of the engines. They did not perform a flight test.

The following items were found after paying the invoice and taking delivery
of the aircraft.

13) RH engine tach generator cannon plug was not safety wired.

14) There were no AN931-5-9 elastic grommets installed where the spark
plug wires go through the metal baffle to the spark plugs. Some of the
spark plug wires are already starting to chafe from rubbing on the
metal baffle. This also causes cooling air to be lost instead of being
forced through the cylinder cooling fins.

15) Elastic grommets (AN931) where not installed in the metal baffle
on the aft section where the upper deck air lines pass through the
baffle. These open holes in the baffle will cause cooling air to be
lost instead of being forced through the cylinder cooling fins.

16) On the LH engine by the #5 cylinder spark plug wire, the new
silicone baffling that was installed has tears in it. The #2 cylinder
baffle area had a 1 inch square cut out of it. I was charged $3,002.50
for new silicone baffling to be installed, I would expect it to not
have holes in it.

17) The quote included cleaning of the engine compartments. There was
obviously no cleaning performed as the compartments are full of oil,
grease, dirt, and grim.

18) The RH engine oil temp probe was suppose to have a new
MS3106A12S3S cannon plug installed. The cannon plug was
owner supplied. The old cannon plug is still installed. The log
entry shows it was replaced, but it was not. The old wiring with
splices is still there, a new connector would have needed new
wires soldered to the connector. The new connector that was
provided to you, but not installed, needs to be returned to me.

19) The old SCAT tubing that was re-installed has numerous
holes in it. I had several times requested all of the SCAT to be
replaced. Why would an A&P/IA or FAA repair station install
SCAT tubing in this condition? This is not cosmetic, the SCAT
tubing has a purpose.

20) The clamps which mount the air/oil separators onto the
engines are missing.

21) Both exhaust tail pipes have new life limited S1921-1 clamps
installed. The old clamps were installed a couple years ago, p/n
NH1000897-40 and are $694.95 each. The old clamps need to be
returned to me, they are the style that are NOT life limited. I was not told
new clamps were being installed and did not approve this.

22) None of the old exhaust was returned to me. It could be inspected,
recertifed and sold.

23) Mixture controls are mis-rigged, when leaned they do not line up, they
are off about 3/4".

24) LH engine idle is low at 500 RPM, RH engine idle is high 800 RPM.

25) Full power fuel flow is low on the LH engine at 27.4 GPH. The RH
engine is 28.6 GPH. They both should be 29.5 GPH. Idle mixtures are
off too, was the fuel system setup per the Continental service builtin?

26) On both engines the 25 year old flexible fuel lines between the flow
transducers and fuel manifolds were not replaced. I requested multiple
times that all the fuel lines be replaced and Yingling confirmed they would be.

27) Both engines had the main fuel line routed too close to the turbo charger,
the RH fuel line was within an 1/8" of the turbo!

28) They used a white pipe sealing compound on the AN fittings in the fuel flow
transducers, but JPI specifically says to not use any compound on the threads.
They did not follow the manufacturers instructions.
 
I had my run out O-470 replaced with an IO-550 at Air Plains in Wellington, KS. They did a superb job. Sorry you had trouble.
 
Did you ask them to fix any of the items? Did you pay with a credit card?
 
Did you ask them to fix any of the items? Did you pay with a credit card?
I did not pay with a credit card. I asked for a refund on some items, like the torn up silicone baffle. They offered to send a small piece so I could replace part of it. If I bought a new car (which cost less than this did) and the leather seats had a tear in them, I would not want a patch applied...
 
I did not pay with a credit card. I asked for a refund on some items, like the torn up silicone baffle. They offered to send a small piece so I could replace part of it. If I bought a new car (which cost less than this did) and the leather seats had a tear in them, I would not want a patch applied...
Guessing it’s far away? Sorry about your experience.
 
A pair of new engines on a T310Q is always going to cost more than the aircraft is worth, but you end up with a great plane in the end.

Suspect no one is seeing a lot of twin Cessnas getting this amount of work any once anymore. And certainly very few 310s, most of which are now on the downside of the "maintenance vs. desirability" curve, meaning that many have now been ridden hard and put away wet. 340/414/421, a little better, but these are all complicated wonderful machines that are getting very long in the tooth.

While this is a miserable list, it does seem that most of it can be rectified. The band clamp substitution is troublesome - are the non-life limited ones rare or common? Been out of the turbo game for a while, but have seen various ADs for band clamps out of the old SBs. And some threads that say they are unobtanium or were for a while.

How did they break an alternator? Did they drop it or mess up the expensive gear coupling? Were the engines RAM overhauls that Yingling was to hang?
 
A pair of new engines on a T310Q is always going to cost more than the aircraft is worth, but you end up with a great plane in the end.

Suspect no one is seeing a lot of twin Cessnas getting this amount of work any once anymore. And certainly very few 310s, most of which are now on the downside of the "maintenance vs. desirability" curve, meaning that many have now been ridden hard and put away wet. 340/414/421, a little better, but these are all complicated wonderful machines that are getting very long in the tooth.

While this is a miserable list, it does seem that most of it can be rectified. The band clamp substitution is troublesome - are the non-life limited ones rare or common? Been out of the turbo game for a while, but have seen various ADs for band clamps out of the old SBs. And some threads that say they are unobtanium or were for a while.

How did they break an alternator? Did they drop it or mess up the expensive gear coupling? Were the engines RAM overhauls that Yingling was to hang?
Flying several states away back to Yingling to rectify the discrepancies did not seem like a viable solution to me. I tried to rectify a lot of the issues while the aircraft was still there, but they were dismissive or ignored me. A partial refund would work best, for example I should be refunded the full cost for the new silicone baffle that was cut up (for unknown reasons) by them. The non-life limited clamps are available but cost 4 times as much as the life limited clamps they put on. I had the same question on the alternator, but never got a response. The invoice says the ear was broke off, so I assume they dropped it or maybe over torqued it? The engines were Continental factory rebuilt. Plus the age of the aircraft should not have been a cause of any of these issues, after all the engines and accessories were new.
 
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Here is a photo of some of the SCAT tubing they installed. The back side is in even worse shape. Also note how close this is to the turbo. The main fuel line is inside that SCAT! It is supposed to be routed forward of the throttle body and fuel/air control unit, it was properly routed before they worked on it.
image.jpg
 
The IA I use would never sign that off. Not even a ferry flight.
 
Here is a photo of some of the SCAT tubing they installed. The back side is in even worse shape. Also note how close this is to the turbo. The main fuel line is inside that SCAT! It is supposed to be routed forward of the throttle body and fuel/air control unit, it was properly routed before they worked on it.
View attachment 135911
Notwithstanding the incorrect routing, is the fuel line firesleeved inside that SCAT hose? Also, would rather switch to SKEET if doing a major and everything is out anyhow. Don't know what the aluminum line is doing, but amazing how good a zip tie can be at starting to carve into it. Adel clamp please, at least to make a stand-off.
 
Notwithstanding the incorrect routing, is the fuel line firesleeved inside that SCAT hose? Also, would rather switch to SKEET if doing a major and everything is out anyhow. Don't know what the aluminum line is doing, but amazing how good a zip tie can be at starting to carve into it. Adel clamp please, at least to make a stand-off.
It is fire-sleeved, but still it should not be routed where it is. I requested multiple times to have all the SCAT replaced and they did not replace any of it. Some is so mangled, they must have had a hard time getting it over the fuel lines.
 
It is fire-sleeved, but still it should not be routed where it is. I requested multiple times to have all the SCAT replaced and they did not replace any of it. Some is so mangled, they must have had a hard time getting it over the fuel lines.
I'd have probably just routed it correctly away from turbo and let the firesleeve do its job without the SCAT there, but maybe there's a good reason for it.
 
I'd have probably just routed it correctly away from turbo and let the firesleeve do its job without the SCAT there, but maybe there's a good reason for it.
The SCAT provides cooling, it is connected to an air intake on the bottom of the cowl. Safety, helps with hot starts, and the TC requires it. The holes are allowing the air to not flow properly.
 
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The SCAT provides cooling, it is connected to an air intake on the bottom of the cowl. Safety, helps with hot starts, and the TC requires it. The holes are allowing the air to not flow properly.
Ah, starting to sound familiar. Actually I found the TSIO-520s pretty easy to hot start. Had more trouble cold starting them, including managing to frost all the plugs a cold morning in AZ. Just waited that one out, but could have been a long delay if it was a truly cold place...
 
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