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Thinking of buying a PA38

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Thinking of buying a PA38

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Old 21st Aug 2017, 00:24
  #41 (permalink)  
 
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I have flown the PA 38 including instructing in it. Flying wise it is a pretty decent handling airplane and the killer spin rep is a total myth as there is nothing wrong with the spin characteristics.

The one thing that really put me off the aircraft was the brutally crap build quality. A Yugo looks better built than this aeroplane. It is no coincidence that virtually every flying school has gotten rid of them and in many cases gone back to Cessna 152's.

Personally if you are looking for a good certified 2 seater, go look at the Grumman AA1B or even better a AA1C. Less money than a 152, an honest 10 knots faster and with delightful handing, great visibility, thanks to the canopy, and a surprisingly wide and comfortable cockpit.

I have owned a AA1B for 17 years and found it a cheap and cheerful run about. It has proven very reliable and it is fully supported by Fletch Air.

The Grummans have an excellent type club at aya.org.
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Old 21st Aug 2017, 15:01
  #42 (permalink)  
 
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They surely do restore them or, why the wing spar mod ?


You might have cause to regret a Robin HR100. I owned one and one day the flap deployment motor failed. Getting spares out of Robin is like asking a Yorkshireman for a loan.


The position of the motor in the a/c makes it all but inaccessible. The a/c disappeared for about two months and I received a huge bill. That, plus the bill for the Star annual as it then was removed me from the list of Robin satisfied customers. That said, the a/c was a delight to fly.
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Old 21st Aug 2017, 15:08
  #43 (permalink)  
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I think he wants a Grumman Tiger next.
I have a share in a Cheetah (Tiger with a smaller engine and lower MTOW) and love it for touring, as well as very much preferring it to fly and instruct on to the standard Piper and Cessna products (not that I dislike the PA38 or C152, although I find the PA28 and C172 dull and heavy) - a Tiger would be nicer still.

I've never flown one, but suspect that BPF's views on AA1s may well be good here in the UK also - there's a reasonable amount of expertise around on how to operate and maintain them, and Mattair at Bournemouth are a very ready source of spares if needed for all of the Grummans.

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Old 22nd Aug 2017, 10:10
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People don't restore Tomahawks in America. Once the engine is done, this are pushed to the weeds.
I had a complete PA38 that was repainted, and de registered in the hope it would go on the N reg. I parted it out rather than spend 4-5k getting it airworthy and going through the hassle of getting a DAR here. It made alot more in parts than I could have got for it flying.
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Old 22nd Aug 2017, 11:16
  #45 (permalink)  
 
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Learnt to fly in one, including spinning. Nice a/craft and more space than a 152.

If I was looking to buy a 2 seater though, I'd look at something like an RV.
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Old 22nd Aug 2017, 13:18
  #46 (permalink)  
 
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Originally Posted by Big Pistons Forever
I have flown the PA 38 including instructing in it. Flying wise it is a pretty decent handling airplane and the killer spin rep is a total myth as there is nothing wrong with the spin characteristics.
The souls that lost their life in one beg to differ.
Semantics but was it the spin characteristics or how it spun?
The yoke rod would get stuck in the panel in the full aft position thus not allowing for recovery.
Fatalities included flight instructors, examiners as spins are required in the USA for flight instructor training/examining.
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Old 22nd Aug 2017, 18:09
  #47 (permalink)  
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Can you post a link to the accident investigation report on the fatality you're talking about B2N2?

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Old 22nd Aug 2017, 19:57
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Originally Posted by Genghis the Engineer
Can you post a link to the accident investigation report on the fatality you're talking about B2N2?

G
I'll look for it when I'm not on my phone.
In the mean time it's been discussed here before
http://www.pprune.org/archive/index.php/t-309978.html

The issue is mentioned here:

Piper Service Bulletin 661, entitled "Control Column Installation Modification", was issued on August 22, 1979. The purpose for issuance of Piper Service Bulletin 661 was reported as, "It has been reported that roughness or binding of the control shaft in the instrument panel cutout hole can occur when the control wheel is full aft and direct forward or upward-and-forward pressure, rather than linear pressure along the control shaft, is applied. This Service Release contains instructions for the modification of the control wheel shaft bushing assembly to provide a smoother forward movement of the control shaft from a fully aft and up position." A copy of Piper Service Bulletin 661 is attached to this factual report.
Piper Service Bulletin 800, entitled "Elevator Control Travel Modification", was issued on November 19, 1984. The purpose for issuance of Piper Service Bulletin 800 was reported as, "It has been reported that when either control wheel is full aft and an upward-and-forward pressure is applied, the potential exists that the pilot may be unable to move the control yoke out of the full aft position. This Service Bulletin provides instructions to modify the elevator up travel to alleviate the above described problem."
https://app.ntsb.gov/pdfgenerator/ReportGeneratorFile.ashx?EventID=20001212X19701&AKey=1&RType =Final&IType=FA

I'll look for more.
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