bnt83
Final Approach
Remember that when you buy a set of cables and turnbuckles from Piper, the liability clock on those parts starts again.
Does the 15 year rule cover aftermarket parts manufacturers also?
Remember that when you buy a set of cables and turnbuckles from Piper, the liability clock on those parts starts again.
How many owners do you believe have replaced these cables?
Plus how many of those owners will use a replacement cable manufactured in the field?
Lots of common sense things simply do not add up in this AD.
I doubt that aggressive control checks come anywhere near to the proof load of an 1/8 cable and its terminal.
Corrosion problems seems reasonable tho.
Proof load is 60% cable rated breaking strength which for 1/8 inch 7x19 steel cable would be 1200 pounds.
My thoughts exactly.Cuz it aint a problem with the hardware. If it was it would be on the hardware, at least all the hardware on the affected planes, not just the stab ones. Me thinks that it has something to do with the environment created for the hardware my their position in the tail of certain piper aircraft
I don't see why not. The AD is for aircraft type, not turnbuckle maker.Does the 15 year rule cover aftermarket parts manufacturers also?
I don't see why not. The AD is for aircraft type, not turnbuckle maker.
I meant to say that I don't see why it would cover the buckle itself. I wrote it wrong. You are right about that.The FAA knows if they hit the turnbuckle manufacturer and all the aircraft that uses them there would be a riot in the Aviation industry.
I have survived an elevator cable failure at rotation in a PA32-300. This occurred 7 hours after the AD Inspection. My opinion is "Change the Cables" it is cheap insurance. Reaction time to the failure approximately 3-4 seconds after the bang and control yoke coming into my lap.
The Piper Service Bulletin was not being complied with, so the FAA made it an AD. Don't wait for annual. Have this inspection completed immediately. The life you save may be your own. Mechanics are seeing cable problems in many aircraft that are being inspected.
Wow...I have survived an elevator cable failure at rotation in a PA32-300. This occurred 7 hours after the AD Inspection. My opinion is "Change the Cables" it is cheap insurance. Reaction time to the failure approximately 3-4 seconds after the bang and control yoke coming into my lap.
The Piper Service Bulletin was not being complied with, so the FAA made it an AD. Don't wait for annual. Have this inspection completed immediately. The life you save may be your own. Mechanics are seeing cable problems in many aircraft that are being inspected.
Aren't they the ones that don't believe Hawaii is a state?Who are the 49ers?
Many aren't doing well about looking at cable wear. I found all four aileron cables looking like this.
I have survived an elevator cable failure at rotation in a PA32-300. This occurred 7 hours after the AD Inspection..
There's a first time for everything, I suppose.J Mac McClellan hits it out of the park.
Look up the Stearman. There are a total of five AD's, last one came out in 1963.
Most of what I have read about the failures is back near the vent fan mounting location. Many times moisture is present from entering the intake screen in the vertical stab. Breaks in the scat tubing and sometimes just leakage through the scat tube connections allow moisture into the empanage near the turnbuckle causing corrosion. I knew about this prior to purchasing and had the A&P crawl back into the tail section to look at it. Nothing was found on the cable or swage or turnbuckle, but some corrosion was noted behind the battery box which I had him remove and treat.
Hopefully it won't take too long at annual, or I might have it looked at next time I have my A&P in my plane.
FWIW I am working on this AD now on a -140, turnbuckles are clean but there is an area of corrosion right under the lower turnbuckle. This is directly under the low spot on the scat tube coming from the vent fan...
got a pic of it?