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- Jan 9, 2013
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- Jon
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- KCMA
I need some help figuring out the math for the Piper wing AD.
One of our locals is looking at a PA28-140 with 3,890 on the airframe with 28 100 hour inspections.. So does this look right?
(N × 100) + [T - (N × 100)] / 17 = Factored Service Hours (FSH)
(28 × 100) + [3890 - (28 × 100)] / 17
2800 + 1090/17
3,890/17
FSH = 229
I didn't find anything here...
drs.faa.gov
Forthcoming AD on Piper wing spars for much of the PA-28 and PA-32 fleet. Of the 2800 eddy current inspection reports from the prior interim AD around 100 "anomalies" and 6 fully developed fatigue cracks were found. The spar was cold formed leading to high residual stress near the bolt hole locations. Piper has changed the manufacturing process to machine the bend to avoid this issue on all new airframes.
The proposed AD has more info but it appears a variety of scenarios can eventually develop...
In advance... thanks
One of our locals is looking at a PA28-140 with 3,890 on the airframe with 28 100 hour inspections.. So does this look right?
(N × 100) + [T - (N × 100)] / 17 = Factored Service Hours (FSH)
(28 × 100) + [3890 - (28 × 100)] / 17
2800 + 1090/17
3,890/17
FSH = 229
I didn't find anything here...
Dynamic Regulatory System
Forthcoming AD on Piper wing spars for much of the PA-28 and PA-32 fleet. Of the 2800 eddy current inspection reports from the prior interim AD around 100 "anomalies" and 6 fully developed fatigue cracks were found. The spar was cold formed leading to high residual stress near the bolt hole locations. Piper has changed the manufacturing process to machine the bend to avoid this issue on all new airframes.
The proposed AD has more info but it appears a variety of scenarios can eventually develop...
- xenadu
- Replies: 193
- Forum: Maintenance Bay
In advance... thanks


