Does anybody have any insights into the history and disposition of this SB?
Specifically, I am wondering:
How prevalent are the rib cracking problems that the SB addresses?
Is an Airworthiness Directive likely to follow?
About how many hours of labor will the recurrent inspection add to an
annual?
About how many hours of labor would be required to install the Piper
Service Kit (per wing)?
Any insights from other Piper owners and/or A&Ps would be appreciated.
-Elliott Drucker
BT
<e.dr...@nyetspam.verizon.net> wrote in message
news:ZIeWf.16307$W75.12066@trnddc07...
> I read where the inspections are required every 100hrs, and a repeat of
> the initial inspection every 500hrs.
The initial inspection requires the removal of the main gear side braces and
dye penetrant on the affected rib. This dye penetrant inspection is
"required" (bear in mind this is a SB, not an AD, so the "requirement" is
not a legal one) subsequently every 500 hours. However, the SB also calls
for a much simpler visual inspection, that does not require jacking or
removal of the side braces, every 100 hrs. I would guess that visual
inspection will take no more than 15 minutes or so. All requirements for
inspections go away if the service kit is installed.
-Elliott Drucker
Haven't seen anything on prevalence, just anecdotal from Cherokee
Pilots Assn - appears fairly common, but not universal.
e.dr...@nyetspam.verizon.net wrote:
> Last week I received a new Piper Service Bulletin, which seems to affect all
> older (pre 1983) retractable gear PA-28s (Arrow), PA-32s (Lance/Saratoga),
> PA-34s (Seneca),
Pre 83, I hope so. I read the bulletin and it mentions Seneca 4's and
5's. So why limit it to pre 83?
> Pre 83, I hope so. I read the bulletin and it mentions Seneca 4's and
> 5's. So why limit it to pre 83?
The SB lists possibly affected SNs for each model, rather than model year.
However, the affected ribs carry a date code of 8312 (12th week of 1982) or
lower. Of course, airplanes built for some time after that date might have
used older ribs in initial construction. And it's even POSSIBLE that a
newer airplane has had an older (salvage?) rib installed to repair damage.
But my guess is that the vast majority of pre-1983 Piper retracts are
affected, and the vast majority of post-1983 planes are not.
-Elliott Drucker
OK, hate to rain on the parade, but unless they have started re-using
or have had parts laying around for 22 years, my PA44-180, factory new
and built (reportedly) in Oct and Nov 05, is in the serial number
range for this SB. so it's not just pre-1983.
Feedback from a guy (Dick Russ) of the Cherokee Pilot's association is
that the inspection would take approximately two hours and the repair,
if needed, would be about 30 hours of labor plus $500 and change for the
kit.
I'll post more details on our estimate in a new thread.
If you're interested in pictures, drop me an e-mail. I have photos of
our cracks on the side of the ribs opposite the side brace bracket. I
can also send you a picture of what Dick Russ's cracked rib looked like.
His was on a Lance and he had one crack on the side brace/bracket side
of one rib.
--
Jack Allison
PP-ASEL-Instrument Airplane
Arrow N2104T
"When once you have tasted flight, you will forever walk the Earth
with your eyes turned skyward, for there you have been, and there
you will always long to return"
- Leonardo Da Vinci
(Remove the obvious from address to reply via e-mail)
> Feedback from a guy (Dick Russ) of the Cherokee Pilot's association is
> that the inspection would take approximately two hours and the repair,
> if needed, would be about 30 hours of labor plus $500 and change for the
> kit.
Well, I'm not sure I believe the two hour figure for the inspection. Seems
kind of optimistic for the actual inspection (dye penetrant) AND the time
for disassembling and reassembling the gear side brace on each wing. And
this assumes that the plane is already on jacks and that the gear has to be
swung anyway (i.e. during the annual). However, even if it's more like 3
hours it still would be hard to justify undertaking the 30 labor hr "repair"
prophylactically. But as your situation demonstrates, you sure want to
catch any cracks before they propagate to a point where repair is not
feasible.
-Elliott Drucker