by Zach Grant L1011jock » Mon Jan 28, 2013 4:29 am
Ray,
In the instance you cite, the 5 year, 500 hr, or 100 hrs after Oct 22, 2012, whichever is later, would only apply if there was a used servicable horn installed prior to the effective date of the AD. This is different from inspecting the existing horn as the existing horn was probably installed new during production (and would fall under part 1). How it is different I don't know but the FAA saw fit to make the distinction. It probably has to do with the fact that it would be impossible to inspect as per the SB 1189 before that SB was actually published. They gave us an out for that in section two I believe. In my best legal opinion thinking like a Fed, if you inspected prior to the release of SB 1189 dated 29 April 2010, then you would have had to install a used servicable horn assembly (even if it was the same part that was removed from your airplane). After that date, if you reinstalled the existing horn, the horn would have been the same one as installed new, inspected IAW SB 1189, and thusly compliant with this AD, and would subsequantly be covered under the repetitive inspection requirements of the AD. You would have inspected your horn as per SB 1189, not replaced with a used servicable horn, and would not fall under part 2, but rather the simple 5 yr or 500 hour reinspection requirement found in (1) (i). Note also that part (j) (2) requires that the only acceptable stated method of compliance with the inspection requirements of this AD are contained in Piper SB 1189. The referenced sections are attached below. -Zach
(1) When a new stabilator horn assembly has been installed (during production or replacement)and the stabilator horn assembly reaches a total of 1,000 hours time-in-service (TIS) or 10 years after
installation, or within the next 100 hours TIS after October 22, 2012 (the effective date of this AD),
whichever occurs later, do one of the following actions:
(i) Initially inspect the stabilator horn assembly for corrosion or cracks. Repetitively thereafter
inspect at intervals not to exceed 500 hours TIS or 5 years, whichever occurs first.
(ii) Replace the stabilator horn assembly with a new stabilator horn assembly. When the new
stabilator horn assembly reaches a total of 1,000 hours TIS after replacement or within 10 years after
replacement, whichever occurs first, you must do one of the actions in paragraph (g)(1) of this AD.
(iii) Replace the stabilator horn assembly with a used serviceable stabilator horn assembly that
has been inspected before installation and found free of cracks or corrosion. Repetitively thereafter
inspect at intervals not to exceed 500 hours TIS or 5 years, whichever occurs first.
(2) When a used serviceable stabilator horn assembly that has been inspected before installation
and found free of cracks or corrosion has been installed and the stabilator horn assembly reaches a
total of 500 hours TIS or 5 years after installation, or within the next 100 hours TIS after October 22,
2012 (the effective date of this AD), whichever occurs later, do one of the following actions:
(i) Initially inspect the stabilator horn assembly for corrosion or cracks. Repetitively thereafter
inspect at intervals not to exceed 500 hours TIS or 5 years, whichever occurs first.
(ii) Replace the stabilator horn assembly with a new stabilator horn assembly. When the new
stabilator horn assembly reaches a total of 1,000 hours TIS after replacement or within 10 years after
replacement, whichever occurs first, you must do one of the actions in paragraph (g)(1) of this AD.
(iii) Replace the stabilator horn assembly with a used serviceable stabilator horn assembly that
has been inspected before installation and found free of cracks or corrosion. Repetitively thereafter
inspect at intervals not to exceed 500 hours TIS or 5 years, whichever occurs first.
(j) Material Incorporated by Reference
(1) The Director of the Federal Register approved the incorporation by reference (IBR) of the
service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do the actions required by this AD,
unless the AD specifies otherwise.
(i) Piper Aircraft, Inc. Service Bulletin No. 1189, dated April 29, 2010.
(ii) Reserved.
"Keep it above 5 feet and don't do nuthin dumb!"