12-A-052030-A-S4080-79203-A-01-1
Structural component listed in
para 2
Perform those parts of SB 04-009
(latest revision) that affect
this component
SB 04-009 successfully
completed and S/N specific
release statement available for
this component?
Establish a tracking system for
this component (see FAA AC
120.93 App. 7 Part 43 §43.9)
Continue operation up to the
life limit or SSID threshold
inspection (whichever comes first)
Start the Supplemental
Structural Inspection Programm
(SSIP) as defined in AMM Ch.04
and perform the required initial
inspections and reviews
S/N specific release statement
available for this component?
Continue operation up to the
life limit or LOV, whichever
comes first, i.a.w the SSID.
Component must stay on the
original aircraft, or be scrapped
Scrap the component
yes
1
no
no
yes
yes
2
3
4
5
6
7
8
no
Figure 1 Serialized Structural Components - LEP Flowchart(1of1)
PC-12/47E AMM Doc No 02300, ISSUE 01 REVISION 27 MSN 545, 1001-1719, 1721-1942
12-B-AM-00-00-00-I
UNCLASSIFIED
Effectivity: All
12-B-05-10-30-00A-010A-A
UNCLASSIFIED
19.07.2017 Page 5