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All damage tolerance critical structure parts are listed in the Forced Structure Maintenance Program (FSMP). These items were listed by ADD prior to the RCMA.
The initial visual inspections identified by RCMA shall be used in the FSMP. Specific non-destructive inspection (NDI) requirements to be identified by this analyst's ADD counterpart at a later date.
ItemNo. |
Detail
InspectionArea |
Description |
Visual Inspection |
N D I |
AnalysisNo. |
Remark |
||
Initial Inspection(FH) |
RepeatInterval |
Initial Inspection(FH) |
RepeatInterval |
|||||
1 |
330/350 |
Rivet
holes of cap,fr lwr spar cap/ splicer attachment Stbd/BL0-BL70 |
|
|
|
25,000 |
HS-6-01-02 |
81551301-01 81551301-02 |
2 |
330/350 |
Rivet
holes of connector,fr lwr spar cap/ splicer attachment. Stbd/BL0-BL70 |
|
|
|
25,000 |
HS-6-01-03 |
81551303-01 |
3 |
330/350 |
Port/Stbd
rear fitting holes, fuselage/horizontal tail attachment, FS9802 |
|
|
|
25,000 |
HF-8-02-01 |
81534472-01 81534473-01 |
4 |
280 |
Front
stiffener holes, fuselage/ horizontal tail attachment, FS9361 |
|
|
|
25,000 |
HF-8-01-01 |
81534453-01 |
NOTE: Items #1 and #2 are not Damage Tolerance Critical per ADD analysis,
but it is deemed prudent to add
them to the FSMP due to the criticality of the end effect of the functional
loss of the Horizontal Stabilizer. |
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