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Forced Structure Maintenance Plan

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.

Item

No.

Detail

Inspection

Area

Description

Visual Inspection

N D I

Analysis

No.

Remark

Initial

Inspection

(FH)

Repeat

Interval

Initial

Inspection

(FH)

Repeat

Interval

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.

 

Introduction
Work Scope
SSI Selection
F M E C A
M T B F
Figure 1
RCMA Pt 1
Item Data
RCMA Pt 2
Answers
Inspections
Age Exploration
F S M P
Follow Up