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Boeing SB A3515: Revision 1

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Copy · U.S. DOT/FAA - SB-707-00A3515-01 · 38 pages

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© The Boeing Company. Filed by the FAA in regulations.gov docket FAA-2015-2965; AD 2016-08-11 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.

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Page 37Open in PDF

The step numbers shown below agree with the numbers shown in the circle symbols in the figure.

MORE DATAQTYIDENTIFICATIONNAMETASKSTEP

(a) (b)2-Forward Skin FlangeInspect1

(a) Do a Low Frequency Eddy Current (LFEC) inspection of the left and right side horizontal stabilizer rear spar lower inboard chord forward skin flange between stabilizer station -13.179 and 92.55 for any cracking in accordance with 707, 720 NDT, Part 6, 55-10-07, Figure 8.

(b) Exclude inspection of areas not accessible due to interference with any vortex generators mounted on the lower surface. However, if any cracks are found at any of the first six (6) inspectable fasteners on either side of the vortex generator, remove the vortex generator and inspect all fastener locations.

FIGURE 6: HORIZONTAL STABILIZER - REAR SPAR - LOWER INBOARD CHORD - FORWARD SKIN FLANGE - STABILIZER STATION -13.179 TO STABILIZER STATION 92.55 - INSPECTION (SHEET 1 OF 1) Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.

Original Issue: December 19, 2007 A3515Revision 1 October 10, 2014 37 of 38 BOEING SERVICE BULLETIN A3515

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Page 38Open in PDF

FLIGHT CYCLES:FLIGHT HOURS:AIRPLANE REGISTRY:

LEFT SIDE Horizontal Stabilizer Stabilizer Serial Number (a):Stabilizer Part Number (a):

Spar Chord Material (b): (from Part 2 - Configuration Check) LocationSpar Chord Segment Side of Body to SSTA 182.55Upper Inboard Side of Body to SSTA 182.55Lower Inboard SSTA 182.55 to Stabilizer TipUpper Outboard SSTA 182.55 to Stabilizer TipLower Outboard RIGHT SIDE Horizontal Stabilizer Stabilizer Serial Number (a):Stabilizer Part Number (a):

Spar Chord Material (b) (from Part 2 - Configuration Check) LocationSpar Chord Segment Side of Body to SSTA 182.55Upper Inboard Side of Body to SSTA 182.55Lower Inboard SSTA 182.55 to Stabilizer TipUpper Outboard SSTA 182.55 to Stabilizer TipLower Outboard Record the horizontal stabilizer part number and serial number as recorded on the data plate.

(a) Record spar chord material, 7079-T6 or 7075-T73511, as determined from maintenance record review, or electrical conductivity test. Do the electrical conductivity test in accordance with 707 Non-Destructive Testing (NDT) Manual D6-48023 Part 6, 51-00-00, Figure 20, dated April 5, 2004, and Boeing Process Specification BAC5946, Table I, Page 12, Revision (AA) dated July 9, 2001.

(b) Comments:

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Appendix A: CONFIGURATION VERIFICATION - INSPECTION RESULTS FORM - MATERIAL DATA (SHEET 1 OF 1) Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.

Original Issue: December 19, 2007 A3515Revision 1 October 10, 2014 38 of 38 BOEING SERVICE BULLETIN A3515

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