# SDR UIEA2021030100433

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: March 9, 2021
- Submitted: March 12, 2021
- Operation: Air carrier
- Aircraft: [N1013A](https://openairdocs.org/aircraft/N1013A), registered now
- Make and model: Boeing 767-36N
- Registry model: [Boeing 767-36N](https://openairdocs.org/model/boeing-767-36n) (OpenAirDocs)
- Aircraft serial: 30110
- Aircraft time: 82,327 hours, 11,845 cycles
- System (JASC): [5330 · Fuselage Main, Plate/Skin](https://openairdocs.org/jasc/5330)
- Part: Skin
- Condition: Cracked
- Location: Fuselage
- Stage of operation: IN
- How discovered: E
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/UIEA2021030100433

## Discrepancy

UPPER FUSELAGE DURING HFEC FOUND CRACKS BETWEEN RIVETS ON I/B SIDE OF ELT ANTENNA CUT OUT. NOTE OUTER SKIN(<DIV> / </DIV><P STYLE="MARGIN:0IN;MARGIN-BOTTOM:.0001PT"><SPAN>COMPLIED WITH WORK INSTRUCTIONS / BELOW AND EO6753A923</SPAN></P><P CLASS="XXMSOLISTPARAGRAPH" STYLE="MARGIN: 0IN 0IN 0.0001PT;"><SPAN>1.     REMOVE AND DISCARD THE EXISTING / ANTENNA DOUBLER FOUND BETWEEN DOOR FRAME STATION STA911 AND STA923.7,</SPAN></P><P CLASS="XXMSOLISTPARAGRAPH" STYLE="MARGIN: 0IN 0IN 0.0001PT;"><SPAN>2.     REMOVE THE ELT TRAY (INTERCOSTAL) / BETWEEN BSTA 1540 TO 1562 ATTACH SERVICEABLE TAG AND ROUTE TO STORES</SPAN></P><P CLASS="XXMSOLISTPARAGRAPH" STYLE="MARGIN: 0IN 0IN 0.0001PT;"><SPAN>3.     REMOVE ELT TRAY (INTERCOSTAL) / ATTACH BRACKET AT BSTA 1540 AND 1562 ATTACH SERVICEABLE TAG AND ROUTE TO STORES</SPAN></P><P CLASS="XXMSOLISTPARAGRAPH" STYLE="MARGIN: 0IN 0IN 0.0001PT;"><SPAN>4.     AT BOTH REMOVED BRACKET LOCATION / OF THE FRAME AT BSTA 1540 AND 1562 ACCOMPLISH OPEN HOLE HFEC INSPECTION FOR NO / CRACK CONDITION  </SPAN></P><P CLASS="XXMSOLISTPARAGRAPH" STYLE="MARGIN: 0IN 0IN 0.0001PT;"><SPAN>5.     ON BOTH FRAMES BSTA 1540 AND 1562 /  INSTALL PLUG RIVET AT THE OPEN HOLES AS PER B767-300 SRM 53-00-07-1A-1, / NOTE D</SPAN></P><P CLASS="XXMSOLISTPARAGRAPH" STYLE="MARGIN: 0IN 0IN 0.0001PT;"><SPAN>6.     TRIM THE REPORTED DAMAGE AREA BY / INCLUDING THE EXISTING ANTENNA INSTALLATION FOOTPRINT IN RECTANGULAR PATTERN /  BY MAINTAINING MINIMUM MATERIAL REMOVAL WITH 1 INCH MINIMUM CORNER RADIUS</SPAN></P><P CLASS="XXMSOLISTPARAGRAPH" STYLE="MARGIN: 0IN 0IN 0.0001PT;"><SPAN>7.     INSTALL REPAIR AS PER B767-</SPAN><SPAN>300 SRM <A HREF="HTTP://" TARGET="_BLANK" TITLE="THIS EXTERNAL LINK WILL OPEN IN A NEW WINDOW"><SPAN STYLE="COLOR: WINDOWTEXT; TEXT-DECORATION-LINE: NONE;"><SPAN>53-00-01-2R-1 / REPAIR 1 - FUSELAGE SKIN - EXTERNAL REPAIR AT A STRINGER</SPAN></SPAN></A></SPAN></P><P CLASS="X_X_MSOLISTPARAGRAPH"><A HREF="HTTP:" TITLE="THIS EXTERNAL LINK WILL OPEN IN A NEW WINDOW" REL="NOOPENER NOREFERRER" TARGET="_BLANK" STYLE="COLOR: #0066CC; TEXT-DECORATION-LINE: NONE; OUTLINE: NONE;" DATA-MCE-HREF="HTTP:"><SPAN STYLE="COLOR: #1F497D;"></SPAN></A></P>)

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