Service difficulty reports · 8
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DU4R2007068Structure · damagedFOUND TRIMMED OUT AREA AT FS 157 ALONG THE AFT EDGE OF THE E/E BAY DOOR CUTOUT. REPAIRED BY FABRICATING AND INSTALLING REPAIR 22 BY 10.5 FROM 6AL-4V .032 IAW TIMCO REO-L00681 REV IR DATED 11/10/03 APPROVED BY FAA FORM 8110-3.SDR DU4R2007067Repair · damagedFOUND CORROSION BLEND OUTS AND EXISTING EXTERNAL REPAIRS ON LT HORIZONTAL STABILIZER INBD LEADING EDGE. REPAIRED BY FABRICATING AND INSTALLED REPAIRS 17-1/4 BY 5-1/2, 15 BY 4-1/2 AND 5-1/2 BY 5-1/2 FROM 6AL-4V032 AND 6.0 BY 6.0, 15-1/2 BY 5-1/4 AND 5-1/4 BY 5SDR DU4R2007066Repair · damagedFOUND CORROSION BLEND OUTS AND EXISTING EXTERNAL REPAIRS ON LT HORIZONTAL STABILIZER INBD LEADING EDGE. REPAIRED BY FABRICATING AND INSTALLED REPAIRS 5 BY 4 FROM 6AL-4V040 AND 6 BY 5 FROM 6AL-4V032 AS DIRECTED TIMCO RFTS 60030 AND REO-L00677 REV A DATED 10-3SDR DU4R2007065Angle · misinstalledFOUND INTERCOSTAL 22 IMPROPERLY FITTED FS 1155 TO FS 1175 LT. REPAIRED BY REMOVING ANGLE, TRIMMED REPAIR ANGLE 13-1/4 BY 3/4 BY 2-3/4 FROM 7075-T6 .071 AND INSTALLED IAW MD-80 SRM 51-30-2, 51-70-5 FIG 1.SDR DU4R2007064Cusp Web · corrodedFOUND CORRODED CUSP WEB AT LT O/B FS 1175. REPAIRED BY CUTTING OUT CORRODED SECTION FROM FS 1174 TO FS 1193. FABRICATED AND INSTALLED REPAIR CUSP WEB 21 BY 15 FROM 7075-T6 .025 IAW MD-80 SRM 51-70-4.SDR DU4R2007063Cusp Web · corrodedFOUND EXFOLIATED CORROSION AT LT O/B CUSP WEB FROM FS 1135 TO FS 1175. REPAIRED BY FABRICATING AND INSTALLING CUSP WEB REPAIR SECTION 4.5 BY 20.2 FROM 7075-T6 .063 IAW DC-9/MD-80 SRM 51-10-2, 51-10-3, 51-10-4 AND 53-14-3 FIG 12.SDR DU4R2007061Skin · corrodedFOUND PREV REPAIRED AREA AT FS 332 TO FS 355 BETWEEN L-23L AND L-26L. REPAIRED BY REMOVING SECTION OF SKIN AND 2 EXISTING REPAIRS IAW DC-9/MD-80 SRM 53-04 FIG 12C. FABRICATED AND INSTALLED SKIN REPAIR 31.75 BY 25.5 FROM 2024-T3 .050, 3 SKIN REPAIRS 17.75 BY SDR DU4R2007060Vent · corrodedS/O 244001 N/R 22938 N/R 22839 CORROSION ON I/B END OF EXISTING REPAIR ON AFT L/H WING VENT BOX REPAIRED BY REMOVING EXISTING DOUBLER, FLAP PEENED CORROSION IAW BWIA DWG BW-D9-57-A/5120 AND MD-80 MM 20-10-10. FABRICATED AND INSTALLED DOUBLER 41.9 X 3.5, FILLER