N288UP

Service difficulty reports · 300

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N288UP' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR UPS08M53781Splice · crackedINSPECTION TYPE:1C LT WING FIXED L/E SPLICE FOUND CRACKED AT STA 775 COMPARTMENT AREA. REMOVED, FABRICATED, AND INSTALLED SPLICE IAW DWG ARB3954 AND MD-11 SRM 51-33-01.Oct 8, 2008 · N288UP · Doug MD11F · Wing Miscellaneous StructureSDR UPS08M53628Splice · crackedINSPECTION TYPE:1C RT WING FIXED L/E COMPT APPROX STA 775 SPLICE FOUND CRACKED. REMOVED, FABRICATED, AND INSTALLED SPLICE IAW SGW ARB3954 AND MD-11 SRM 51-33-01.Oct 8, 2008 · N288UP · Doug MD11F · Wing Miscellaneous StructureSDR UPS08M53624Stringer · crackedINSPECTION TYPE:1C RT WING FIXED L/E BELOW NR 8 SLAT TRACK CUTOUT STRINGER FOUND CRACKED. REMOVED STRINGER, FABRICATED, AND INSTALLED IAW MD-11 SRM 51-33-01, 51-35-01 AND DWG 2933.Oct 8, 2008 · N288UP · Doug MD11F · Wing, Longeron/StringerSDR UPS08M53379Skin · crackedINSPECTION TYPE:N/A, DENT AND CRACK DAMAGE FOUND ON FUSELAGE SKIN AT STA 1741 TO STA 1761 L LT, LONGERON 38 AND 39. DAMAGED AREA TRIMMED OUT, LENGTH = 12" X WIDTH = 5.5" AND REPAIRED AS PER SRM 53-20-00 FIG 2, VOL I, REV 40, AND UPS EO MD11-5330-18894C.Sep 22, 2008 · N288UP · Doug MD11F · Fuselage Main, Plate/SkinSDR UPS08M53119Unknown · failedEMERGENCY POWER TEST FAIL. RESET CIRCUIT BREAKERS. OPS CHECK NORMAL.Aug 16, 2008 · N288UP · Doug MD11F · DC Generating SystemSDR UPS07M50070Floor Support · crackedINSPECTION TYPE:C CABIN, FLOOR SUPPORT STRUCTURE STA 1887 - 1902, RBL 18 INTERCOSTAL FOUND CRACKED. CRACK INTERCOSTAL AT CABIN FLOOR SUPPORT STRUCTURE STA 1887 TO 1902 RBL 18 AREA REMOVED. NEW STRUCTURE P/N AGA7408-27 FAB PER DWG AGA7408 INTERCOSTAL WEB HEATJun 8, 2007 · N288UP · Doug MD11F · Fuselage Miscellaneous StructureSDR UPS07M50069Intercostal · crackedINSPECTION TYPE:C CABIN - FLOOR SUPPORT STRUCTURE STA 1887 - 1902, LBL 18 INTERCOSTAL FOUND CRACKED. CRACK AREA TRIMMED OUT PER SRM 53-00-01 FIG 6 VOL I REV38. HFEC INSP C/OUT FOUND 2 CRACKS APPROX 1" EACH. CRACK AREAS TRIMMED OUT PER SRM 53 -00-01 FIG 6 VOJun 8, 2007 · N288UP · Doug MD11 · Fuselage Miscellaneous StructureSDR UPS07M50155Web · crackedINSPECTION TYPE:C RIGHT WINGTIP LOWER WINGLET LOWER STRUCTURAL BORE FOUND CRACK. WEB CRACK END STOP HOLE DRILLED PER EN 1350-07. CRACK BOLT HOLE REAMED PER EN 1350-07. REP BUSHING FAB & INSTALLED PER EN 1350-07. FPI CARRIED OUT AS PER DPS 4.707 REV AW ON FMay 29, 2007 · N288UP · Doug MD11F · Wing Miscellaneous StructureSDR UPS07M50115Structure · corrodedINSPECTION TYPE:C LT HORIZONTAL STABILIZER BARREL NUT NR 25 BORE FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED, REMAINING BLEND OUT FOUND EXCEEDING LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOIDS AND BOTTOM PERIPHERY RADIUSED SMMay 28, 2007 · N288UP · Doug MD11 · Horizontal Stabilizer StructureSDR UPS07M50114Structure · corrodedINSPECTION TYPE:C LT HORIZONTAL STABILIZER BARREL NUT HOLE NR 22 BORE FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED, REMAINING BLEND OUT FOUND EXCEEDING LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOIDS AND BOTTOM PERIPHERY RADIUSMay 28, 2007 · N288UP · Doug MD11 · Horizontal Stabilizer StructureSDR UPS07M50108Structure · corrodedINSPECTION TYPE:C RT HORIZONTAL STABILIZER BARREL NUT HOLE NR 16 BORE FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED, REMAINING BLEND OUT FOUND EXCEEDING LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOID AND BOTTOM PERIPHERY RADIUSEMay 22, 2007 · N288UP · Doug MD11 · Horizontal Stabilizer StructureSDR UPS07M50107Structure · corrodedINSPECTION TYPE:C RT HORIZONTAL STABILIZER BARREL NUT HOLE NR 7 BORE FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED, REMAINING BLEND OUT FOUND EXCEEDING LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOID AND BOTTOM PERIPHERY RADIUSEDMay 22, 2007 · N288UP · Doug MD11 · Horizontal Stabilizer StructureSDR UPS07M50113Structure · corrodedINSPECTION TYPE:C RT HORIZONTAL STABILIZER BARREL NUT HOLE NR 22 BORE FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED, REMAINING BLEND OUT FOUND EXCEEDING LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOID AND BOTTOM PERIPHERY RADIUSEMay 21, 2007 · N288UP · Doug MD11 · Horizontal Stabilizer StructureSDR UPS07M50106Structure · corrodedINSPECTION TYPE:C RT HORIZONTAL STABILIZER BARREL NUT HOLE NR 19 BORE FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED, REMAINING BLEND OUT FOUND EXCEEDING LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOID AND BOTTOM PERIPHERY RADIUSEMay 21, 2007 · N288UP · Doug MD11 · Horizontal Stabilizer StructureSDR UPS07M50112Structure · corrodedINSPECTION TYPE:C LT HORIZONTAL STABILIZER BARREL NUT HOLE NR 23 BORE FOUND CORRODED. CORROSION AT BARREL NUT BORE REMOVED, REMAINING BLEND OUT FOUND EXCEEDING LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOID AND BOTTOM PERIPHERY RADIUSEMay 15, 2007 · N288UP · Doug MD11 · Horizontal Stabilizer StructureSDR UPS07M50105Structure · corrodedINSPECTION TYPE:C LT HORIZONTAL STABILIZER BARREL NUT HOLE NR 36 FOUND CORRODED. ACCESS CUT AT UPPER TORQUE BOX WEB. CORROSION AT BARREL NUT BORE REMOVED, REMAINING BLEND OUT FOUND EXCEED LIMITS. DVI C/OUT FOUND NO CORROSION. REPAIR SLEEVE BUSHING, DOUBLERMay 11, 2007 · N288UP · Doug MD11 · Horizontal Stabilizer StructureSDR UPS07M50111Structure · corrodedINSPECTION TYPE:C RT HORIZONTAL STABILIZER BARREL NUT NR 23 FOUND BORE CORRODED. CORROSION AT BARREL NUT BORE REMOVED, REMAINING BLEND OUT FOUND EXCEEDING LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOID AND BOTTOM PERIPHERY RADIUSED SMOMay 10, 2007 · N288UP · Doug MD11 · Horizontal Stabilizer StructureSDR UPS07M50110Structure · corrodedINSPECTION TYPE:C LT HORIZONTAL STABILIZER BARREL NUT NR 30 FOUND BORE CORRODED. CORROSION AT BARREL NUT BORE REMOVED, REMAINING BLEND OUT FOUND EXCEEDING LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOIDS AND BOTTOM PERIPHERY RADIUSED SMMay 10, 2007 · N288UP · Doug MD11 · Horizontal Stabilizer StructureSDR UPS07M50104Structure · corrodedINSPECTION TYPE:C RT HORIZONTAL STABILIZER BARREL NUT NR 20 FOUND BORE CORRODED. CORROSION AT BARREL NUT BORE REMOVED, REMAINING BLEND OUT FOUND EXCEEDING LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOID AND BOTTOM PERIPHERY RADIUSED SMOMay 10, 2007 · N288UP · Doug MD11 · Horizontal Stabilizer StructureSDR UPS07M50073Web · crackedINSPECTION TYPE:C COCKPIT, 1ST OBSERVER SEAT SUPPORT WEB FOUND CRACKED. COCKPIT 1ST OBS SEAT SUPPORT WEB CRACKED AREA TRIMMED OFF PER SRM 53-00-01 VOLI REV 39. HFEC INSP C/OUT ON TRIMMED OFF AREA, NO CRACK REINFORCED DOUBLER FAB PER SRM 53-00-01 VOLI FIG 6 RMay 8, 2007 · N288UP · Doug MD11 · Fuselage Main, StructureSDR UPS07M50101Structure · corrodedINSPECTION TYPE:C EMPENNAGE/LT HORIZONTAL STABILIZER BARREL NUT NR 24 LT FOUND BORE CORRODED. CORROSION AT BARREL NUT BORE REMOVED, BOTTOM REMAINING BLEND OUT EXCEEDS LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOIDS AND BOTTOM PERIPHERYMay 7, 2007 · N288UP · Doug MD11 · Horizontal Stabilizer StructureSDR UPS07M50100Structure · corrodedINSPECTION TYPE:C EMPENNAGE/LT HORIZONTAL STABILIZER BARREL NUT NR 15 LT FOUND BORE CORRODED. CORROSION AT BARREL NUT BORE REMOVED, BOTTOM REMAINING BLENDED OUT EXCEEDS LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUTS AND BOTTOM PERIPHERY RAMay 7, 2007 · N288UP · Doug MD11 · Horizontal Stabilizer StructureSDR UPS07M50099Structure · corrodedINSPECTION TYPE:C EMPENNAGE/LT HORIZONTAL STABILIZER BARREL NUT NR 9 LT FOUND BORE CORRODED. CORROSION AT BARREL NUT BORE REMOVED, BOTTOM REMAINING BLENDED OUT EXCEEDS LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT VOID AND BOTTOM PERIPHERYMay 7, 2007 · N288UP · Doug MD11 · Horizontal Stabilizer StructureSDR UPS07M50109Structure · corrodedINSPECTION TYPE:C RT HORIZONTAL STABILIZER BARREL NUT NR 2 RT FOUND BORE CORRODED. CORROSION AT BARREL NUT BORE REMOVED, REMAINING BLEND OUT FOUND EXCEEDING LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT AND BOTTOM PERIPHERY RADIUSED SMOOTHMay 6, 2007 · N288UP · Doug MD11 · Horizontal Stabilizer StructureSDR UPS07M50098Structure · corrodedINSPECTION TYPE:C EMPENNAGE/RT HORIZONTAL STABILIZER BARREL NUT NR 15 RT FOUND BORE C CORRODED. CORROSION AT BARREL NUT BORE REMOVED, BOTTOM SURFACE REMAINING BLEND OUT FOUND EXCEEDING LIMITS. DVI C/OUT FOUND NO CORROSION. BARREL NUT BORE BLEND OUT, BOTTOM May 6, 2007 · N288UP · Doug MD11 · Horizontal Stabilizer StructureSDR UPS07M50071Doubler · crackedINSPECTION TYPE:C RT WING, FIXED L/E INTERIOR FOUND BEADED DOUBLER CRACKED BETWEEN XOS 698 TO XOS 703 AS MARKED. RIBS AT RHW FIXED L/E REPAIR AREA REMOVED. CRACK AREA TRIMMED OFF PER SRM 57-10-00 FIG 27 VOLI REV 39. HFEC INSP C/OUT ON TRIMMED OFF AREA FOUNDMay 5, 2007 · N288UP · Doug MD11 · Leading Edge DevicesSDR UPS07M49819Attach Angle · crackedINSPECTION TYPE:C COCKPIT - STA 383 - 401 APPROX LBL 4 WEB P/N: ABA7121-25 & ABA7121-39 CLIP ANGLE FOUND CRACKED. ATTACH CRACK INTERCOSTAL FASTENERS & INNER SUPPORT PARTS REMOVED PER SRM 51-31-01 VOL 2 REV 38. NEW INTERCOSTAL P/N:ABA7121-25 & CLIP ABA7121- 3May 4, 2007 · N288UP · Doug MD11F · Fuselage Main, Attach FittingsSDR UPS07M50157Doubler · crackedINSPECTION TYPE:C RIGHT WING L/E COMPARTMENT AT STA XORS 550 APPROX FOUND UPPER SKIN DOUBLER CRACKED AS MARKED. DAMAGED AREA AT RIGHT WING L/E COMPT AT STA XORS 550 APPROX, UPPER SKIN DOUBLER AREA TRIMMED OUT AS PER SRM 57-10-00 V.I FIG 27 IAW EN 1294-07. HFApr 25, 2007 · N288UP · Doug MD11F · Wing, Plate/SkinSDR UPS07M50139Doubler · crackedINSPECTION TYPE:C LEFT LEADING EDGE LWR COMPT 519CB (PRESSURE REFUEL) FOUND STIFFENER DOUBLER SUSPECTED CRACK AS MARKED. HFEC INSP CUTOUT FOUND CRACK APPROX .25 INCH. LEFT WING LEADING EDGE LWR COMPT 519CB (PRESS REFUEL) RIBS REMOVED. CRACK AREA TRIMMED OUTApr 24, 2007 · N288UP · Doug MD11F · Wing Miscellaneous StructureSDR UPS07M50117Stiffener · crackedINSPECTION TYPE:C LT LE LWR COMPT ACCESS NR 519DB FOUND STIFFENER DOUBLER SUSPECTED CRACK AS MARKED, JUST O/B OF REFUEL PNL NR 519CB. HFEC INSP C/OUT FOUND CRACK APPROX 1/4". LT LE LWR COMPT ACCESS NR 51 9DB CLAMPS REMOVED. DAMAGED AREA AT LT LE LWR COMPT NApr 24, 2007 · N288UP · Doug MD11 · Wing Miscellaneous StructureSDR UPS07M50116Hinge · corrodedINSPECTION TYPE:C RT O/B FLAP I/B AFT HINGE LOWER BORE (02EA) FOUND RUSTY. RT AFT O/B FLAP I/B HINGE PIVOT I/B AND O/B BORE BUSHING REMOVED. SPOT FACE CORROSION REMOVED FOUND EXCEED LIMIT. FPI C/OUT ON REWORK AREA FOUND NO CORROSION AND NO CRACK. REWORK ARApr 24, 2007 · N288UP · Doug MD11 · Trailing Edge FlapsSDR UPS07M50125Rib · crackedINSPECTION TYPE:C RIGHT WING L/E SLAT TRACK NR 16 I/B SUPPORT RIB FOUND CRACK. RIGHT WING L/E SLAT TRACK NR 16 ATTACHING PARTS & WIRE HARNESS REMOVED. NR 16 CRACK I/B SUPPORT RIB REMOVED. HOLES TRANSFERRED TO NEW NR 16 RIB ASSY. RIGHT WING L/E SLAT TRACK NApr 18, 2007 · N288UP · Doug MD11F · Wing, Rib/BulkheadSDR UPS07M50074Rib · deformedINSPECTION TYPE:C RT WING LOWER SURFACE FIXED L/E COMPARTMENT BETWEEN STA XOS 657 AND XO S 714 APPROX FOUND 04 SUPPORT RIB DEFORMED. 4 SUPPORT DEFORMED RIBS REMOVED. NEW SUPPORT RIBS FAB PER DWG ARB2924-8, ARB2924-6, ARB2924-4 AND ARB2930-16. RIBS HEAT TREAApr 18, 2007 · N288UP · Doug MD11 · Wing, Rib/BulkheadSDR UPS07M50144Skin · dentedINSPECTION TYPE:C RIGHT WING UPPER SURFACE FIXED L/E STRUCTURE FOUND DEEP DENT AT STA XORS 593 AREA. RIGHT WING L/E COMPT RIBS 4EA REMOVED. RIGHT WING L/E DAMAGED SKIN TRIMMED PER EN12 63-07. HFEC INSP CUT OUT ON TRIMMED OFF AREA, FOUND NO CRACK. REPAIR SKApr 16, 2007 · N288UP · Doug MD11F · Wing, Plate/SkinSDR UPS07M50061Longeron · crackedINSPECTION TYPE:C CTR CARGO COMPT AT STATION 5-128 LONGERON 45 LT FOUND SUSPECTED CRACKED ON DOUBLER AREA AS MARK. HFEC INSP C/OUT PER DAC NDT SPM REV 13 PART 06-10-01-001 ON DOUBLER FOUND CRACK. CRACK LONGERON SPLICE AT CTR CARGO STA 5-128 L45 LT REMOVED. Apr 16, 2007 · N288UP · Doug MD11 · Fuselage Main, Longeron/StringerSDR UPS07M50059Longeron · crackedINSPECTION TYPE:C CTR CARGO COMPT AT STATION 5-128 LONGERON 43 RT FOUND SUSPECTED CRACK ON DOUBLER AREA AS MARKED. HFEC INSP C/OUT PER DAC NDT SPM REV 13 PART 06-10-01-001 ON DOUBLER FOUND CRACK. CRACK LONGERON SPLICE AT CTR CGO STA5-128 L43RH REMOVED. NEW Apr 16, 2007 · N288UP · Doug MD11 · Fuselage Main, Longeron/StringerSDR UPS07M50072Web · crackedINSPECTION TYPE:C AFT FUSELAGE COMPARTMENT HAS UPPER TORQUE BOX WEB CRACKED AT STA 2015 APPROX RBL 25 AT MAN HOLE ACCESS CUTOUT STICKER 8344. AFT FX COMPT STA2015 APPROX RBL 25 UPP TORQUE BOX WEB CRACK AREA ATTACHING PARTS REMOVED. HFEC INSP C/OUT FOUND CRACApr 14, 2007 · N288UP · Doug MD11 · Fuselage Miscellaneous StructureSDR UPS07M49818Intercostal · crackedINSPECTION TYPE:C CABIN - INTERCOSTAL FOUND CRACKED AT L7 RIGHT STA 5-53 TO 5-73. EXISTING INTERCOSTAL & ATTACHED PARTS AT L7 RIGHT STA 5-53 TO 5-73 REMOVED PER SRM 51-31-01 VOL 2 REV 38. INTERCOSTAL P/N:A5A7071-10, FAB PER BOEING DWG A5A7071. INTERCOSTAL HApr 14, 2007 · N288UP · Doug MD11F · Fuselage Miscellaneous StructureSDR UPS07M49817Intercostal · crackedINSPECTION TYPE:C CABIN - INTERCOSTAL FOUND CRACKED AT L7 RIGHT STA 1541 - 1561. EXISTING INTERCOSTAL & ATTACHED PARTS STA 1541-1561 L7 LEFT REMOVED PER SRM 51-31-01 VOL 2 REV 38. INTERCOSTAL P/N AFA7761-9 FAB PER BOEING DWG AFA7761 REV D. INTERCOSTAL HEAT Apr 14, 2007 · N288UP · Doug MD11F · Fuselage Miscellaneous StructureSDR UPS07M49816Intercostal · crackedINSPECTION TYPE:C CABIN - INTERCOSTAL FOUND CRACKED AT L7 RIGHT STA 1661 - 1681. EXISTING INTERCOSTAL & ATTACH PARTS L7 RIGHT STA 1661-1681 REMOVED PER SRM 51-31-01 VOL 2 REV 38. INTERCOSTAL P/N:AFA7761-21 FAB PER BOEING DWG AFA7761 REV D. INTERCOSTAL HEAT Apr 14, 2007 · N288UP · Doug MD11F · Fuselage Miscellaneous StructureSDR UPS07M49815Seat Track · corrodedINSPECTION TYPE:C CABIN - CORROSION ON SEAT TRACK CROWN AT STA 1351 X=-75.0. SEAT TRACK CORROSION REMOVED FOUND EXCEEDED LIMITS PER SRM 53-70-00 FIG 3 REV 38 VOL 1. SEAT TRACK ATTACHED PARTS STA 1264-1391 X=-75 REMOVED PER SRM 51-31-01 VOL 2 REV 38. CORRODEApr 12, 2007 · N288UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR UPS07M50156Seat Track · corrodedINSPECTION TYPE:C MID CABIN - CORROSION ON SEAT TRACK CROWN AT STA 909 X=-75.0. CABIN STA 909 X=-75 SEAT TRACK BASE CORROSION REMOVED & REPROTECTED PER SRM 53-70-00 FIG 3 V.I R.39 & SRM 51-21-01 V.II R.39. CABIN STA 909.6 X =-75 SEAT TRACK CROWN CORROSION REApr 9, 2007 · N288UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR UPS07M50154Seat Track · corrodedINSPECTION TYPE:C AFT CABIN - CORROSION ON SEAT TRACK CROWN & FLANGE AT STA 1966 X=107. CURVE SEAT TRACK ATTACHMENT & ATTACHED PARTS AT STA 1831-2007 X=107 LEFT REMOVED PER SRM 51-31-01 V.II R.39. CLEAN UP REWORKED AREA PER SRM 51-21- 01 V.II R.39. NEW SEATApr 9, 2007 · N288UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR UPS07M49814Seat Track · corrodedINSPECTION TYPE:C AFT CABIN CORROSION ON SEAT TRACK CROWN & FLANGE AT STA 1966 X=-107. RIGHT NR 4 PASSENGER DOOR SILL REMOVED. REMOVED SEAT TRACK & ATTACH PARTS STA 1831-2007 RBL 107 PER SRM 51-31-01 VOL 2 REV 38. CORRODED SEAT TRACK TRIMMED OFF. HFEC INSPApr 9, 2007 · N288UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR UPS07M49795Seat Track · corrodedINSPECTION TYPE:C MID CABIN - CORROSION ON SEAT TRACK CROWN & FLANGE AT STA 859 - 899 X= -8.0. SEAT TRACK PARTS REMOVED PER SRM 51-31-01 VOL 2 REV 38. CORRODED SEAT TRACK TRIMMED OFF PER SRM 53-70-00 FIG 1 VOL 1 REV 38. HFEC INSP CUTOUT & FOUND NO CRACK. CApr 9, 2007 · N288UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR UPS07M49794Seat Track · corrodedINSPECTION TYPE:C MID CABIN - CORROSION ON SEAT TRACK CROWN AT STA 859 & STA 891 X=8.0. REMOVED SEAT TRACK PER SRM 51-31-01 VOL 2 REV 28. CORRODED SEAT TRACK TRIMMED OFF PER SRM 53-70-00 FIG 1 VOL 1 REV 38. HFEC INSP CUTOUT & FOUND NO CRACK. CORRODED SEAT Apr 9, 2007 · N288UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR UPS07M50060Longeron · crackedINSPECTION TYPE:C CTR CARGO COMPT AT STA 5-128 LONGERON 45 RT FOUND SUSPECTED CRACKED ON DOUBLER AREA. HFEC INSP C/OUT PER DAC NDT SPM REV 13 PART 06-10-01-001 ON DOUBLER FOUND CRACK. CRACK LONGERON SPLICE AT CTR CGO STA 5-128 L45R REMOVED. NEW SPLICE P/N Apr 6, 2007 · N288UP · Doug MD11 · Fuselage Main, Longeron/StringerSDR UPS07M50058Skin · damagedINSPECTION TYPE:C RHW, INBD FLAP LOWER AFT INBD AND OUTBD SEGMENTS NEED RE-SKIN. RHW I/B FLAP LWR AFT I/B AND O/B SEGMENTS REMOVED. RHW RELATED PARTS AND I/B FLAP I/B AND O/B SEGMENTS LWR SKINS REMOVED. NEW SKINS FAB PER DWG ARC2736 AND ARC2444. NEW SKINS Mar 28, 2007 · N288UP · Doug MD11 · Trailing Edge FlapsSDR UPS07M50046Skin · damagedINSPECTION TYPE:C LTW, INBD FLAP LOWER AFT INBD AND OUTBD SEGMENTS NEED RE-SKIN. LHW I/B FLAP LWR AFT I/B AND O/B SEGMENTS REMOVED. DAMAGED SKIN REMOVED. NEW SKIN FAB PER DWG ARC2736. NEW SKIN PROTECTED, PAINTED AND INSTALLED. LHW I/B FLAP O/B SEGMENT FABMar 28, 2007 · N288UP · Doug MD11 · Trailing Edge FlapsSDR UPS07M49813Door Frame · damagedINSPECTION TYPE:C AFT CARGO DOOR FWD AND AFT JAMBS HAS SCALLOPED IN SEVERAL AREA. REMOVED HEAT DUCT ON AFT CARGO STA 1926 PER AMM20-50-02 REV 50. FWD & AFT JAMB FASTENERS REMOVED PER SRM 51-31-01 VOL 2 REV 38. HFEC INSP CUT OUT FOUND NO CRACK. REPAIR DOUBLMar 28, 2007 · N288UP · Doug MD11F · Fuselage Main, Structure
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