Mcdonnell Douglas MD-11

Service difficulty reports · 7,956

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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 aircraft_model_key = 'MD11'
  ORDER BY difficulty_date DESC"

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SDR UPS08M52355Skin · crackedINSPECTION TYPE:C LEFT WING L/E FIXED WING AFT SKIN APPROX STA XORS 522 FOUND CRACKED (2478). ATTACHED RIBS 2 EA REMOVED. INNER SKIN BEADED SKIN TRIM OFF. HFEC INSP C/O ON TRIM OUT AREA, FOUND NO CRACK EVIDENT. THREE EA REPAIR ANGLES, REPAIR DOUBLERS & FILApr 10, 2008 · N295UP · Doug MD11 · Wing, Plate/SkinSDR UPS08M52430Bushing · damagedINSPECTION TYPE:C CLG RT TRUNNION FITTING AFT HOLE FOUND SCORING MARK ON EXISTING BUSHING. CLG RT TRUNNION FITTING AFT HOLE BUSHING REMOVED. FPI C/O ON REWK AREA AND FOUND NO CORROSION EVIDENT. AFT BOLT HOLE DIA: 1.4380" & FOUND EXCEED LIMIT MAX ALLOWABLE DApr 8, 2008 · N295UP · Doug MD11 · Main Landing Gear Attach SectionSDR UPS08M52429Stringer · crackedINSPECTION TYPE:C LEFT WING FUEL TANK LOWER NR 40 STRINGER END SUSPECT CRACK. HFEC INSP C/O & FOUND CRACK APPROX 6.5 INCH. LEFT WING NR 40 STRINGER END SPLICE REMOVED. ATTACH CLIP & FASTENERS REMOVED. SLOT OUT CRACK AREA C/O & HFEC INSP C/O ON REWK AREA & Apr 7, 2008 · N295UP · Doug MD11 · Wing, Longeron/StringerSDR UPS08M52193Longeron · crackedINSPECTION TYPE:C CTR CARGO COMPT BILGE AREA BETWEEN STA 5-113 & STA 1541 LEFT LONGERON 44 FOUND SUSPECTED CRACK WITH STICKER NR 5190. HFEC INSP C/O & FOUND CRACK APPROX 1 INCH. CRACKED LONGERON SPLICE BETWEEN STA 5-113 & 1541 LT L-44 REMOVED. SPLICE HOLES Apr 7, 2008 · N295UP · Doug MD11 · Fuselage Main, Longeron/StringerSDR UPS08M52176Longeron · crackedINSPECTION TYPE:C CTR CARGO COMPT/BILGE AREA BETWEEN STA 5-113 AND STA 1541, RT LONGERON 44 FOUND SUSPECTED CRACK WITH STICKER NR 5185 AND 5126. HFEC INSP C/O AND FOUND CRACK APPROX 1 INCH CRACKED LONGERON SPLICE BETWEEN STA 5-113 AND 1541, L-44R REMOVED. HApr 7, 2008 · N295UP · Doug MD11 · Fuselage Main, Longeron/StringerSDR UPS08M52175Longeron · crackedINSPECTION TYPE:C CENTER CARGO COMPT/BILGE AREA BETWEEN STA 5-113 AND STA 1541 RT LONGERON 45 FOUND SUSPECTED CRACK WITH STICKER NR 5125 AND 5786. HFEC INSP C/O AND FOUND CRACK APPROX 3 INCHES. CRACKED LONGERON SPLICE BETWEEN STA 5-113 AND 1541, L-45R REMOVEApr 7, 2008 · N295UP · Doug MD11 · Fuselage Main, Longeron/StringerSDR UPS08M52174Longeron · crackedINSPECTION TYPE:C CENTER CARGO COMPT/BILGE AREA BETWEEN STA 5-113 AND STA 1541, RT LONGERON 47 FOUND SUSPECTED CRACK WITH STICKER NR 5187 AND 5189. HFEC INSP C/O AND FOUND CRACK APPROX 4 INCHES. CRACKED LONG SPLICE BETWEEN STA 5- 113 AND 1541 REMOVED PER SRMApr 7, 2008 · N295UP · Doug MD11 · Fuselage Main, Longeron/StringerSDR UPS08M52362Stringer · crackedINSPECTION TYPE:C RIGHT WING FUEL TANK LOWER 44 STRINGER END SUSPECT CRACK. HFEC INSP C/O & FOUND CRACK APPROX 0.5 INCH. STR 44 END ARROWHEAD FITTING REMOVED. ATTACHED CLIP & FASTENERS REMOVED. CRACKED AREA TRIMMED OFF. HFEC C/O ON TRIM EDGE, FOUND NO CRAApr 6, 2008 · N295UP · Doug MD11 · Wing, Longeron/StringerSDR UPS08M52361Stringer · crackedINSPECTION TYPE:C LEFT WING FUEL TANK LOWER 43 STRINGER END SUSPECT CRACK. HFEC INSP C/O & FOUND CRACK APPROX 8 INCH. STR 43 END SPLICE REMOVED. ATTACHED CLIP & FASTENERS REMOVED. SLOT OUT CRACKED AREA C/O. HFEC INSP C/O ON REWK AREA, FOUND NO CRACK EVIDEApr 6, 2008 · N295UP · Doug MD11 · Wing, Longeron/StringerSDR UPS08M52360Stringer · crackedINSPECTION TYPE:C LEFT WING FUEL TANK UPPER 14 STRINGER END SUSPECT CRACK. HFEC INSP C/O & FOUND CRACK APPROX 0.5 INCH. STR 14 END SPLICE REMOVED. ATTACH CLIP & FASTENERS REMOVED. SLOT OUT CRACKED AREA C/O. HFEC INSP C/O ON REWORK AREA & FOUND NO CRACK EVApr 4, 2008 · N295UP · Doug MD11 · Wing, Longeron/StringerSDR UPS08M52359Stringer · crackedINSPECTION TYPE:C LEFT WING FUEL TANK UPPER NR 11 STRINGER END SUSPECT CRACK. HFEC INSP C/O & FOUND CRACK APPROX 11.5 INCH. STR 11 SPLICE REMOVED. ATTACHED CLIP & FASTENERS REMOVED. SLOT OUT CRACKED AREA C/O. HFEC INSP C/O ON SLOT OUT AREA, FOUND NO CRACKApr 4, 2008 · N295UP · Doug MD11 · Wing, Longeron/StringerSDR UPS08M52357Stringer · crackedINSPECTION TYPE:C LEFT WING FUEL TANK UPPER NR 12 STRINGER END SUSPECT CRACK. HFEC INSP C/O & FOUND CRACK APPROX 11.5 INCH. STR 12 END SPLICE REMOVED. STR 12 ATTACH CLIP & FASTENERS REMOVED. SLOT OUT CRACKED AREA C/O. HFEC INSP C/O ON RWK AREA, FOUND NO CApr 4, 2008 · N295UP · Doug MD11 · Wing, Longeron/StringerSDR UPS08M52356Stringer · crackedINSPECTION TYPE:C LEFT WING FUEL TANK LOWER NR 41 STRINGER END SUSPECT CRACK. HFEC INSP C/O & FOUND CRACK APPROX 8.5 INCH. LEFT WING NR 41 STRINGER END SPLICE REMOVED, ATTACHED CLIP & FASTENERS REMOVED. SLOT OUT CRACKED AREA C/O. HFEC INSP C/O ON REWK AREAApr 4, 2008 · N295UP · Doug MD11 · Wing, Longeron/StringerSDR UPS08M52099Seat Track · corrodedINSPECTION TYPE:C CABIN, CORROSION ON SEAT TRACK CROWN AND CHANNEL AT STA1199 X=-8. CORROSION AT AFFECTED AREA REMOVED MAT'L REMOVED 0.040" (STA1199), MAT'L REMN: 0.105", FOUND OUT OF LIMIT. NEW SEAT TRACK FROM STA 1129 TO 1209 X=-8 REWORKED. HOLES PICKED UApr 3, 2008 · N295UP · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR UPS08M52286Longeron · crackedINSPECTION TYPE:C CTR CARGO - BILGE AREA AT BS 1701 TO BS 1710 LONGERON 52 FOUND CRACKED AS MARKED. EXISTING SPLICE AT STA 1701 - 1710 LONGERON 52 REMOVED, CRACKED LONGERON TRIMMED. HFEC INSP C/O ON REWORKED AREA, FOUND NO CRACK EVIDENT. REPAIR LONGERON FABApr 2, 2008 · N295UP · Doug MD11 · Fuselage Main, Longeron/StringerSDR UPS08M52614Frame · chafedINSP TYPE-C, FWD TAILCONE ACCESS CUT OUT LT FRAME, FOUND CHAFED MARK ON PREVIOUS REPAIR. FWD TAILCONE UPPER FWD DOOR OPENING MECH ASSY REMOVED FOR ACCESS. CHAFE MARK FOUND OUT OF LIMIT & REMOVED IAW SRM 51-31-01 VII R35. FAB NEW FWD TAILCONE FRAME WITH HEATApr 1, 2008 · N295UP · Doug MD11 · Aerodynamic FairingsSDR UPS08M52285Seat Track · corrodedINSPECTION TYPE:C CABIN - CORROSION ON SEAT TRACK CROWN, CHANNEL & FLANGE AT STA 808-839 X=107. CORROSION ON AFFECTED AREAS REMOVED. MAT'L THK:0.080" (FLANGE), MAT'L REMOVED: 0.040" (STA 808-824), MAT'L REMN:0.040" FOUND OUT OF LIMIT. DISCREPANT SEAT TRACK Apr 1, 2008 · N295UP · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR UPS08M52284Seat Track · corrodedINSPECTION TYPE:C CABIN - CORROSION ON SEAT TRACK CROWN & CHANNEL AT STA 893 X=107. CORROSION ON AFFECTED AREA REMOVED. MAT'L THK:0.145" (CROWN), MAT'L REMOVED:0. 045", MAT'L REMN:0.100" FOUND OUT OF LIMIT. DISCREPANT SEAT TRACK ON EXIST SPLICE HAT SECT FROMar 29, 2008 · N295UP · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR UPS08M52504Hinge · corrodedINSPECTION TYPE:C RHW O/B FLAP O/B HINGE CENTER CAVITY HOLE FOUND CORRODED AS MARKED. RHW AFT O/B FLAP O/B HINGE FWD MOUNTING CENTER CAVITY HOLE CORROSION. REMOVED ORG DIA EVIDENT FLAP HINGE CENTER CAVITY HOLE OF DIA 1.788 INCH EVAL AND FOUND ACCEPTED PER EMar 26, 2008 · N295UP · Doug MD11 · Trailing Edge FlapsSDR UPS08M52246Seat Track · corrodedINSPECTION TYPE:C CABIN - SEAT TRACK AT STA 791 - 909 X=+75.25 FOUND CORROSION. CORR ON AFFECTED AREA REMOVED MAT'L THK:0.145"(CROWN), MAT'L REMOVED: 0.045"(STA.869-896), MAT'L REMN:0.100". FOUND OUT OF LIMIT. DISCREPANT SEAT TRACK ON EXISTING SPLICE HAT SEMar 25, 2008 · N295UP · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR UPS08M52162Seat Track · corrodedINSPECTION TYPE:C CABIN SEAT TRACK AT STA 859 - 919 X=+8.5 FOUND CORROSION. CORROSION ON AFFECTED AREA REMOVED MAT'L THK: 0.080" (FLANGE), MAT'L REMOVED: 0.050", MAT'L REMN: 0.030 INCH (STA 880) FOUND OUT OF LIMIT. DISCREPANT SEAT TRACK AT STA 849 AND STA929Mar 25, 2008 · N295UP · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR UPS08M52135Seat Track · corrodedINSPECTION TYPE:C CABIN SEAT TRACK AT STA 929 - 979 X=+8.5, FOUND CORROSION. CORROSION ON SEAT TRACK AT AFFECTED AREA REMOVED MAT'L THK: 0.100"(BASE) MAT'L REMOVED: 0.040", MAT'L REMN: 0.060"(STA959), FOUND OUT OF LIMIT. DISCREPANT SEAT TRACK AT STA 929-989 Mar 25, 2008 · N295UP · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR UPS08M52100Seat Track · corrodedINSPECTION TYPE:C CABIN SEAT TRACK AT STA 859 - 909 X=+27.5 FOUND CORROSION. CORROSION ON AFFECTED AREA REMOVED MAT'L THK: 0.145", MAT'L REMOVED: 0.040" (STA899), MAT'L REMN: 0.105". FOUND OUT OF LIMIT. DISCREPANT SEAT TRACK AT STA 849 TO 929 X=+27.5 TRIMMEMar 25, 2008 · N295UP · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR UPS08M52081Seat Track · corrodedINSPECTION TYPE:C CABIN, SEAT TRACK AT STA 919 - 969 X=-75.25 FOUND CORROSION. CORROSION AT AFFECTED AREA REMOVED. MAT'L THK:0.145", MAT'L REMOVED 0.040 INCH (STA 939), MAT'L REMOVED: 0.105 INCH. FOUND OUT OF LIMIT. DISCREPANT SEAT TRACK TRIM OUT. C HFEC Mar 25, 2008 · N295UP · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR UPS08M52613Skin · crackedINSPECTION TYPE-C, CENTER CARGO DOOR CUTOUT, FOUND PREVIOUS REPAIR DOUBLER AT LOWER AFT EDGE CRACKED AND WITH NON STANDARD FASTENERS AS MARKED. CENTER CARGO DOOR CUTOUT-LOWER AFT SIDE HEATING TUBE REMOVED. PREVIOUS REPAIR DOUBLER REMOVED. SKIN TRIMMED & PROTEMar 24, 2008 · N295UP · Doug MD11 · Fuselage Main, Plate/SkinSDR UPS08M52602Skin · damagedINSPECTION TYPE:C FWD CARGO DOOR CUTOUT AFT LOWER SKIN EDGE FROM RT L37-L42 FOUND SEVERAL BLENDOUT REPAIRS AS MARKED. FWD CARGO DOOR CUTOUT AFT LOWER HEATING TUBE & SKIN FASTENERS REMOVED. SKIN BLENDED REPAIR AREA TRIM OUT & REPROTECTED. HFEC INSP C/O ON TRMar 20, 2008 · N295UP · Doug MD11 · Fuselage Main, Plate/SkinSDR UPS08M52173Seat Track · corrodedINSPECTION TYPE:C CABIN CORROSION ON SEAT TRACK CROWN AND FLANGE AT STA 824-865 X=-27. CORROSION ON AFFECTED AREA REMOVED. MATL THK:0.145 INCH (CROWN), MATL REMVD:0.060" (STA 859-861), MATL REMAINED:0.085 INCH FOUND OUT OF LIMIT. DISCREPANT SEAT TRACK REMOVMar 20, 2008 · N295UP · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR UPS08M52150Fairing · damagedINSPECTION TYPE:C PYLON NR 2 EXHAUST FAIRING LT FWD SEAL MOUNT 3RD HOLE FROM BOTTOM FOUND ELONGATED AFTER REMOVAL OF SEAL AND RETAINER. DAMAGED AREA TRIMMED OUT PER EN1131-08. HFEC INSP C/OUT PER DAC NDTSPM R.13 06-10-01.001 FOUND NO CRACK EVIDENT. EXTERNALMar 20, 2008 · N294UP · Doug MD11 · Nacelle/Pylon Miscellaneous StructureSDR UPS08M52149Fairing · damagedINSPECTION TYPE:C PYLON NR 2 EXHAUST FAIRING RT FWD SEAL 2ND MOUNT HOLE FROM BOTTOM FOUND ELONGATED AFTER REMOVAL OF SEAL AND RETAINER. DAMAGED AREA TRIMMED OUT PER EN1131-08 AND MD11-54-20174. HFEC INSP C/OUT PER DAC NDT SPM R.13 06-10-01.001 FOUND NO CRACKMar 20, 2008 · N294UP · Doug MD11 · Nacelle/Pylon Miscellaneous StructureSDR UPS08M52079Seat Track · corrodedINSPECTION TYPE:C CABIN - CORROSION ON SEAT TRACK CROWN & CHANNEL AT STA 830-899 X=-75. CORR AT AFFECTED AREA REMVD. MAT'L THK:0.145"(CROWN), MAT'L REMVD:0.05 0" (STA840), MAT'L REMN:0.095". FOUND OUT OF LMT. DISCREPANT SEAT TRAC K (STA830-929) TRIMMED OUTMar 20, 2008 · N295UP · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR UPS08M52409Skin · chafedINSPECTION TYPE:C, RIGHT TAIL CONE DOOR ASSY INTERIOR BELOW BARRIER KEEPER SKIN CHAFED. KEEPER SKIN CHAFE MARK REMOVED & REPROTECTED. MAT'L REMOVED 0.008" ORG THK 0.032", REMN THK 0.024" FOUND OUT OF LIMIT. EXCEEDED LIMIT SKIN TRIMMED OFF. HFEC INSP C/O ONMar 17, 2008 · N295UP · Doug MD11 · Aerodynamic FairingsSDR UPS08M52134Longeron · crackedINSPECTION TYPE:C CTR CARGO COMPT BILGE AREA BETWEEN STA 1781 AND STA 1801 AT RT LONGERON 45 FOUND SUSPECTED CRACK. HFEC INSP C/OUT IAW DAC NDT SPM R.13 PART06-10-01.001 AND CRACK CONFIRM APPROX 1 1/4 INCH. CRACKED LONG REMOVED FR STA 1671-1811 L45 RT PER SRFeb 22, 2008 · N294UP · Doug MD11 · Fuselage Main, Longeron/StringerSDR 08FDEA00528Skin · dentedLEFT WING - INBOARD FLAP LOWER SURFACE FOUND SEVERAL DENTS AT XIFH 244. DENT AREA FOUND OUT OF LIMIT AS PER SRM 57-10-00 FIGURE 17 VOLUME I AND REPAIR CARRIED OUT AT LEFT HAND WING INBOARD FLAP LOWER SURFACE AS PER SRM 57-10-00 FIGURE 3 VOLUME I. REPAIR Feb 20, 2008 · N621FE · Doug MD11 · Trailing Edge FlapsSDR UPS08M52152Longeron · corrodedINSPECTION TYPE:C CTR CARGO BILGE AREA STA 1541 LONGERON R48 FOUND WITH CORROSION AS MARKED (DECAL 7932) LONGERON CORROSION REMOVED FOUND EXCEED LIMIT PER SRM 53-10-00 FIG 2A V OL1R.40 MATL REMOVED .118" ORIG THK:0.150". EXISTING SKIN STRAP REMOVED FR STA 5-9Feb 16, 2008 · N294UP · Doug MD11 · Fuselage Main, Longeron/StringerSDR UPS08M52071Structure · corrodedINSPECTION TYPE:C CENTER CARGO BILGE RT L48 STA 1715-1695 FOUND MAJOR CORROSION ON LONGERON AS MARKED, LONGERON MAJOR CORROSION REMOVED. FOUND EXCEEDED LIMIT PER SRM 53-10-00 FIG 2A V.1R.40. MAT`L REMOVED:0.075 INCH ORIG THK:0.105 INCH. NEW LONG REWORK C/OUFeb 14, 2008 · N294UP · Doug MD11 · Fuselage Main, StructureSDR UPS08M52012Longeron · corrodedINSPECTION TYPE:C CENTER CARGO BILGE LH44 STA 1721 FOUND CORROSION AS MARKED ON LONGERON UNDERSIDE. LONGERON CORROSION REMOVED AND FOUND EXCEEDED LIMIT PER SRM 53-10-00 FIG 2A V.1R.40. MATL REMOVED:0.044", ORIG THK:0.071". CORRODED LONG SPLICE CUT C/OUT AT Feb 14, 2008 · N294UP · Doug MD11 · Fuselage Main, Longeron/StringerSDR UPS08M52010Longeron · corrodedINSPECTION TYPE:C CENTER CARGO BILGE LT 46 STA 1721 FOUND CORROSION AS MARKED ON LONGERON STA 1721 L46 LT CORROSION REMOVED, REMOVED THK0.027" ORIG THK:0.072 INCH FOUND EXCEEDED LIMIT PER SRM 53-10-00 FIG 2A V.1R.40. CORRODED LONG SPLICE CUT C/OUT AT STA 1691Feb 14, 2008 · N294UP · Doug MD11 · Fuselage Main, Longeron/StringerSDR UPS08M52055Hinge Fitting · corrodedINSPECTION TYPE:C LEFT O/B TRAILING EDGE FLAP I/B WING MOUNTED HINGE PIVOT BORE HOLE AND FACE AREA FOUND RUSTY AS MARKED. (PIVOT BEARING REMOVED). LEFT FWD O/B FLAP I/B HINGE PIVOT BORE HOLE & FACE AREA CORROSION REMOVED & FOUND EXCEED LIMIT PER CMM57-44-08.Feb 13, 2008 · N294UP · Doug MD11 · Trailing Edge FlapsSDR UPS08M52030Skin · damagedINSPECTION TYPE:C LT WING FIXED L/E LOWER SURFACE ABOVE NR 1 ENGINE PYLON O/B SIDE AT APPROXIMATELY STA XORS 299 FOUND SCRATCH MARKS AS MARKED. DAMAGE SKIN REMOVED PER SRM 51-31-01V.2R.40. NEW SKIN FAB PER BOEING DRAWING ARB2363 USING MATL 7075T6-0.090". NEFeb 12, 2008 · N294UP · Doug MD11 · Wing, Plate/SkinSDR UPS08M52013Frame · crackedINSPECTION TYPE:C FAC AFT COMPARTMENT AT STA 449.250 FOUND CRACKED FRAME STRUCTURE JUST BELOW NR 1 RAM AIR INLET SCOOP AFT SECTION AS MARKED. DAMAGE AT RETURN FLANGE TRIM OFF PER EN1071-08. HFEC INSP C/OUT PER DAC NDTSPM R.13 PART06.10.01.001 FOUND NO CRACK Feb 12, 2008 · N294UP · Doug MD11 · Fuselage Main, FrameSDR UPS08M52136Frame · chafedINSPECTION TYPE:C RT RAM AIR EXHAUST CUTOUT FRAME STRUCTURE I/B FWD LOCATION FOUND DEEP CHAF CAUSED BY RAM AIR ACTUATOR LINKAGE. CHAFING MARK SMOOTHENED AND PROTECTED PER SRM 57-21-01V.2R.40. ORIG THK:0. 093 INCH, MATL REM:0.041" FOUND OUT OF LIMIT PER SRM 5Feb 11, 2008 · N294UP · Doug MD11 · Fuselage Main, FrameSDR WRLA2008022Sensor · malfunctionedDURING APPROACH RECEIVED SLAT DISAGREE ALERT, FOLLOWED BY STICK SHAKER. PERFORMED SLAT DISAGREE CHECKLIST, DIVERTED TO KPSM DUE TO RUNWAY CONDITIONS. EMERGENCY DECLARED. REPLACED SLAT POS. SENSORS D1-17 AND D1-18 PER MM 27-84-02. PERFORMED THE SLAT RANGE OFFeb 11, 2008 · N272WA · Doug MD11 · Leading Edge Slat Position Indicating SystemSDR UPS08M52084Spar · crackedINSPECTION TYPE:C LT WING FRONT SPAR ENCLOSURE APPROX STA XORS 514 UPPER SKIN FOUND CRACKED. CRACK AREA TRIM OFF PER EN1007-08. HFEC CARRIED OUT IAW DAC NDT SPM R.13 PART06-10-01.001 FOUND NO CRACK EVIDENT. REPAIR ANGLES FAB USING 7075-0-0.063" MAT`L PER SRFeb 4, 2008 · N294UP · Doug MD11 · Wing SparSDR UPS08M52029Skin · corrodedINSPECTION TYPE:C RT I/B TE FLAP O/B LOWER SEGMENT BOTTOM SKIN TO BE REPLACED DUE TO MULTIPLE DENTS AND CORROSION. NEW SKIN FABRICATED PER BOEING DRAWING ARC2444 USING MATL 2024T3-0.040" NEW SKIN HOLES PICKED UP PER SRM 51-31-01 V.2R40. NEW SKIN PROTECTED PEFeb 3, 2008 · N294UP · Doug MD11 · Trailing Edge FlapsSDR UPS08M52028Skin · corrodedINSPECTION TYPE:C RT I/B TE FLAP LOWER SEGMENT BOTTOM SKIN TO BE REPLACED DUE TO MULTIPLE DENTS AND CORROSION. NEW SKIN FABRICATED PER BOEING DRAWING ARC2736 USING 2024T3-0.040" MATL NEW SKIN HOLE PICKED UP PER SRM 51-31-01 V.2R.40. NEW SKIN PROTECTED PER SRFeb 3, 2008 · N294UP · Doug MD11 · Trailing Edge FlapsSDR WRLA2008017Skin · crackedDURING A CHECK INSPECTION 9 INCH CRACK FOUND RIGHT WING INBOARD FLAP UPPER SKIN INBOARD AFT SKIN PANEL AT XIFH231.2. REPAIRED PER MD-11 SRM 57-20-00 VOL 1 REF ERA 466462-14.Feb 1, 2008 · N272WA · Doug MD11 · Trailing Edge FlapsSDR UPS08M51971Longeron · crackedINSPECTION TYPE:C CAC: BETWEEN STA 6-70 AND STA 6-90, LONGERON 52L FOUND CORROSION CRACK. EXISTING LONG END SPLICE & LONG FASTENERS REMOVED AT STA 6.50-6.90 L52 PER SRM 51-31-01 V.2R.40. CORRODED LONG CUT OUT AT STA 6-60L52 PER SRM 53-10 00 FIG 1V.1R.40. HJan 31, 2008 · N294UP · Doug MD11 · Fuselage Main, Longeron/StringerSDR UPS08M52139Seat Track · corrodedINSPECTION TYPE:C CABIN RT SEAT TRACK AT STA 1964-1953 RBL=107 FOUND CORRODED AS MARKED. CORRODED SEAT TRACK REMOVED PER SRM 51-31-01V.2R.40. HFEC INSP C/OUT IAW DAC NDTSPM 06-10-01.001R.13 FOUND NO CRACK EVIDENT. NEW SEAT TRACK AND SPLICE REWORK PER SRM 53Jan 30, 2008 · N294UP · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR UPS08M52085Skin · chafedINSPECTION TYPE:C RT I/B AILERON FOUND CHAFF MARKS ALONG L/E LOWER SKIN, O/B SIDE. RT I/B AILERON CHAFF SKIN REMOVED PER SRM 51-35-01 V.2R.40. NEW SKIN HOLES PICKED UP PER SRM 51-31-01V.2R.40. NEW SKIN INSTALLED PER SRM 51-35- 01V.2R.40. RHW I/B AILERON LOJan 27, 2008 · N294UP · Doug MD11 · AileronsSDR UPS08M51974Skin · chafedINSPECTION TYPE:C LEFT I/B AILERON FOUND CHAFE MARKS ALONG L/E LOWER SKIN I/B SIDE. CHAFED SKIN REMOVED PER SRM 51-35-01 V.2R40. HOLES ON NEW SKIN PICKED UP PER SRM 51-31-01 V.2 REV.40. NEW SKIN INSTALLED PER SRM 51-35-01 V.2 REV.40.Jan 27, 2008 · N294UP · Doug MD11 · Ailerons
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