N286UP

Service difficulty reports · 350

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 = 'N286UP' 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 IPXA09M55886Aileron · misrepairedINSPECTION TYPE:2C REPAIR SURVEY SEQ NR 286-W3-05, EXISTING REPAIR DOUBLER ON LT WING INBD AILERON UPPER LE SKIN AT XIA 318-324 IS INCORRECT MATERIAL GAUGE. REMOVED EXISTING REPAIR DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLER REF MD11 SRM 57-10-00 FIG 38.May 7, 2009 · N286UP · Doug MD11F · AileronsSDR IPXA09M55945Skin · misrepairedINSPECTION TYPE:2C REPAIR SURVEY SEQ NR F1-10, EXISTING REPAIR BETWEEN FS2122-2164, L5R- L8R SIMULAR TO VOL 1 SRM 53-20-00 CLASS 1 REPAIR WITH DEVIATIONS. REMOVED EXISTING REPAIR BETWEEN FS 2122-2164 L5R-L8R ON FUSELAGE AND INSTALLED REPAIR REF IPXA EO MD11-5May 5, 2009 · N286UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA09M55937Skin · misrepairedINSPECTION TYPE:2C REPAIR SURVEY SEQ NR S4-01 EXISTING REPAIR ON UPPER RUDDER LT SIDE BETWEEN ZAR 510-524 BONDED SKIN PANEL NOT PER SRM, NOT ON MRCSSR. REMOVED EXISTING REPAIR ON UPPER RUDDER LT SIDE BETWEEN ZAR 510-524, FABBED AND INSTALLED FILLER AND REPAIRMay 5, 2009 · N286UP · Doug MD11F · Rudder, Plate/SkinSDR IPXA09M55929Skin · misrepairedINSPECTION TYPE:2C REPAIR SURVEY SEQ NR 286-W3-14 EXISTING REPAIR ON LT WING FIXED LE UPPER SKIN BETWEEN XIS 168-178 AT WING SPAR NOT PER SRM AND NOT ON MRCSSR. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED REPLACEMENT REPAIR IAW IPXA EO MD11-5720-33511-AMay 5, 2009 · N286UP · Doug MD11F · Wing, Plate/SkinSDR IPXA09M55885Skin · gougedINSPECTION TYPE:2C REPAIR SURVEY SEQUENCE W4-12 RT WING FIXED L/E UPPER SKIN BETWEEN XIS 242- XIS 252 REPAIR IS GOUGED. REMOVED DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD-11 SRM 57-10-00 FIG 24.May 3, 2009 · N286UP · Doug MD11F · Wing, Plate/SkinSDR IPXA09M55936Wedge · misrepairedINSPECTION TYPE:2C REPAIR SURVEY SEQ W4-05, RT INBD FLAP T/E WEDGE HAS AN EXISTING REPAIR BETWEEN XIFH207-225 THAT IS NOT PER SRM, NOT ON MRCSSR, DISCREPANCY IS WITH FASTENERS. REMOVED AND REINSTALLED RT INBD FLAP TE WEDGE REPAIR REF EO MD11-5750-3 3513-A ANMay 1, 2009 · N286UP · Doug MD11F · Trailing Edge FlapsSDR IPXA09M55935Skin · misrepairedINSPECTION TYPE:2C REPAIRED SURVEY SEQ NR W3-07, LT INBD FLAP UPPER SKIN EXISTING REPAIR BETWEEN XIFH213.050-219 NOT PER SRM, NOT ON MRCSSR. REMOVED EXISTING REPAIR, FABRICATED REPAIR DOUBLER AND INSTALLED REF MD11 SRM VOL 1 57-10-00 FIG 38.May 1, 2009 · N286UP · Doug MD11F · Trailing Edge FlapsSDR IPXA09M55934Wedge · misrepairedINSPECTION TYPE:2C REPAIR SURVEY SEQ W3-08, LT INBD FLAP T/E WEDGE BETWEEN XIFH165-171 NOT PER SRM, NOT ON MRCSSR, DISCREPANCY IS WITH FASTENERS. REMOVED LT INBD FLAP TE WEDGE, FABRICATED 2 Z-ANGLES AND INSTALLED Z-ANGLE AND T/E WEDGE REF SRM VOL1 57-10-00 FIMay 1, 2009 · N286UP · Doug MD11F · Trailing Edge FlapsSDR IPXA09M55928Skin · gougedINSPECTION TYPE:2C REPAIR SURVEY SEQ NR 286-W4-03 EXISTING REPAIR ON RT WING FIXED LE BETWEEN XOS 882-896 AT SLAT TRACK CUT OUT IS NOT PER SRM, HAS A GOUGE .071 AND HAS BLIND RIVETS. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED REPLACEMENT REPAIR IAW MD-May 1, 2009 · N286UP · Doug MD11F · Wing, Plate/SkinSDR IPXA09M55927Skin · misrepairedINSPECTION TYPE:2C REPAIR SURVEY SEQ NR 286-W3-06 LT INBD FLAP LWR SKIN EXISTING REPAIR NOT PER SRM AND NOT ON MRCSSR. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED REPLACEMENT REPAIR IAW MD-11 SRM VOL 1 57-10-00 FIG 38.May 1, 2009 · N286UP · Doug MD11F · Trailing Edge FlapsSDR IPXA09M55926Pressure Panel · misrepairedINSPECTION TYPE:2C REPAIR SURVEY SEQ NR 286-F2-02 EXISTING REPAIR ON HORIZONTAL PRESSURE PNL BETWEEN FS 1401-1441 RBL 80 NOT PER SRM AND NOT ON MRCSSR. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED REPLACEMENT REPAIR IAW IPXA EO MD11-5330-33514-A AND SAA May 1, 2009 · N286UP · Doug MD11F · Fuselage Main, BulkheadSDR IPXA09M55897Skin · damagedINSPECTION TYPE:2C REPAIR SURVEY SEQ NR 286-P2-01 EXISTING REPAIR ON RT NR 2 PYLON BETWEEN STA YID 524.303 - YID 546.559 NOT PER SRM. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED REPLACEMENT REPAIR IAW IPXA EO MD11-5430-33491-A AND SAA EA 011-5430-01-A17May 1, 2009 · N286UP · Doug MD11F · Nacelle/Pylon, Plate/SkinSDR IPXA09M55887Web · misrepairedINSPECTION TYPE:2CAG EVALUATE AND REPAIR AS REQUIRED PER IPXA EO MD11-5100-33150-A EXISTING EPAIR ON STA 1841 AND BETWEEN BL 0 TO LBL 10 ON CTR CARGO COMPT. REMOVED EXISTING REPAIR DOUBLER FABRICATED AND INSTALLED DOUBLER REF EO 5310-33472-A AND EA 011-5310-0May 1, 2009 · N286UP · Doug MD11F · Fuselage Miscellaneous StructureSDR IPXA09M55878Skin · misrepairedINSPECTION TYPE:2C REPAIR SURVEY SEQ F1-05 EXISTING REPAIR BETWEEN FS 1601-1621 LONGERON 51R-51L NOT PER SRM. REMOVED DOUBLER, FABRICATED AND INSTALLED INNER, EXTERNAL, AND FINGER DOUBLER IAW MD-11 SRM 53-20-00 FIG 2 SHT 1-3 AND 53-20-00 PG 1 PARA A.May 1, 2009 · N286UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA09M55872Skin · misrepairedINSPECTION TYPE:2C REPAIR SURVEY SEQ. F2-01 EXISTING REPAIR ON HORIZONTAL PRESSURE PANEL BETWEEN FS 1421- 1441 BL0- RBL 15 NOT PER SRM, NOT ON MRCSSR. REMOVED DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLER AND FINGER DOUBLER IAW IPXA EO MD11-5330-33470.May 1, 2009 · N286UP · Doug MD11F · Fuselage Main, Plate/SkinSDR IPXA09M55871Longeron · misrepairedINSPECTION TYPE:2C REPAIR SURVEY SEQ. F1-06, EXISTING FLUSH REPAIR BETWEEN FS 1621-1641 LONGERON 51L - 51R NOT PER SRM. REMOVED REPAIR DOUBLER, REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND FINGER DOUBLER IAW MD-11 SRM 53-20-00 FIG 6 SHT 10.May 1, 2009 · N286UP · Doug MD11F · Fuselage Main, Longeron/StringerSDR IPXA09M55868Skin · misrepairedINSPECTION TYPE:2C REPAIR SURVEY SEQ. W4-07, RT INBD FLAP LWR SKIN, EXISTING REPAIR BETWEEN XIFH 249-255 IS NOT PER SRM, NOT ON MRCSSR. REMOVED DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-10-00 FIG 38 AND 57-10-00 PG 1 PARA 1.May 1, 2009 · N286UP · Doug MD11F · Trailing Edge FlapsSDR IPXA09M55896Skin · damagedINSPECTION TYPE:2C REPAIR SURVEY SEQ NR 286-W4-04 EXISTING REPAIR HAS A GOUGE ON RT INBD FLAP UPPER SKIN BETWEEN XIFH 231-243. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED REPLACEMENT REPAIR IAW IPXA EO MD11-5750-33490-A AND SAA EA 011-5753-01-A1764.Apr 29, 2009 · N286UP · Doug MD11F · Trailing Edge FlapsSDR IPXA09M55869Stringer · misrepairedINSPECTION TYPE:2C EVALUATE AND REPAIR AS REQUIRED PER IPXA EO MD11-5100-33150-A, EXISTING REPAIR ON THE STR 14 BETWEEN XORS 506-538. REMOVED REPAIR, FABRICATED AND INSTALLED REPAIR ANGLES IAW MD-11 SRM 57-20-00 FIG 10 SHEET 7.Apr 29, 2009 · N286UP · Doug MD11F · Wing, Longeron/StringerSDR IPXA09M55919Doubler · crackedINSPECTION TYPE:2C RT WING FIXED L/E BEADED DOUBLER XFS 669 CRACKED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER, FILLER, AND ANGLE IAW MD-11 SRM 57-10-00 FIG 27 SHEETS 1-4.Apr 28, 2009 · N286UP · Doug MD11F · Wing Miscellaneous StructureSDR IPXA09M55750Doubler · gougedINSPECTION TYPE:2C REPAIR SURVEY SEQ 286-W4-11, EXISTING REPAIR DOUBLER ON RT WING FIXED L/E BETWEEN XOS 1164-1171 HAS A GOUGE. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD-11 SRM 57-10-00 FIG 7 SHEET 1-3.Apr 28, 2009 · N286UP · Doug MD11F · Wing Miscellaneous StructureSDR IPXA09M55918Doubler · crackedINSPECTION TYPE:2C LT WING L/E BEADED DOUBLER XFS 681 CRACKED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, ANGLE AND DOUBLER IAW MD-11 SRM 57-10-00 FIG 27 SHEET 1-4.Apr 27, 2009 · N286UP · Doug MD11F · Wing Miscellaneous StructureSDR IPXA09M55895Skin · damagedINSPECTION TYPE:2C REPAIR SURVEY SEQ NR 286-W4-01 EXISTING REPAIR DOUBLER ON RT WING FIXED LE BETWEEN XOS 461-473 HAS A GOUGE. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED REPLACEMENT REPAIR IAW IPXA EO MD11-5730-33489-A AND SAA EA 011-5730-01-A1754.Apr 27, 2009 · N286UP · Doug MD11F · Wing, Plate/SkinSDR IPXA09M55888Skin · gougedINSPECTION TYPE:2C REPAIR SURVEY SEQ NR 286-W3-02, EXISTING REPAIR DOUBLER ON LT WING FIXED L/E BETWEEN XOS461-473 HAS A GOUGE. REMOVED EXISTING REPAIR FABRICATED NEW REPAIR AND INSTALLED REF SRM 57-10-00 FIG 43.Apr 27, 2009 · N286UP · Doug MD11F · Wing, Plate/SkinSDR IPXA09M55917Skin · gougedINSPECTION TYPE:2C REPAIR SURVEY SEQUENCE F1-03 FOUND GOUGED REQUIRES REPLACEMENT OF REPAIR ON FWD CARDO DOOR CUTOUT LWR AFT CORNER. REMOVED DOUBLERS, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW MD-11 SRM 53-50-00 FIG. 17 VIEW B AND C.Apr 26, 2009 · N286UP · Doug MD11F · Cargo/Baggage DoorsSDR UPS09M54547Battery · dischargedEMERGENCY LIGHT BATTERY 1 LOW ALERT WITH EMERGENCY LIGHT TEST. DEFERRED PER MEL 33-50-4. M394085. R&R EMERGENCY LIGHTING BATTERY POWER SUPPLY PER MM 33-51-01-4 AND PERFORMED OPS TEST PER MM 33-51-01-5. SATISFACTORY.Feb 4, 2009 · N286UP · Doug MD11F · Emergency LightingSDR UPS08M54103Cover · out of positionINSPECTION TYPE:N/A SLIDE CASING ON L1 DOOR IS ASKEW AND INTERFERES WITH DOOR OPENING. INSTALLED SLIDE CASING DOOR L1 CORRECTLY REF MM 25-61-05. OK FOR SERVICE.Dec 5, 2008 · N286UP · Doug MD11F · Escape SlideSDR UPS08M53852Skin · damagedINSPECTION TYPE:N/A RIVETS PULLED THROUGH UPPER SKIN OF INBOARD FLAP LT WING. REPAIR IAW EO MD11-5750-31055-B.Nov 4, 2008 · N286UP · Doug MD11F · Trailing Edge FlapsSDR UPS08M53226Lever · inoperativeL1 DOOR ARM LEVER WILL NOT ARM. ADJUSTED LOWER DOOR INTERIOR COVER. OPS CHECK NORMAL. DOOR LIGHT EXTINGUISHED.Aug 25, 2008 · N286UP · Doug MD11F · Escape SlideSDR UPS08M52539Skin · damagedINSPECTION TYPE:1C EVALUATE EXISTING REPAIR DOUBLER AT FS 879 AND LONGERON 28L ON EXTERNAL SKIN. EXISTING REPAIR AT FS 879 AND LONG 28L DOES NOT MEET SRM CRITERIA. REMOVED EXISTING REPAIR, CUT OUT DAMAGED SKIN, FABRICATED REPAIR DOUBLER, TRIPLER, AND FINGER Jun 12, 2008 · N286UP · Doug MD11F · Fuselage Main, Plate/SkinSDR UPS07M50209Wire · brokenDUE TO MCDU NR 2 FAILURE DEFERRED PER MEL 31-65-1. DEF 354944 & 355043. ON T/S FOUND WIRE BROKEN AT PIN 41 OF P1-1026A. REPAIRED IAW SWP AND WEDM 34-63-22. R&R NR 3 MCDU IAW AMM 31-65-01-4. OPS TEST IAW AMM 31-65-01-5 NOW NORMAL. DMI CLOSED, PLACARD REMOVED.Jul 21, 2007 · N286UP · Doug MD11F · Instrument System WiringSDR UPS07M49198Idg · overservicedINSPECTION TYPE:N/A WHILE EN ROUTE TO CRK, THE CREW ADVISED DISPATCHER OF THE LOSS OF THE NR 3 GENERATOR. THE FLIGHT WAS APPROX 45 MINUTES OUT OF CRK DUE TO A PREV DEF OF THE NR 1 GENERATOR, & THE APU. ONLY THE NR 2 GENERATOR REMAINED AS A POWER SOURCE. EPCFeb 14, 2007 · N286UP · Doug MD11F · AC Generator-AlternatorSDR UPS07M48817Skin · corrodedINSPECTION TYPE:C EMP EXTERNAL SKIN RT SIDE FROM Y=2084 TO Y=2164 AND S-34R TO S-35R FOUND CORROSION AT HORZ STAB FAIRING CUTOUT ATTACH HOLES AS MARKED. CORROSION REMOVED & TREATED AS PER SRM 51-21-01 VOL II REV 38 MATL TH K 0.125 INCH, THK REMOVED 0.005 INCHDec 5, 2006 · N286UP · Doug MD11F · Fuselage Main, Plate/SkinSDR UPS07M48949Stiffener · crackedINSPECTION TYPE:C AFT FX COMPT FWD BULKHEAD APPROX AT RBL 10 FOUND VERTICAL STIFFENER TOP EDGE CRACKED. CRACK STIFFENER PARTS & FASTENERS REMOVED PER SRM 53-00-01 FIG 8 VIR38 & 51-31-01VIIR38. CRACK STIFFENER CUTOFF PER SRM 53-00-01 FIG 8VIR38. HFEC C/O PERDec 4, 2006 · N286UP · Doug MD11F · Fuselage Main, BulkheadSDR UPS07M48884Beam · corrodedINSPECTION TYPE:C CTR CARGO, UPPER DOOR JAMB AREA, STA 1601 FOUND WITH CORROSION UPON OPENING OF TOP BOX. CTR CARGO, UPPER DOOR JAMB AREA STA 1601 CORROSION REMOVED PER SRM 51-31-01 VOL II REV 38. MATERIAL ORIGINAL THK 0.085" STA 1601, REMOVED 0.039" REMAIN Nov 30, 2006 · N286UP · Doug MD11F · Fuselage Main, StructureSDR UPS07M48883Beam · corrodedINSPECTION TYPE:C CTR CARGO, DOOR JAMB AREA, UPPER AREA STA 1721 - 1745 UPON REMOVAL OF TOP BOX, FOUND CORROSION INSIDE AS MARKED. CORROSION REMOVED PER SRM 51-21-01VOL II REV38. MATL ORIG THK 0.125" STA 1721-173 0 REMOVED 0.026" REMAINING 0.099", STA 1730-1Nov 30, 2006 · N286UP · Doug MD11F · Fuselage Main, StructureSDR UPS06M48760Skin · dentedRT UPPER FUSELAGE SKIN INDENTATION MARK, 36 INCHES FWD OF NR 2 ENG INLET. RT UPPER FUSE SKIN STA 1811-1821 L9R-11R FASTENERS REMOVED PER SRM 53-20-0 0 FIG 2 SHT 23 VOLI R38 AND 51-31-01 VOL II R38. INDENTATION MARK REMOVED PER SRM 5 3-20-00 FIG 2 SHT 23VOLI Nov 29, 2006 · N286UP · Doug MD11F · Fuselage Main, Plate/SkinSDR UPS07M49066Support · corrodedINSPECTION TYPE:C AFT CARGO, STA 1841 TO STA 1967, RT SLOPE PANEL LOWER MOUNT, FOUND WITH CORROSION AT SEVERAL PLACES AS MARKED. CORROSION REMOVED, FOUND BEYOND LIMIT PER SRM 53-00-01 FIG 1A VOLI REV38. SUPPORT REMOVED PER SRM 51-35-01 VOL II REV 38. NEW SUNov 24, 2006 · N286UP · Doug MD11F · Fuselage Miscellaneous StructureSDR UPS07M49065Support · corrodedINSPECTION TYPE:C AFT CARGO, STA 1841 TO STA 1921, LT SLOPE PANEL LOWER MOUNT, FOUND WITH CORROSION AS MARKED AT SEVERAL LOCATIONS. CORROSION REMOVED FOUND BEYOND LIMIT PER SRM 53-00-01 FIG 1 AVOLIREV38. SUPPORT REMOVED PER SRM 51-35-01 VOL II REV38. NEW SUNov 24, 2006 · N286UP · Doug MD11F · Fuselage Miscellaneous StructureSDR UPS07M49036Skin · dentedINSPECTION TYPE:C LH WING, I/B AILERON LOWER SURFACE FOUND DENT MARKS. LHW I/B AIL LWR SURF DENT DEPTH MEASURE 0.066" EXCEED LIMIT AND 4 PL DENT DEEPER DEPTH MEASURE 0.030" WITHIN LIMIT PER SRM 51-80-01VIIR38. HFEC C/O PER DACNDTSPMR12PT06.10.01.001 ON SKIN Nov 16, 2006 · N286UP · Doug MD11F · AileronsSDR UPS07M49035Skin · scratchedINSPECTION TYPE:C RT WING I/B AILERON LOWER SURFACE, SCRATCH MARK FOUND AT 8" MEASURE FROM I/B. I/B AIL FROM I/B AND O/B STRIPS 2 AND SCRATCH MARK SKIN FASTENERS REMOVED PER SRM 51-35-01VIIR38. SKIN PNL CUT-OFF PER SRM 57-10-00 FIG 1 VIR38. HFEC C/O PER DACNov 16, 2006 · N286UP · Doug MD11F · AileronsSDR UPS07M48882Structure · corrodedINSPECTION TYPE:C CTR CGO, RT TUNNEL AREA, STA 1761-1781, LONGERON R27, FOUND CORROSION ON SUPPORT STRUCTURE AS MARKED. STA 1761 BEAM AT LONG R27 CORROSION REMOVED 0.018" BY 2" BY 4" REMAINING 0.107" ORIG THK 0.125" WITHIN LIMIT PER SRM53-00-01VOL I FIG1 AREVNov 16, 2006 · N286UP · Doug MD11F · Fuselage Miscellaneous StructureSDR UPS07M48876Bearing · corrodedINSPECTION TYPE:C LT WING, O/B FLAP O/B HINGE BRACKET (WING SIDE), SIDE LINK ATTACHMENT BEARING SURFACE CORRODED. SURF CORROSION REMOVED CMM57-44-09PG402-408R56 ORIG THK I/B 0.486" O/B 0. 446" REMAINING THK I/B 0.484" O/B 0.444" MATL REMOVED I/B 0.002" O/B 0.Nov 15, 2006 · N286UP · Doug MD11F · Trailing Edge FlapsSDR UPS07M48837Seat Track · corrodedINSPECTION TYPE:C CABIN SEAT TRACK AT STA 1964 RBL=107 FOUND CORRODED AS MARKED. SEAT TRACK CROWN SURF CORROSION REMOVED SRM 51-21-01 VOLIIR38 MATL REMOVED 0.056" EXCEED LIMIT PER SRM 53-70-00 FIG3 VOLI. DAMAGED SEAT TRACK CUTOFF AND REMOVED SRM 53- 70-00 FNov 15, 2006 · N286UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR UPS07M48836Seat Track · corrodedINSPECTION TYPE:C CABIN SEAT TRACK AT STA 1913 LBL=107 FOUND CORRODED AS MARKED. SEAT TRACK CORROSION REMOVED PER SRM 51-21-01 VOLIIR38 MAT`L. REMOVED 0.063" EXCEED LIMIT PER SRM53-70-00 FIG 3 VOLIR38. DAMAGED SEAT TRACK CUTOFF AND REMOVED PER SRM 53-7 0-00Nov 15, 2006 · N286UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR UPS06M48784Web · dentedINSPECTION TYPE:C CTR CARGO, STA 1841, WEB FOUND WITH DENTS AS MARKED. REMOVED WEBS ATTACH SUPPORTS & FASTENERS PER SRM 51-31-01VOL IIR38. FAB WEBS AGA7170-3 & -4 PER DWG AGA7170. NEW WEBS REPROTECTED PER SRM 52-21-01 VOL IIR38. NEW WEBS PAINTED PER SRM 51Nov 15, 2006 · N286UP · Doug MD11F · Fuselage Miscellaneous StructureSDR UPS07M48872Hinge · corrodedINSPECTION TYPE:C LT WING, I/B FLAP O/B HINGE (FLAP SIDE) O/B LUG O/B FLANGE CORRODED. LHW IB FLAP OB HINGE AFT SIDE OB STRAP OB SURF LOCAL BLEND CORROSION REMAINING THK 0.205" AND CORROSION STILL EXIST MIN ALLOW THK 0.205" CMM57-52-03. ST ARP REMOVED SRM 51Nov 7, 2006 · N286UP · Doug MD11F · Trailing Edge FlapsSDR UPS07M48871Hinge · corrodedINSPECTION TYPE:C RT WING, I/B FLAP O/B HINGE, O/B LUG O/B FLANGE CORRODED. RHW IB FLAP OB HINGE AFT SIDE OB STRAP OB SURF LOCAL BLEND CORRODED, REMAINING THK 0.205" AND CORROSION STILL EXIST MIN ALLOW THK 0.205" CMM 57-52-03. STRAP REMOVED SRM 51-33-01VINov 7, 2006 · N286UP · Doug MD11F · Trailing Edge FlapsSDR UPS07M49090Spar · corrodedINSPECTION TYPE:C LEFT WING - UPPER SKIN AT AFT SPAR, SKIN BULGING (CORROSION) IN 3 DIFFERENT AREAS. REAR SPAR XORS 683, 738, 735, 825 CORR REMOVED FOUND WITHIN LIMIT PER SRM 57-20-00 FIG 16 R38VI. XORS 799 CORR REMOVED EXCEED LIMIT PER SRM 57-20-00 FIG 6VIRSep 29, 2006 · N286UP · Doug MD11F · Wing SparSDR UPS07M49089Structure · dentedINSPECTION TYPE:C LEFT WING - NR 4 SLAT L/E DENTS (2), 3 INCHES OUTBOARD OF INBOARD EDGE. LEFT WING NR 4 SLAT L/E DENTS 2 EA MEASRUED 0.063 & 0.043 DEEP 0.5 INCH APART EXCEED LIMITS IAW SRM 57-10-00 FIG 6VI. DAMAGED AREA TRIMMED OUT PER SRM 57-10-00 FIG 5 VISep 28, 2006 · N286UP · Doug MD11F · Leading Edge Devices
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