N291UP

Service difficulty reports · 280

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 = 'N291UP' 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 UPS08M51364Stringer · crackedINSPECTION TYPE:C RIGHT WING FUEL TANK STRINGER NR 9 END SUSPECT CRACKED. HFEC INSP C/O FOUND CRACK APPROX 10.25". STR 9 SPLICE END & HI-LOKS AT REPAIR AREA REMOVED. CRACK AT STR 19 SLOT OUT PER SRM 57-10-00 FIG 10 VI R35. HFEC INSP C/O ON SLOT OUT AREA, NNov 19, 2007 · N291UP · Doug MD11F · Wing, Longeron/StringerSDR UPS07M51295Skin · crackedINSPECTION TYPE:C LHW L/E LOWER ACCESS STA XORS 538 AT O/B REFUELING RECEPTACLE TOP FOUND CORRUGATED SKIN CRACKED AS MARKED. LHW L/E LWR CAVITY BEADED SKIN FASTENERS AT DAMAGED AREA AND ATTACH PARTS REMOVED. DAMAGED AREA ON BEADED DOUBLER TRIMMED OFF PER SRMNov 19, 2007 · N291UP · Doug MD11 · Wing, Plate/SkinSDR UPS08M51550Structure · corrodedINSPECTION TYPE:C HORIZ STAB CONSTANT SECTION RT NR 09 BARREL NUT BORE FOUND WITH CORROSION. CORROSION AT B-NUT BORE REMOVED. BORE BOTTOM REMAINED BLEND OUT 0.030" BORE REAM TO 0.988" DIA, REMAIN BLEND OUT 0.060" FOUND EXCEED LIMITS 10X MAG INSP C/O AND FOUNNov 16, 2007 · N291UP · Doug MD11 · Horizontal Stabilizer StructureSDR UPS08M51512Structure · corrodedINSPECTION TYPE:C HORIZ STAB CONSTANT SECTION LT NR 36 BARREL NUT BORE FOUND WITH CORROSION. CORROSION AT B-NUT BORE REMOVED. BORE BOTTOM REMAINING BLEND OUT 0.075" DEEP. BORE REAM TO 2.538" DIA AND REMAINING BLEND OUT 0.080" DEEP, FOUND EXCEED EO MD 11-551Nov 15, 2007 · N291UP · Doug MD11 · Horizontal Stabilizer StructureSDR UPS08M51399Stringer · crackedINSPECTION TYPE:C RIGHT WING FUEL TANK STRINGER 11 END SUSPECT CRACKED. HFEC INSP C/O AT STR 11, FOUND CRACK 11 INCHES LONG. RIGHT WING STR 11 SPLICE END, ATTACH BRACKETS & HI-LOKS REMOVED. STR 11 RIGHT WING TRIM OFF. HFEC INSP C/O ON TRIM OFF AREA, FOUND Nov 13, 2007 · N291UP · Doug MD11F · Wing, Longeron/StringerSDR UPS08M51398Stringer · crackedINSPECTION TYPE:C LEFT WING UPPER FUEL TANK STRINGER 9 END SUSPECT CRACKED. HFEC INSP C/O AT STR 9 END, FOUND APPROX 15 INCH CRACK. STR 9 SPLICE END & HI-LOKS REMOVED. CRACKED END AT LEFT WING STR 9 TRIMMED OFF. HFEC INSP C/O ON TRIM OFF AREA, FOUND NO CRANov 13, 2007 · N291UP · Doug MD11F · Wing, Longeron/StringerSDR UPS07M51349Stringer · crackedINSPECTION TYPE:C RT WING FUEL TANK STRINGER NR 10 END SUSPECT CRACKED. HFEC INSP C/O AT STR NR 10 END FOUND CRACK OF APPROX 11 INCHES LONG. STR NR 10 SPLICE END & HI-LOKS AT REPAIR AREA REMOVED. CRACK AT STR NR 10 SLOT OUT PER SRM 57-20-00 FIG 10 VI R35. Nov 13, 2007 · N291UP · Doug MD11F · Wing, Longeron/StringerSDR UPS07M51348Stringer · crackedINSPECTION TYPE:C LT WING UPPER FUEL TANK STRINGER NR 12 END SUSPECT CRACKED. HFEC INSP C/O AT STR NR 12 END FOUND CRACK OF APPROX 10.5 INCHES LONG. STR 12 SPLICE END & HI-LOKS REMOVED. CRACK AT LT WING STR NR 12 SLOT OUT PER SRM 57-2 0-00 FIG 10 VI R35. HNov 13, 2007 · N291UP · Doug MD11F · Wing, Longeron/StringerSDR UPS07M51347Stringer · crackedINSPECTION TYPE:C RT WING UPPER FUEL TANK STRINGER NR 12 END SUSPECT CRACKED. HFEC INSP C/O AT STR NR 12 END FOUND CRACK OF APPROX 8" LONG. STR NR 12 SPLICE END AND LOCK FASTENERS AT REPAIR AREA REMOVED. CRACK AT STR NR 12 SLOT OUT PER SRM 57-20-00 FIG 10 VNov 13, 2007 · N291UP · Doug MD11 · Wing, Longeron/StringerSDR UPS07M51346Stringer · crackedINSPECTION TYPE:C LT WING UPPER FUEL TANK STRINGER NR 10 END SUSPECT CRACKED. HFEC INSP C/O AT STR NR 10 FOUND CRACK APPROX 10" LENGTH. STR NR 10 SPLICE END AND LOCK FASTENER AT REPAIR AREA REMOVED. CRACK AT STR NR 10 SLOT OUT PER SRM 57-20-00 FIG 10 VIR35.Nov 13, 2007 · N291UP · Doug MD11F · Wing, Longeron/StringerSDR UPS07M51345Stringer · crackedINSPECTION TYPE:C LT WING UPPER FUEL TANK STRINGER NR 11 END SUSPECT CRACKED. HFEC INSP C/O AT STR NR 11, FOUND CRACK OF APPROX 5" LENGTH. STR NR 11 SPLICE END AND LOCK FASTENER AT REPAIR AREA REMOVED. CRACK AT LT WING STR NR 11 SLOT OUT PER SRM 57-20-00 FINov 13, 2007 · N291UP · Doug MD11F · Wing, Longeron/StringerSDR UPS08M51581Skin · damagedINSPECTION TYPE:C FWD FUSE CROWN AT STA 615.0 BETWEEN RT L4 AND L7 FOUND PREVIOUS DENT BLENDOUT REPAIR. REMOVED EXISTING FASTENER FOR ACCESS AND TRIM OFF DENT AREA PER SRM 53-20-00 VIR35 FIG2. HFEC INSP C/O ON TRIM OFF AREA, FOUND NO CRACK EVIDENT. FAB NEW Nov 7, 2007 · N291UP · Doug MD11F · Fuselage Main, Plate/SkinSDR UPS08M51418Doubler · corrodedINSPECTION TYPE:C AFT CARGO/AT STATION 1954 LONGERON 51 RT, DOUBLER FOUND WITH SURFACE CORROSION. AFT CARGO STA 1954 L51 RT LONG END SPLICE FASTENERS REMOVED, END SPLICE CORRODED REMOVED, FOUND EXCEEDED LIMIT PER SRM 53-00-01 FIG1 AVIR35. NEW END SPLICE AGA3Nov 7, 2007 · N291UP · Doug MD11 · Fuselage Main, Plate/SkinSDR UPS07M51339Shear Tie · corrodedINSPECTION TYPE:C AFT CARGO/AT STATION 1954 IN BETWEEN LONGERON 49 LT TO 49 RT FRAME SHEAR CLIP FOUND WITH SURFACE CORROSION. AFT CARGO STA 1954 - 1964 L52 (01EA) AND L51 (01EA) EXISTING INTERCOSTAL ALSO REMOVED. EXISTING BRACKETS 05EA REMOVED AT STA 1954 L4Nov 7, 2007 · N291UP · Doug MD11 · Fuselage Internal Mounting StructureSDR UPS08M51384Rib · crackedINSPECTION TYPE:C RIGHT WING L/E CAVITY, L/E RIB LOWER END SUSPECT CRACK AT 19 INCHES O/B OF SLAT TRACK NR 3 AS MARKED. HFEC INSP C/O ON O/B OF SLAT TRACK NR 3 FOUND CRACK OF APPROX 1.5 INCH LENGTH. RIGHT WING L/E CAVITY L/E RIB LOWER REMOVED PER SRM 51-31-0Nov 6, 2007 · N291UP · Doug MD11F · Wing, Rib/BulkheadSDR UPS08M51383Rib · crackedINSPECTION TYPE:C RIGHT WING L/E CAVITY, L/E RIB LOWER END SUSPECT CRACK AT 6 INCHES I/B OF SLAT TRACK NR 3 AS MARKED. HFEC INSPECTION C/O AT I/B OF SLAT TRACK NR 3, FOUND CRACK AS MARKED APPROX 1 INCH LENGTH. RIGHT WING L/E CAVITY, L/E LOWER RIB REMOVED PERNov 6, 2007 · N291UP · Doug MD11F · Wing, Rib/BulkheadSDR UPS07M51289Longeron Splice · crackedINSPECTION TYPE:C CTR CARGO/AT STATION 1535 LONGERON 40 LT FOUND DOUBLER WITH SUSPICIOUS CRACKED AS MARKED. HFEC C/O IAW DAC NDT SRM R13, PT06-10-01.001 ON CRACKED AREA. CRACK CONFIRMED APPROX 1 INCH LONG. CRACKED LONGERON SPLICE REMOVED. NEW SPLICE FAB FRNov 5, 2007 · N291UP · Doug MD11 · Fuselage Main, Longeron/StringerSDR UPS07M51288Seat Track · corrodedINSPECTION TYPE:C CABIN, CORROSION ON SEAT TRACK CROWN AND CHANNEL AT STA1381 - 1501 X=-8. CORROSION REMOVED FOUND EXCEEDED LMT PER SRM 53-70-00 FIG3 VIR 35. DAMAGED SEAT TRACK SECTIONAL CUT-OUT AND REMOVED BTW STA 1411-1531 PER SRM 51-31-01 VIIR 35. HFEC Nov 5, 2007 · N291UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR UPS07M51225Longeron · corrodedINSPECTION TYPE:C CTR CARGO AT STATION 5-32 TO STA 5-52 LONGERON 46L 14 EACH FASTENERS FOUND WITH RUSTY NUT AS MARK. CENTER CARGO STA 5-32 TO 5-52 LONGERON 46 LT RUSTY NUTS 14 EA REMOVED PER SRM 51-33-01VIIR35. NEW NUTS 3D0006-3 (14 EA). INSTALLED AT CTR CANov 5, 2007 · N291UP · Doug MD11 · Fuselage Main, Longeron/StringerSDR UPS07M51282Seat Track · corrodedINSPECTION TYPE:C AFT CABIN, CORROSION ON SEAT TRACK CROWN AT STA1911 AND STA1964 X=107. DAMAGED SEAT TRACK FOUND OUT OF LIMIT PER SRM 53-70-00 FIG 3 (ORG MAT'L: 0.145", REMVD: 0.090") AND REMOVED FROM STA1831 - 2007 X=107 PER SRM 51-31. -01VIIR35. NEW SEAT Nov 4, 2007 · N291UP · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR UPS07M51257Seat Track · corrodedINSPECTION TYPE:C CABIN - CORROSION ON SEAT TRACK CROWN, CHANNEL & FLANGE AT STA 1289 TO STA 1381 X=-75. CORROSION REMOVED PER SRM 51-21-01 VII R35. ORG THK: 0.080", MATL REMN: 0.035" (CHANNEL). FOUND EXCEED LIMIT. DAMAGED SEAT TRACK SECTIONAL CUT OUT & RENov 4, 2007 · N291UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR UPS07M51291Skin · dentedINSPECTION TYPE:C LT WING I/B FLAP I/B LOWER SEGMENT LOWER SURFACE FOUND NUMEROUS DENTS. LT I/B FLAP I/B SEGMENT REMOVED AND SKIN REMOVED PER SRM 51-35-01VIIR 35. NEW SKIN FAB USING 2.24-T3 0.040" MAT'L PER DOUGLAS DWG ARC2736 REV B. FASTENER HOLES DRILLED Oct 30, 2007 · N291UP · Doug MD11 · Trailing Edge FlapsSDR UPS07M51290Skin · dentedINSPECTION TYPE:C LT WING I/B FLAP O/B LOWER SEGMENT LOWER SURFACE FOUND NUMEROUS DENTS. LT I/B FLAP O/B SEGMENT REMOVED PER CMM 51-52-03R59. LHW I/B FLAP O/B LOWER SEGMENT SKIN REMOVED PER SRM51-35-01VIIR 35. NEW SKIN FAB USING 2024T3-0.040" MAT'L PER DOUGOct 30, 2007 · N291UP · Doug MD11 · Trailing Edge FlapsSDR UPS07M51340Skin · crackedINSPECTION TYPE:C LT WING L/E LOWER ACCESS, 12" O/B OF SLAT TRACK NR 11, FOUND CORRUGATED SKIN CRACKED AT 05 EA PLACES AS MARKED. LHW L/E CAVITY BEADED SKIN FASTENERS AT DAMAGED AREA AND ATTACHED PARTS REMOVED. DAMAGED AREA ON BEADED DOUBLER TRIM OFF PER SRMOct 29, 2007 · N291UP · Doug MD11 · Wing, Plate/SkinSDR UPS07M51338Skin · crackedINSPECTION TYPE:C LT WING L/E LOWER ACCESS, IN BETWEEN REFUELING RECEPTACLES FOUND CORRUGATED SKIN CRACKED AT 04 EA PLACES AS MARKED. LT WING REFUELING RECEPTACLE O/B SIDE REMOVED. LT WING L/E CAVITY BEADED SKIN FASTENERS AT DAMAGED AREA AND ATTACH PARTS REMOct 29, 2007 · N291UP · Doug MD11 · Wing, Plate/SkinSDR UPS07M51258Seat Track · corrodedINSPECTION TYPE:C CABIN - CORROSION ON SEAT TRACK CROWN & CHANNEL AT STA 999-1079. CORROSION REMOVED PER SRM 51-21-01 VII R35. ORG THK: 0.100", MATL REMN: 0.047" (CHANNEL). FOUND EXCEED LIMIT. DAMAGED SEAT TRACK SECTIONAL CUT OUT BETWEEN STA 969 - STA 1089Oct 29, 2007 · N291UP · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR UPS08M51385Rib · crackedINSPECTION TYPE:C LEFT WING L/E SLAT TRACK NR 16, I/B RIB FOUND CRACKED AS MARKED. LEFT WING NR 8 SLAT CABLE REMOVED. LEFT WING NR 16 SLAT TRACK DOOR, SLAT TRACK, BRACKET, PULLEY, ATTACHING HARDWARES & 04 EA BEARINGS REMOVED. LEFT WING L/E ELECT WIRING FROMOct 27, 2007 · N291UP · Doug MD11F · Wing, Rib/BulkheadSDR UPS08M51365Rib · crackedINSPECTION TYPE:C RIGHT WING L/E SLAT TRACK 16, I/B RIB FOUND CRACKED AS MARKED. RIGHT WING 8 SLAT CABLES REMOVED. NR 16 SLAT TRACK, DOOR, BRACKET, PULLEY, HARDWARES, BEARINGS 4EA & I/B RIB REMOVED. NEW RIB INSTALLED PER SRM 51-31-01 VII R35. RIGHT WING 16Oct 27, 2007 · N291UP · Doug MD11F · Leading Edge DevicesSDR UPS07M51223Seat Track · corrodedINSPECTION TYPE:C CABIN, CORROSION ON SEAT TRACK CROWN AND CHANNEL AT STA 902 X=27. CORROSION ON SEAT TRACK SECTIONAL TRIM OUT BTWN STA830 - 909, X=27 AND REMOVED PER SRM 51-31-01 VIIR 35. HFEC INSP C/O PER DAC NDTSPM R13 06-10-01.001 ON TRIM OUT AREA AND FOct 27, 2007 · N291UP · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR UPS07M51204Seat Track · corrodedINSPECTION TYPE:C CABIN, CORROSION ON SEAT TRACK FLANGE FROM STA 806-840 X=-75. REMOVED PER SRM 51-21-01VIIR35. ORG THK:0.100", MATL REMN: 0.040", EXCEED LMT PER SRM 53-70-00VI FIG 3 R35. CORROSION SEAT TRACK REMOVED PER SRM 51-31-01VIIR35. NEW SEAT TRACK ROct 27, 2007 · N291UP · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
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