N579UP

Service difficulty reports · 248

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 = 'N579UP' 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 IPXA2014020381754Housing · corrodedINSPECTION C, LEFT WING INBD FORE FLAP OTBD LEVER HOUSING CORRODED. REPLACED AND INSTALLED IAW SRM 51-10-02 AND SRM 51-40-02, REV 27.Jan 19, 2014 · N579UP · Boeing 74745E · Trailing Edge FlapsSDR IPXA2014020381750Skin · crackedINSPECTION C, BS 400, S44-45R RT NLG WW AFT CORNER SKIN PANEL FOUND CRACKED RUNNING FWD & AFT APPROXIMATELY .1875" IN LENGTH. REPAIRED IAW RI-53-11-10439, REV A AND EO B747-5330-53290.Jan 19, 2014 · N579UP · Boeing 74745E · Fuselage Main, Plate/SkinSDR IPXA2014020381751Skin · crackedINSPECTION C, BS 400, S44-45R NLG WW AFT CORNER SKIN PANEL FOUND CRACKED AT SECOND LAYER COUNTED FROM SKIN SURFACE RUNNING FWD & AFT THROUGH THICKNESS. SPLICE PLATE FABRICATED AND INSTALLED IAW RI-53-11-10439, REV A AND EO B747-5330-39256-C, APPENDIX D.Jan 18, 2014 · N579UP · Boeing 74745E · Fuselage Main, Plate/SkinSDR IPXA2014020381747Skin · crackedINSPECTION C, BS 400 LT SIDE NOSE WHEEL WELL AFT CORNER FOUND CRACKED AT SKIN LAYER. REPAIRED AT BETWEEN BS 380 - 420, S43-47L IAW NR RI-53-11-10442 REV A AND EO-5330-53287-A.Jan 18, 2014 · N579UP · Boeing 74745E · Fuselage Main, Plate/SkinSDR IPXA2014020381744Doubler · crackedINSPECTION C, BS 400 LEFT SIDE NOSE WHEEL WELL AFT CORNER FOUND CRACKED AT SECOND LAYER FROM SURFACE TOWARD UP & DOWN WITH LENGTH APPROX 0.030" & 0.020". INTERNAL SPLICE PLATE IS REPLACED AND INSTALLED IAW SRM 51-10-02, REV.27 AND HX RI NO RI-53-11-10442 REJan 18, 2014 · N579UP · Boeing 74745E · Fuselage Main, StructureSDR IPXA2014020381742Filler · crackedINSPECTION C, FUSELAGE BS 400, LT SIDE NOSE WHEEL WELL AFT CORNER FOUND CRACKED IN FIRST LAYER FROM SURFACE. FILLER REPLACED IAW SRM 51-10-02, REV 27 AND INSTALLED IAW RI-53-11-10442, REV A.Jan 18, 2014 · N579UP · Boeing 74745E · Fuselage Miscellaneous StructureSDR IPXA2014020381740Doubler · crackedINSPECTION C, BS 400 LT SIDE NOSE WHEEL WELL AFT CORNER FOUND CRACKED . REPAIRED BETWEEN BS 380 - 420, S43-47L IAW RI-53-11-10442, REV A AND EO-5330-53287-A.Jan 18, 2014 · N579UP · Boeing 74745E · Fuselage Main, StructureSDR IPXA2014020581778Channel · damagedINSPECTION C, LT WING REFUELING PANEL 521CB INBD LATCH ATTACH CHANNEL FOUND CORRODED & CRACKED. LATCH ATTACH CHANNEL REPLACED IAW SRM 51-10-02 AND 51-40-02, REV 27.Jan 16, 2014 · N579UP · Boeing 747400 · Wing Miscellaneous StructureSDR IPXA2014020381756Channel · corrodedINSPECTION C, LEFT WING REFUELING PANEL 521CB INBD LATCH ATTACH CHANNEL FOUND CORRODED AND CRACKED. ATTACH CHANNEL REPLACED IAW SRM 51-10-02 AND SRM 51-40-02, REV 27.Jan 16, 2014 · N579UP · Boeing 74745E · Wing, Plate/SkinSDR IPXA2014020381755Skin · crackedINSPECTION C, RT SIDE OF NLG WHEEL WELL AFT CORNER SKIN PANEL CRACKED. REPAIRED IAW RI-53-11- 10439, REV A & EO B747-5330-53290-A. MAJOR REPAIR.Jan 13, 2014 · N579UP · Boeing 74745E · Fuselage Main, Plate/SkinSDR IPXA2014020381741Skin · crackedINSPECTION C, BS 400, NOSE WHEEL WELL LT AFT CORNER SKIN PANEL CRACKED. REPAIRED BETWEEN BS 380-420 S43-47L IAW RI-53-11-10442, REV A AND EO-5330-53287-A. MAJOR REPAIR.Jan 13, 2014 · N579UP · Boeing 74745E · Fuselage Main, Plate/SkinSDR IPXA2014020581776Channel · corrodedINSPECTION C, LT WING REFUELING PANEL 521CB INBD LATCH ATTACH CHANNEL FOUND CORRODED AND CRACKED. REFUELING PANEL INBD LATCH ATTACH CHANNEL REPLACED IAW SRM 51-10-02 AND SRM 51-40-02, REV 27.Jan 6, 2014 · N579UP · Boeing 74745E · Wing Miscellaneous StructureSDR IPXA201307229437Skin · puncturedRIGHT WING INBD FLAP LOWER T/E PUNCTURE DAMAGED. REPAIRED IAW EO B747-5750-51514-A.Jul 21, 2013 · N579UP · Boeing 747400 · Trailing Edge FlapsSDR IPXA201307229433Skin · puncturedRT INBD MID FLAP LWR SURFACE PUNCTURE 1.4" FROM INBD EDGE. REPAIRED IAW EO B747-5750-51513-A.Jul 21, 2013 · N579UP · Boeing 747400 · Trailing Edge FlapsSDR IPXA3B79304Floor Panel · puncturedFLOOR PANEL, BS 1920 PUNCTURED. REPAIRED IAW SRM 53-00-50-2R, REPAIR 1.Jul 14, 2013 · N579UP · Boeing 74745E · Fuselage Floor PanelSDR IPXA3B78095Bulb · inoperativeEMERGENCY LIGHT ON CREW MEMBER STAIR CEILING LIGHT INOPERATIVE. R & R BULB, OPS CHECKED GOOD IAW AMM 33-51-06.Apr 29, 2013 · N579UP · Boeing 74745E · Emergency LightingSDR IPXA12B76065Skin · deformedFWD LWR CARGO DOOR AFT LWR CORNER SKIN DAMAGED. INSTALLED DOUBLER/TRIPLER REPAIR IAW EO B747-5230-48614-B.Oct 26, 2012 · N579UP · Boeing 74745E · Cargo/Baggage DoorsSDR IPXA12B76024Floorboard · gougedMAIN CARGO DECK POS 4L OTBD PANEL I.25 FROM OTBD AND 22" FROM FWD EDGE LESS THAN 1" GOUGE. REPAIRED IAW SRM 53-00-50-2R-1.Oct 22, 2012 · N579UP · Boeing 74745E · Fuselage Floor PanelSDR IPXA12B76023Floorboard · puncturedMC DECK POS 4L HAS .5" HOLE. REPAIRED FLOORBOARD IAW SRM 53-00-50, 2R-1 PARA 4C.Oct 22, 2012 · N579UP · Boeing 74745E · Fuselage Floor PanelSDR IPXA12B74922Frame · crackedINSPECTION TYPE: 1C, MAIN DECK LT BS 1265 FRAME ONE FASTENER HOLE FOUND CRACKED. REPAIRED IAW EO B747-5310-28006-C.Aug 17, 2012 · N579UP · Boeing 74745E · Fuselage Main, FrameSDR IPXA2B74897Support Fitting · crackedINSPECTION TYPE: 1C, LEFT WING SPOILER ACTUATOR NR 6 SUPPORT FITTING INBD LWR LUG AREA FOUND CRACKED. LT WING SPOILER NR 6 SPOILER SUPPORT FITTING INBD LOWER LUG AREA REPAIRED SRM 57- 51-13, REPAIR 1 R.22. REPAIR CLASSIFIED AS MAJOR.Aug 2, 2012 · N579UP · Boeing 74745E · Wing, Attach FittingsSDR IPXA2B74896Support Fitting · crackedINSPECTION TYPE: 1C, RT WING SPOILER ACTUATOR NR 7 SUPPORT FITTING OTBD LWR LUG AREA FOUND CRACKED. RT WING SPOILER ACTUATOR NR 7 SPT FITTING OTBD LWR LUG AREA IS REPAIRED IAW SRM 57-51-13, REPAIR 1 R.22. MAJOR REPAIR.Aug 2, 2012 · N579UP · Boeing 74745E · Wing, Attach FittingsSDR IPXA2B72577Blades · damagedON GEAR RETRACTION AFTER TAKE OFF, MULTIPLE ENGINE REPORTS LOUD AND ASSOCIATED VIBRATIONS ON ENG NR 1. SHUTDOWN NR 1 ENGINE IAW QRH. DUMPED FUEL RETURNED TO DEPARTURE. NO WING CAUTION MESSAGES OR ALERTS. AFT INSPECTION, FOUND 26 FAN BLADES DAMAGED. R &Mar 20, 2012 · N579UP · Boeing 74745E · Turbine Engine Compressor SectionSDR IPXA12B71827Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL AT 4L HAS A HOLE APPROX STA 574 LBL 93.4. REMOVED DAMAGE AND REPAIRED IAW SRM 53-00-50, REPAIR 1.Feb 22, 2012 · N579UP · Boeing 74745E · Fuselage Floor PanelSDR IPXA11B70796Bulb · inoperative1 EMERGENCY LIGHT INOPERATIVE ON CEILING OF UPPER DECK. R & R BULB IAW AMM 33-51-07-2. OPS CHECK GOOD IAW AMM 33-51-07-2.Dec 28, 2011 · N579UP · Boeing 74745E · Emergency LightingSDR IPXA1B70524Floor Panel · damagedFLOOR PANEL STA 852, LBL 25 HAS HOLE. REPAIRED IAW SRM 53-00-50.Dec 4, 2011 · N579UP · Boeing 74745E · Fuselage Floor PanelSDR IPXA1B70523Floor Panel · damagedFLOOR PANEL HAS 3.75" HOLE STA 1770 LBL 90, .5" FWD OF AFT EDGE. REPAIRED IAW SRM 53-00-50.Dec 4, 2011 · N579UP · Boeing 74745E · Fuselage Floor PanelSDR IPXA1B70522Floor Panel · damagedFLOOR PANEL BS 1770, LBL 101.5 HAS .5" HOLE 5" FWD OF AFT EDGE. REPAIRED IAW SRM 53-00-50.Dec 4, 2011 · N579UP · Boeing 74745E · Fuselage Floor PanelSDR IPXA11B68369Battery Pack · dischargedUPPER DECK LT EMER DOOR BATTERY PACK DOESN'T TEST. REPLACED LT DOOR BATTERY PACK IAW MM 52-23-14-4.Jul 31, 2011 · N579UP · Boeing 74745E · Emergency ExitsSDR IPXA1B67442Slide · unwanted deployUPPER DECK RT ENTRY DOOR ESCAPE SLIDE DEPLOYED INADVERTANTLY. MX OPEN ED DOOR WITH ARMING HANDLE IN AUTO. SLIDE DEPLOYED NORMALLY. REPLACED FLOOR MOUNTED SLIDE AND DOOR ASSIST BOTTLE.Jun 21, 2011 · N579UP · Boeing 74745E · Escape SlideSDR IPXA11B67263Bulb · inoperativeEMERGENCY EXIT LIGHT IN CEILING PANEL IN MAIN CARGO DECK FWD, BULB INOPERATIVE. RELAMPED EMERGENCY EXIT LIGHTS FWD. BULB IAW MM 33-51-07-2. OPS CKS NORMAL.Jun 12, 2011 · N579UP · Boeing 74745E · Emergency LightingSDR IPXA11B66954Power Supply · inoperativeUPPER DECK L/T DOOR LIGHT TEST FAILED. REPLACED EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-51-04, OPS TEST OK.May 31, 2011 · N579UP · Boeing 74745E · Emergency LightingSDR IPXA1B65800Stud · inoperativeINSPECTION TYPE:D, U/D EXIT DOOR EMERGENCY LIGHT STUD FOUND BROKEN. U/D EMERGENCY EXIT DOOR SIGN REPLACED. AND OPS TEST FOUND NORMAL AMM 33-51-00.Mar 10, 2011 · N579UP · Boeing 74745E · Light System WiringSDR IPXA1B65793Floor Support · corrodedINSPECTION TYPE:D, BULK CARGO COMPT STA 1920 TO 2040 LBL 53.45 FLOOR SUPPORT CORROSION FOUND. BULK CARGO COMPT STA 1920 TO BS 2040, LBL 53.45 FLOOR SUPPORT REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02, REV 18.Mar 10, 2011 · N579UP · Boeing 74745E · Fuselage Miscellaneous StructureSDR IPXA1B65791Floorbeam · corrodedINSPECTION TYPE:D, BULK CARGO COMPT STA 2044 LBL53" TO RBL53" FLOORBEAM CORRODED. STA 2044, LBL 53- RBL 53 FLOORBEAM REPLACED IAW SRM 51-10-02, REV 18 AND INSTALLED IAW SRM 51-40-02, REV 18, PN 69B03459-2.Mar 10, 2011 · N579UP · Boeing 74745E · Fuselage Main, Floor BeamSDR IPXA1B65784Doubler · corrodedINSPECTION TYPE:D, M/D R4 DOOR FWD LWR CUTOUT REMOVAL DOUBLER AT BS 1665 STR 24R FOUND CORRODED. REVEAL DOUBLER AND REVEAL PANEL EXISTING CUTOUT & REVEAL PANEL CHAFED AREA REPAIRED IAW RS R-53-60-36999 REV A & EO B747-5310-42053 REVEAL DOUBLER ORG MATL IS 707Mar 10, 2011 · N579UP · Boeing 74745E · Fuselage Main, Plate/SkinSDR IPXA1B65833Sill · corrodedINSPECTION TYPE:D, M/D BS 1910 SCD DOOR SILL NR 10 LATCH FTG SERRATE PLATE RUST M/D BS 1910 SCD DOOR SILL NR 10 LATCH FTG SERRATE PLATE. REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02, REV 18.Mar 9, 2011 · N579UP · Boeing 74745E · Fuselage Miscellaneous StructureSDR IPXA1B65799Sill · corrodedINSPECTION TYPE:D, M/DECK SCD DOOR SILL WEB CORRODED AT NR 9 LATCH FTG, STA 1900 WL 117. M/DECK SCD DOOR SILL WEB CORRODED AREA AT STA 1900, WL 117 REPAIRED IAW HX RS R-53-60-36979, REV A & EO B747-5320-42014-A. ORG. MATL IS 7075T6-.125", 0.085" THICKNESS REMMar 9, 2011 · N579UP · Boeing 74745E · Fuselage Miscellaneous StructureSDR IPXA1B65790Sill · corrodedINSPECTION TYPE:D, M/DECK BS 1890 SCD DOOR SILL NR 9 LATCH FTG SERRATE PLATE RUST. M/DECK BS 1890 SCD DOOR SILL NR 9 LATCH FTG SERRATE PLATE REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02, REV 18.Mar 9, 2011 · N579UP · Boeing 74745E · Fuselage Miscellaneous StructureSDR IPXA1B65804Floor Support · corrodedINSPECTION TYPE:D, BULK CARGO COMPT STA 1920 TO 2160, LBL 15" FLOOR PANEL SUPPORT SURFACE FOUND CORRODED. CORROSION REMOVED & REPROTECTED IAW SRM 51-10-02 & SRM 51-20-01 ORG: 0.050" BLENDED DEPTH: 0.002" WIDTH: 0.5", LENGTH: 2" WITHIN SRM 53-00-51 ALLOWABLE DMar 8, 2011 · N579UP · Boeing 74745E · Fuselage Miscellaneous StructureSDR IPXA1B65795Floor Support · corrodedINSPECTION TYPE:D, BULK CARGO COMPT STA 1920 TO 2160, RBL 23" FLOOR PANEL SUPPORT FOUND CORRODED. BULK CARGO COMPT STA 1920 - 2160, RBL 23" FLOOR SUPPORT REPLACED. REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02, REV 18.Mar 8, 2011 · N579UP · Boeing 74745E · Fuselage Miscellaneous StructureSDR IPXA1B65792Floorbeam · corrodedINSPECTION TYPE:D, BULK CARGO COMPT, STA 2018, LBL 8" TO RBL 8" FROM PANEL SUPPORT SURFACE FOUND CORRODED. BULK CARGO COMPT STA 2018, LBL 8 TO RBL 8 FLOOR PANEL SUPPORT REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02, REV 18, PN 146U5092-13.Mar 8, 2011 · N579UP · Boeing 74745E · Fuselage Main, Floor BeamSDR IPXA1B65789Floorbeam · corrodedINSPECTION TYPE:D, BULK CARGO COMPARTMENT, STA 2002, LBL 8" TO RBL 8" FLOOR PANEL SUPPORT SURFACE FOUND CORRODED BULK CARGO COMPARTMENT STA 2002, LBL 8 TO RBL 8 FLOOR SUPPORT REPLACED & INSTALLED IAW SRM 51-10-02 AND 51-40-02, REV 18, PN 146U5092-13.Mar 8, 2011 · N579UP · Boeing 74745E · Fuselage Main, Floor BeamSDR IPXA1B65782Skin · corrodedINSPECTION TYPE:D, M/DECK STA 2280 S24L - S25L DR 5 CUTOUT FX SKIN CORRODED AT INNER FACE. FX SKIN INNER FACE REPAIRED IAW HX RS R-53-61-36981 REV A & EO B747-5330-42049-A. ORG MATL 2024T3-140" THK. CORRODED BLEND OUT DEPTH .101" WIDTH 1" & LENGTH 3" FINAL CUMar 8, 2011 · N579UP · Boeing 74745E · Fuselage Main, Plate/SkinSDR IPXA11B65466Fairing · delaminatedINSPECTION TYPE:D, LT WING OTBD MID FLAP OTBD L/E DELAMINATION. COMPOSITE FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A, FIG 5, REV 17.Mar 8, 2011 · N579UP · Boeing 747400 · Trailing Edge FlapsSDR IPXA1B65814Floor Support · corrodedINSPECTION TYPE:D, BULK CARGO COMPT STA 1920 TO 2040 RBL 45" FLOOR PANEL SUPPORT SURFACE FOUND CORRODED. CORROSION REMOVED & REPROTECTED IAW SRM 51-10-02 & SRM 51-20-01. ORG: 0.050" BLENDED DEPTH: 0.004" WIDTH: 0.6" LENGTH: 2" WITHIN SRM 53-00-51. ALLOWABLE DMar 7, 2011 · N579UP · Boeing 74745E · Fuselage Miscellaneous StructureSDR IPXA1B65813Floor Support · corrodedINSPECTION TYPE:D, BULK CARGO COMPT STA 1920 TO 2160 RBL 31" FLOOR PANEL SUPPORT SURFACE FOUND CORRODED. CORROSION REMOVED AND REPROTECTED AS PER SRM 51-10-02 & SRM 51-20-01. ORG: 0.050" BLENDED DEPTH 0.002" WIDTH: 0.6" LENGTH: 3" WITHIN SRM 53-00-51 ALLOWMar 7, 2011 · N579UP · Boeing 74745E · Fuselage Miscellaneous StructureSDR IPXA1B65812Floor Support · corrodedINSPECTION TYPE:D BULK CARGO COMPT STA 1920 TO 2160 RBL 15" FLOOR PANEL SUPPORT SURFACE FOUND CORRODED. CORROSION REMOVED & REPROTECTED IAW SRM 51-10-02 & SRM 51-20-01. ORG: 0.050" BLENDED DEPTH: 0.003" WIDTH: 2" LENGTH: 3" WITHIN SRM 53-00-51. ALLOWABLE DAMAMar 7, 2011 · N579UP · Boeing 74745E · Fuselage Miscellaneous StructureSDR IPXA1B65811Floor Support · corrodedINSPECTION TYPE:D, BULK CARGO COMPT STA 1920 TO 2160 RBL 8" FLOOR PANEL SUPPORT SURFACE FOUND CORRODED. CORROSION REMOVED & REPROTECTED IAW SRM 51-10-02 & 51-20-01. ORG: 0.050" BLENDED DEPTH: 0.002" WIDTH: 0.6" LENGTH: 2" WITHIN SRM 53-00-51. ALLOWABLE DAMAGMar 7, 2011 · N579UP · Boeing 74745E · Fuselage Miscellaneous StructureSDR IPXA1B65810Floor Support · corrodedINSPECTION TYPE:D, BULK CARGO COMPT STA 1920 TO 2040 LBL 45" FLOOR PANEL SUPPORT SURFACE FOUND CORRODED. CORROSION REMOVED & REPROTECTED IAW SRM 51-10-02 & SRM 51-20-01. ORG: 0.050" BLENDED DEPTH: 0.003" WIDTH: 1" LENGTH: 1" WITHIN SRM 53-00-51 ALLOWABLE DAMMar 7, 2011 · N579UP · Boeing 74745E · Fuselage Miscellaneous Structure
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