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 IPXA1B65809Floor Support · corrodedINSPECTION TYPE:D, BULK CARGO COMPT STA 1920 TO 2040, LBL 38" 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: 2" WITHIN SRM 53-00-51. ALLOWABLE DAMar 7, 2011 · N579UP · Boeing 74745E · Fuselage Miscellaneous StructureSDR IPXA1B65808Floor Support · corrodedINSPECTION TYPE:D, BULK CARGO COMPT STA 1920 TO 2040 LBL 51" FLOOR PANEL SUPPORT FOUND CORRODED. CORROSION REMOVED & REPROTECTED IAW SRM 51-10-02 & SRM 51-20-01, ORG: 0.050" BLENDED DEPTH: 0.003" WIDTH: 1" LENGTH: 2" WITHIN SRM 53-00-51 ALLOWABLE DAMAGE 1 FIGMar 7, 2011 · N579UP · Boeing 74745E · Fuselage Miscellaneous StructureSDR IPXA1B65807Floor Support · corrodedINSPECTION TYPE:D, BULK CGO COMPT STA 1920 TO 2160 LBL 8" 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 DAMAGEMar 7, 2011 · N579UP · Boeing 74745E · Fuselage Miscellaneous StructureSDR IPXA1B65806Floor Support · corrodedINSPECTION TYPE:D, BULK CGO COMPT STA 1920 TO 2040 RBL 51" FLOOR PANEL SUPPORT FOUND CORROSION. CORROSION REMOVED & REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01, ORG: 0.050" BLENDED DEPTH: 0.003" WIDTH: 1" LENGTH: 2" WITHIN SRM 53-00-51. ALLOWABLE DAMAGE 1 FMar 7, 2011 · N579UP · Boeing 74745E · Fuselage Miscellaneous StructureSDR IPXA1B65805Floor Support · corrodedINSPECTION TYPE:D BULK CGO COMPT STA 1920 TO 2160 LBL 31" FLOOR PANEL SUPPORT SURFACE FOUND CORRODED. CORROSION REMOVED & REPROTECTED AS PER SRM 51-10-02 & SRM 51-20-01 ORG: 0.050" BLENDED, DEPTH: 0.002" WIDTH: 1" LENGTH: 2" WITHIN SRM 53-00-51 ALLOWABLE DAMAMar 7, 2011 · N579UP · Boeing 74745E · Fuselage Miscellaneous StructureSDR IPXA1B65803Floor Support · corrodedINSPECTION TYPE:D, BULK CARGO COMPT STA 1920 TO 2160 CTR FLOOR PANEL SUPPORT SURFACE FOUND CORROSION. 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 1 FIGMar 7, 2011 · N579UP · Boeing 74745E · Fuselage Miscellaneous StructureSDR IPXA1B65794Floor Support · corrodedINSPECTION TYPE:D, BULK CARGO COMPT STA 1920 TO 2160 LBL 23" FLOOR PANEL SUPPORT SURFACE FOUND CORRODED. BULK CARGO COMPT STA 1920 TO BS 2160 LBL 23" FLOOR PANEL SUPPORT REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-40-02, REV 18.Mar 7, 2011 · N579UP · Boeing 74745E · Fuselage Miscellaneous StructureSDR IPXA1B65788Reveal · crackedINSPECTION TYPE:D, M/D 4R DOOR FWD CUTOUT REVEAL PANEL CRACKED AT S24R, STA 1666 AREA. M/D 4R DOOR FWD CUTOUT REVEAL PANEL AT STA 1666 STR 24R EXISTING CUTOUT REPAIRED IAW RS R-53-60-36999, REV A & EO B747-5310-42053-A REFER NRC FLJ 509270 FOR WORKING DETAIL.Mar 7, 2011 · N579UP · Boeing 74745E · Fuselage Miscellaneous StructureSDR IPXA1B65787Reveal · crackedINSPECTION TYPE:D, M/D 4R DOOR FWD CUTOUT REVEAL PANEL CRACKED AT S24R STA 1666 AREA. M/D 4R DOOR FWD CUTOUT REVEAL PANEL AT STA 1666, STR 24R EXISTING CUTOUT REPAIRED IAW HX RS R-53-60-36999 REV A & EO NR B747-5310-42053-A REF NRC FLJ 509270 FOR WORKING DETAMar 7, 2011 · N579UP · Boeing 74745E · Fuselage Miscellaneous StructureSDR IPXA1B65786Reveal · chafedINSP TYPE:D, M/D 4R DOOR FWD CUTOUT REVEAL PANEL CHAFING MARK. M/D 4R DOOR FWD CUTOUT REVEAL PANEL CHAFING AREA REPAIRED IAW RS R-53-60-36999, REV A & EO NO B747-5310-42053-A REF NRC FLJ509270 FOR WORKING DETAIL.Mar 7, 2011 · N579UP · Boeing 74745E · Fuselage Miscellaneous StructureSDR IPXA1B65783Floor Support · corrodedINSPECTION TYPE:D, BULK CARGO COMPT STA 1920 TO 2040 RBL 53.45 FLOOR PANEL SUPPORT FOUND CORRODED. CORROSION R & R IAW SRM 51-10-02 & 51-20-01 REV 17, ORG 0.050" BLEND DEPTH 0.003", WIDTH 1" & LENGTH 1" WITHIN SRM 53-00-51 ALLOWABLE DAMAGE 1 FIG, 101 LIMITATIMar 7, 2011 · N579UP · Boeing 74745E · Fuselage Miscellaneous StructureSDR IPXA1B65798Strap · crackedINSPECTION TYPE:D, M/D BS2231 STR 17R FOUND 1EA FASTENER HOLE CRACK AT REVEAL PANEL RUNNING 2 O/C APPROX 0.020" IN LENGTH. M/D BS2231 STR 17R REVEAL DOUBLER (STRAP) REPAIRED. 0.020" CRACK IN LENGTH. FINAL CUTOUT IS 15/16"X1". THIS REPAIR IS CLASSIFIED AS AMar 6, 2011 · N579UP · Boeing 74745E · Fuselage Miscellaneous StructureSDR IPXA1B65797Strap · crackedINSPECTION TYPE:D, M/D BS 2231 S17L FOUND 1 EA FASTENER HOLE CRACK AT REVEAL PANEL RUNNING 12 O/C APPROX. 0.040" IN LENGTH. M/D 2231 S17L REVEAL DOUBLER (STRAP) REPAIRED. THK. 0.040" CRACK IN LENGTH. FINAL CUTOUT IS 15/16"X1". THIS REPAIR IS CLASSIFIED AS Mar 6, 2011 · N579UP · Boeing 74745E · Fuselage Miscellaneous StructureSDR IPXA1B65759Skin · dentedINSPECTION TYPE:D, FUS STA 545, STR 36R TO 37R SKIN FOUND DENT MARK. SKIN REPAIRED IAW SRM 53-00-01. REPAIR 6, FIG 201 REV 18 ORG MATL 0.063" 2024T3. FINAL CUTOUT SIZE 1"DIA REPAIR SIZE 4.25" DIA CLASSIFIED AS MAJOR REPAIR WITH 2024T3-0071IN REPAIR DOUBLER AMar 4, 2011 · N579UP · Boeing 74745E · Fuselage Main, Plate/SkinSDR IPXA11B65470Skin · delaminatedINSPECTION TYPE:D, LT WING INBD FORE FLAP L/E DELAMINATION. COMPOSITE FIBREGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A, FIG 5, REV 17.Mar 4, 2011 · N579UP · Boeing 74745E · Trailing Edge FlapsSDR IPXA11B65469Wedge · delaminatedINSPECTION TYPE:D, RT WING OTBD FORE FLAP UPPER T/E DELAMINATION. COMPOSITE FIBREGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A, FIG 5, REV 17.Mar 4, 2011 · N579UP · Boeing 747400 · Trailing Edge FlapsSDR IPXA11B65468Wedge · delaminatedINSPECTION TYPE:D, RT WING INBD AFT LOWER T/E DELAMINATION. COMPOSITE FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A, FIG 5, REV 17.Mar 4, 2011 · N579UP · Boeing 747400 · Trailing Edge FlapsSDR IPXA11B65467Fairing · delaminatedINSPECTION TYPE:D, LT WING OTBD MID FLAP L/E DELAMINATION. COMPOSITE FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A, FIG 5, REV. 17.Mar 4, 2011 · N579UP · Boeing 74745E · Trailing Edge FlapsSDR IPXA1B65802Battery Pack · inoperativeINSPECTION TYPE:D, EMERGENCY LIGHT BATTERY PACK CAPACITY FUNCTIONALLY CHECK FOUND BATTERY (M5057) FAIL. EMERGENCY LIGHT BATTERY PACK (M5057) REPLACED AND EMERGENCY LIGHT OPS TEST CARRIED OUT RESULT NORMAL. AMM 33-51-04, 33-51-00.Mar 1, 2011 · N579UP · Boeing 74745E · Emergency LightingSDR IPXA1B65801Battery Pack · inoperativeINSPECTION TYPE:D, EMERGENCY LIGHT BATTERY PACK CAPACITY FUNCTIONALLY CHECK FOUND BATTERY (M5056) FAIL. EMERGENCY LIGHT BATTERY PACK (M5056) REPLACED AND EMERGENY LIGHT OPS TEST CARRIED OUT RESULT NORMAL AMM 33-51-04, 33-51-00.Mar 1, 2011 · N579UP · Boeing 74745E · Emergency LightingSDR IPXA1B64281Skin · damagedPYLON SKIN DAMAGED. REPAIRING IAW EO B747-5450-40963-B.Jan 18, 2011 · N579UP · Boeing 747400 · Nacelle/Pylon, Plate/SkinSDR IPXA0B63860Lamp · inoperativeLT UPPER DECK EMERGENCY EXIT GND MODE LIGHT NOT OPERATIVE. RELAMPED GND MODE LIGHT. INDICATION NORMAL.Dec 15, 2010 · N579UP · Boeing 74745E · Emergency LightingSDR IPXA10B62360Floorbeam · crackedFLOOR SUPPORT BEAM DAMAGES AT FWD LWR CARGO STA 570. REPLACED BEAM IAW EO B747-5320-39489-A.Aug 31, 2010 · N579UP · Boeing 74745E · Fuselage Main, Floor BeamSDR IPXA10B62359Seat Track · crackedSEAT TRACK BROKEN AT RBL 45.5. REPLACED TRACK IAW EO B747-5320-39474-A.Aug 31, 2010 · N579UP · Boeing 74745E · Fuselage, Seat/Cargo Attach FittingsSDR IPXA10B60778Skin · damagedLT AFT FLAP SKIN DAMAGED. REPAIRED IAW EO B747-5750-36393-A.Jun 28, 2010 · N579UP · Boeing 74745E · Wing, Plate/SkinSDR IPXA10B59366Skin · dentedINSPECTION TYPE:N/A DENTS TO FUSELAGE AT TAIL BALL STANCHION AREA AT STA 2598 S-42R. REPAIRED REF EO B747-5330-37106-B.Apr 20, 2010 · N579UP · Boeing 74745E · Fuselage Main, Plate/SkinSDR IPXA10B58841Floor Panel · delaminatedFLOOR PNL HAS PUNCTURES AND DELAM AT STA 1730 LBL 100-110. REPAIRED IAW B747 SRM 53-00-50-2R.Mar 14, 2010 · N579UP · Boeing 74745E · Fuselage Floor PanelSDR IPXA10B58855Seal · brokenSEAL BROKEN ON EMERGENCY DESCENT DEVICE. REPLACED DESCENT DEVICE IAW MM 25-61-01-2.Mar 13, 2010 · N579UP · Boeing 74745E · Cabin Equipment/FurnishingsSDR IPXA09B57473Skin · bulgedINSPECTION TYPE:C FUSELAGE STA 1720 TO 1740 STR 42R EXT SKIN BULGED UP. FX BETWEEN BS 1720 TO BS 1741 & STR 41R-43R SKIN REPAIR AS PER SRM 53-00-01 FIG 201 REPAIR 15 REV 12. THIS REPAIR IS CLASSIFIED AS MAJOR CAT B REPAIR REPAIR SIZE 11 X 13.75 INCHES DAMAGESep 28, 2009 · N579UP · Boeing 74745E · Fuselage Main, Plate/SkinSDR IPXA09B57453Frame · crackedINSPECTION TYPE:C NR 3 PYLON INTERIOR AREA STA 346.4 O/B SIDE VERTICAL CHORD FOUND CRACK. NR 3 PYLON INT AREA AT STA 346.4 O/B SIDE VERT FRAME CHORD REPAIRED AS PER HX RS R54-00-36429 REV A. THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR WITH MAT'L 2024T62 0.090"Sep 25, 2009 · N579UP · Boeing 74745E · Nacelle/Pylon, Frame/Spar/RibSDR IPXA09B57426Panel · damagedINSPECTION TYPE:C I/B MID FLAP UPPER T/E PNL 73.5 INCH COUNT FROM I/B SIDE FOUND PUNCH HOLE. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5A REV 12.Sep 23, 2009 · N579UP · Boeing 74744AF · Trailing Edge FlapsSDR IPXA09B57417Wedge · delaminatedINSPECTION TYPE:C RIGHT I/B ELEVATOR T/E WEDGE LOWER SURFACE FOUND DELAMINATED FROM I/B 31 INCHES. RIGHT I/B ELEVATOR T/E COMPOSITE REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5A REV 12.Sep 22, 2009 · N579UP · Boeing 74745E · Elevator StructureSDR UPS08B53921Hmu · malfunctionedINSPECTION TYPE:N/A ENG NR 1 FAILURE ON FINAL WITH SUCCESSFUL AUTO RELIGHT. NR 1 FAILED AGAIN ON GROUND WITH ENG 1 CONTROL MESSAGE. WIND ON FINAL APPROACH TO 26L WAS OUT OF NORTH UP TO 50 KNOTS. REMOVED AND REPLACED NR 1 ENG HMU IAW MM 73-21-14, REMOVED ANDNov 14, 2008 · N579UP · Boeing 74745E · Fuel Control/Turbine EnginesSDR UPS08B53409Tension Tie · crackedINSPECTION TYPE:BCF STA 1180 TENSION TIE LT AFT CHANNEL 6EA FASTENER HOLE CRACK ABOUT OR MORE THAN 0.030 INCH. REPLACED CRACKED TENSION TIE AS PER DWG 65B09631 & SRM 51-40-02.Aug 1, 2008 · N579UP · Boeing 747400 · Fuselage Miscellaneous StructureSDR UPS08B52465Power Supply · dischargedINSPECTION TYPE:N/A FWD RT OVERWING EXTERNAL EMERGENCY EXIT LIGHT INOP. NOTE: TROUBLESHOT TO DEFECTIVE PWR SUPPLY. DEFERRAL M377738 ISSUED. REF MEL 33- 51-2-2. EMERGENCY LIGHTS DEACTIVATED PER SR 747-00-2117. TRANSFERRED TO NR ASL7612Jun 10, 2008 · N579UP · Boeing 747400 · Emergency LightingSDR UPS08B53480Frame · crackedINSPECTION TYPE:BCF RT STA 1140 TENSION TIE FRAME 1EA FASTENER HOLE CRACKED MORE THAN 0.0 30". REPAIRED CRACKED TENSION TIE FRAME AS PER SRM 53-40-07.Mar 8, 2008 · N579UP · Boeing 747400 · Fuselage Main, FrameSDR UPS08B53483Frame · crackedINSPECTION TYPE:BCF STA 1180 LT TENSION TIE FRAME WEB 2EA FASTENER HOLE CRACKED MORE THAN 0.030". REPAIRED CRACKED FRAME WEB AS PER SRM 53-40-07.Jan 8, 2008 · N579UP · Boeing 747400 · Fuselage Main, FrameSDR UPS08B53482Tension Tie · crackedINSPECTION TYPE:BCF STA 1180 TENSION TIE LT FWD CHANNEL 6EA FASTENER HOLE CRACK ABOUT OR MORE THAN 0.030". REPLACED CRACKED TENSION TIE AS DWG 65B09631 AND SRM 51-40-02.Jan 8, 2008 · N579UP · Boeing 747400 · Fuselage Miscellaneous StructureSDR UPS08B53481Tension Tie · crackedINSPECTION TYPE:BCF STA 1180 TENSION TIE RT FWD CHANNEL 6EA FASTENER HOLE CRACK ABOUT OR MORE THAN 0.030". REPLACED CRACKED TENSION TIE AS PER DWG 65B09631, SH14 AND SRM 51-40-0 2.Jan 8, 2008 · N579UP · Boeing 747400 · Fuselage Miscellaneous StructureSDR UPS08B53479Frame · crackedINSPECTION TYPE:BCF STA 1160 LT TENSION TIE FRAME WEB 2EA FASTENER HOLE CRACKED MORE THAN 0.050", 6EA FASTENER HOLE CRACKED ABOUT 0.030". REPAIRED CRACKED TENSION TIE FRAME WEB AS PER SRM 53-40-07.Jan 8, 2008 · N579UP · Boeing 747400 · Fuselage Main, FrameSDR UPS08B53478Tension Tie · crackedINSPECTION TYPE:BCF STA 1140 LT TENSION TIE AFT CHANNEL 5EA FASTENER HOLE CRACKED ABOUT 0 .030" 3EA FASTENER HOLE CRACKED MORE THAN 0.030". REPAIRED CRACKED TENSION TIE AS PER SRM 53-40-30 FIG 201.Jan 8, 2008 · N579UP · Boeing 747400 · Fuselage Miscellaneous StructureSDR UPS08B53477Tension Tie · crackedINSPECTION TYPE:BCF STA 1140 RT TENSION TIE FWD CHANNEL 2EA FASTENER HOLE CRACKED MORE THAN 0.030". REPAIRED CRACKED TENSION TIE AS PER SRM 53-40-30 FIG 201.Jan 8, 2008 · N579UP · Boeing 747400 · Fuselage Miscellaneous StructureSDR UPS08B53476Tension Tie · crackedINSPECTION TYPE:BCF LT STA 1140 TENSION TIE FWD CHANNEL 5EA FASTENER HOLE CRACKED, LENGTH ABOUT 0.030"; 3EA FASTENER HOLE CRACKED LENGTH MORE THAN 0.030". REPAIRED CRACKED TENSION TIE AS PER SRM 53-40-30 FIG 201.Jan 8, 2008 · N579UP · Boeing 747400 · Fuselage Miscellaneous StructureSDR UPS08B53475Tension Tie · crackedINSPECTION TYPE:BCF STA 1140 TENSION TIE RT AFT CHANNEL 2EA FASTENER HOLE CRACKED MORE THAN 0.030". REPAIRED CRACKED TENSION TIE AS PER SRM 53-40-30 FIG 201.Jan 8, 2008 · N579UP · Boeing 747400 · Fuselage Miscellaneous StructureSDR UPS08B53474Failsafe · crackedINSPECTION TYPE:BCF STA 1140 RT TENSION TIE FRAME FAILSAFE CHORD 1EA FASTENER HOLE CRACKED MORE THAN 0.050". REPAIRED CRACKED FRAME FAILSAFE CHORD AS PER SRM 53-70-12.Jan 8, 2008 · N579UP · Boeing 747400 · Fuselage Main, FrameSDR UPS08B53473Failsafe · crackedINSPECTION TYPE:BCF STA 1220 RT TENSION TIE FRAME FAILSAFE CHORD 1EA FASTENER HOLE CRACKED MORE THAN 0.050". REPAIRED CRACKED FAILSAFE CHORD AS PER SRM 51-70-11.Jan 8, 2008 · N579UP · Boeing 747400 · Fuselage Main, FrameSDR UPS08B53472Frame · crackedINSPECTION TYPE:BCF RT STA 1180 TENSION TIE FRAME WEB 2EA FASTENER HOLE CRACKED MORE THAN 0.030". REPAIRED CRACKED FRAME WEB AS PER SRM 53-40-07.Jan 8, 2008 · N579UP · Boeing 747400 · Fuselage Main, FrameSDR UPS08B53470Tension Tie · crackedINSPECTION TYPE:BCF STA 1180 TENSION TIE RT AFT CHANNEL 6EA FASTENER HOLE CRACKED MORE OR THAN ABOUT 0.030". REPLACED CRACKED TENSION TIE AS PER DWG 65B09631 SH14 & SRM 51-40-02.Jan 8, 2008 · N579UP · Boeing 747400 · Fuselage Miscellaneous Structure
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