N581UP
Service difficulty reports · 309
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 = 'N581UP' 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.
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 = 'N581UP' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR IPXA1B68450Skin · puncturedD435426 RT INBD MID FLAP HAS .3750" PUNCTURE ON COVE PANEL. REPAIRED IAW EO B747-5750-43709-A AND SRM 51-70-07.SDR IPXA1B68449Panel · puncturedD435425 LT INBD MID FLAP COVE PANEL HAS .3750" PUNCTURE. REPAIRED IAW EO B747-5750-43710-A AND SRM 51-70-07.SDR IPXA1B67807Floor Panel · damagedFLOOR PANEL, AT STA 1700 POS 17L MULTIPLE DAMAGES. FABRICATED NEW FLOOR PANEL USING BMS4-17, TYPE 2 FLOORBOARD, REF DRAWING 146U5877.SDR IPXA1B67806Floor Panel · damagedFLOOR PANEL AT STA 1760 POS 18L MULTIPLE DAMAGES. FABRICATED NEW FLOOR PANEL USING BMS4-17 TYPE 1 FLOORBOARD, REF DWG 65B23345, D455166 CLEARED.SDR IPXA1B67804Floor Panel · damagedMAIN DECK FLOOR PNL STA 1982, DAMAGED REF EO B747-5320-4 2973-A NR 2 DAMAGED HAS 2 HOLES MEASURING .5 IN DIA WITH 1 IN SEPARATION. REPAIR FLR PNL IAW SRM 53-00-51, REPAIR 1, 4D.SDR IPXA1B67803Floor Panel · damagedMAIN DECK FLOOR PNL, STA 1982, DAMAGED REF EO B747-5320-42973-A NR 3 HOLE 0.5 DIA LOCATED 3 IN AFT OF SECOND DAMAGED AND 6 IN FROM OUTBD EDGE REPAIRED FLR PNL DAMAGE IAW SRM 53-00-50, REPAIR 1, 4C.SDR IPXA1B67802Floor Panel · damagedMAIN DECK FLOOR PANEL STA 1982 DAMAGED REF EO B747-532 0-42973-A NR 4 DAMAGED AREA HAS 4 HOLES 0.25 IN DIA AND ARE 1.5 APART DISBONDING 8.0 X 4 AREA REPAIRED FLOOR PANEL IAW SRM 53-00-50, REPAIR 1 4F.SDR IPXA1B67801Floor Panel · damagedMAIN DECK FLOOR PANEL AT STA 1982, DAMAGED REF EO B747- 5320-42973-A NR 6 DAMAGE HAS HOLE 0.75 IN DIA 6 IN FROM 5TH DAMAGED AREA AND 3.5 IN FROM OTBD EDGE. REPAIRED FLOOR PANEL IAW SRM 53-00-50, REPAIR 1, 4C.SDR IPXA1B67800Floor Panel · damagedMAIN DECK FLOOR PANEL DAMAGED REF EO B747-5320-42973-A NR7 DAMAGED AREA IS 1X0.5 HOLE MINOR GORE DAMAGE LOCATED 4 IN AFT OF 6TH DAMAGED AREA 6 IN FROM OTBD EDGE. REPAIR FLR PANEL IAW SRM 53-00-50, REPAIR 1 4C.SDR IPXA1B67799Floor Panel · damagedMAIN DECK FLOOR PANEL STA 1982 DAMAGED REF EO B747-532 0-42973-A 1ST DAMAGE AREA HAS 3 HORS IN A 2X1 IN AREA. REPAIRED IAW SRM 53-00-50, REPAIR 1 4D.SDR IPXA1B67798Floor Panel · damagedMAIN DECK FLOOR PANEL STA 1982, DAMAGED REF EO B747-5320-429 73-A NR2 HOLES MEASUREING 0.5 DIA WITH 1'' SEPARATION. REPAIR IAW SRM 53-00-51, REPAIR 1, 4D.SDR IPXA1B67797Floor Panel · damagedFLOOR PANEL STA 1767, RBL 95 HAS HOLE 1.5" X .75". LOCATED 1.5" FROM OTBD EDGE. REPAIRED IAW EO B747-5320-42967-A AND SRM 53-50-51 REPAIR 1.SDR IPXA1B67796Floor Panel · damagedFLOOR PANEL STA 290 LBL 36 HAS HOLE IN SKIN 3" X .3" 9" FROM FWD END OF PANEL. REPAIRED IAW EO B747-5320-42963-A AND SRM 53-00-51 REPAIR 1.SDR IPXA1B67795Floor Panel · damagedFLOOR PANEL STA 2127, LBL 87 HAS HOLE IN UPPER SKIN 1.5" FROM OTBD EDGE AND 27" FROM FWD END. REPAIRED IAW EO B747-5320-42968-A AND SRM 53-00-51 REPAIR 1.SDR IPXA1B67794Floor Panel · crackedINSPECTION TYPE:N/A MCD FLOOR PANEL STA 1761 LBL 36 CRACKED WITH DELAMINATION. REPAIRED IAW EO B747-5320-42965-A AND SRM 53-00-51, REPAIR 1.SDR IPXA1B67793Floor Panel · crackedCRACK WITH DELAMINATION FLOOR PANEL STA 919, LBL 25. REPAIRED IAW EO B747-5320-42972-A AND SRM 53-00-51, REPAIR 1.SDR IPXA1B67792Floor Panel · crackedFLOOR PANEL STA 1679, LBL 46 HAS CRACK WITH DEBOND. REPAIRED IAW EO B747-5320-42969-A AND SRM 53-00-51.SDR IPXA10B63543Fairing · chafedINSPECTION TYPE:C, LT WING OTBD FORE FLAP L/E FAIRING OTBD AREA HOLE CHAFED. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5D, FIG 6, REV 57 121, CELSIUS DEGREE.SDR IPXA10B61910Skin · misrepairedINSPECTION TYPE:C, SURVEY SEQUENCE NR 581-F1-05 FWD CARGO DOOR SKIN AND LOWER BEAM AT BETWEEN BS 653-670 AND STR 38R-40R AREA EXISTING REPAIR DOES NOT CORRELATE TO EFN 58120041002. BS653-BS670 & STR 38R-40R AREA REPAIRED & ACCEPTABLE RESPECTIVELY IAW HX RS R5SDR IPXA10B61592Panel · noneINSPECTION TYPE:C, LT WING OTBD AILERON T/E WEDGE UPPER SURFACE EXISTING REPAIR (REDO) REF SURVEY SEQ NO 581-W3-09 (NO REPAIR RECORD). FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1) FIG 5, REV 57.SDR IPXA10B61590Panel · unknownINSPECTION TYPE:C, LT WING OTBD AILERON UPPER PANEL EXISTING REPAIR (REDO) SURVEY SEQ NR 581-W3-04. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1) FIG 5, REV 57.SDR IPXA10B61589Panel · unknownINSPECTION TYPE:C, LT WING OTBD AILERON UPPER PANEL EXISTING REPAIR (REDO) NO REPAIR RECORD. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1), FIG 5, REV 57.SDR IPXA10B61587Panel · unknownINSPECTION TYPE:C, LT WING OTBD AILERON UPPER PANEL EXISTING REPAIR (REDO) SURVEY SEQ NR 581-W3-74 (NO REPAIR RECORD). FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1) FIG 5, REV 57.SDR IPXA10B61586Wedge · misrepairedINSPECTION TYPE:C, LT WING OTBD AILERON T/E WEDGE UPPER SURFACE EXISTING REPAIR (NO REPAIR RECORD). FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1) FIG 5, REV 57.SDR IPXA10B61603Wedge · misrepairedINSPECTION TYPE:C, LT WING INBD FORE FLAP T/E WEDGE LWR SURFACE EXISTING REPAIR NO-STANDARD. REPAIR FIBERGLASS PREPREG LAY UP. REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 57.SDR IPXA10B61602Wedge · misrepairedINSPECTION TYPE:C, LT WING INBD FORE FLAP T/E WEDGE LWR SURFACE EXISTING REPAIR NON-STANDARD REPAIR. FIBERGLASS PREPREG LAYUP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5.C, FIG.2, REV.57.SDR IPXA10B61601Wedge · misrepairedINSPECTION TYPE:C LT WING INBD FORE FLAP T/E WEDGE LWR SURFACE EXISTING REPAIR NON-STANDARD. REPAIR FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5 C, FIG 2, REV 57.SDR IPXA10B61600Wedge · misrepairedINSPECTION TYPE:C LH WING I/B FORE FLAP T/E WEDGE LWR SURFACE EXISTING REPAIR NON-STANDARD REPAIR FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5.C FIG.2 REV 57.SDR IPXA10B61599Wedge · misrepairedINSPECTION TYPE:C, LT WING INBD FORE FLAP T/E WEDGE LWR SURFACE EXISTING REPAIR NON-STANDARD. REPAIR FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5 C, FIG 2, REV 57.SDR IPXA10B61598Wedge · misrepairedINSPECTION TYPE:C, LT WING INB FORE FLAP T/E WEDGE LWR SURFACE EXISTING REPAIR NON-STANDARD. REPAIR FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5 C, FIG 2, REV 57.SDR IPXA10B61597Wedge · misrepairedINSPECTION TYPE:C LT WING INBD FORE FLAP T/E WEDGE LWR SURFACE EXISTING REPAIR NON-STANDARD. REPAIR FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 57.SDR IPXA10B61585Panel · noneINSPECTION TYPE:C, LT WING OTBD AILERON T/E WEDGE LWR SURFACE EXISTING REPAIR. (NO REPAIR RECORD) FIBERGLASS PREPREG LAYUP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1) FIG 5, REV.57.SDR IPXA10B61515Skin · dentedINSPECTION TYPE:C, LT WING NR6 SPOILER UPPER SURFACE FOUND DENTED. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4, FIG 201, SHEET 1, REV 56.SDR IPXA10B61593Wedge · delaminatedINSPECTION TYPE:C, LT WING OTBD AFT FLAP T/E WEDGE LWR SURFACE DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1) FIG 5, REV 56.SDR IPXA10B61514Wedge · delaminatedINSPECTION TYPE:C, LT WING OTBD AFT FLAP T/E WEDGE LWR SURFACE DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1) FIG 5, REV 56.SDR IPXA10B61505Wedge · delaminatedINSPECTION TYPE:C, LT WING OTBD FORE FLAP T/E WEDGE UPPER SURFACE DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1) FIG 5, REV 56.SDR IPXA10B61502Wedge · delaminatedINSPECTION TYPE:C, LT WING OTBD AFT FLAP T/E WEDGE LWR SURFACE DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SEM 51-70-07, PAR 5A (1) FIG 5, REV 56.SDR IPXA0B61956Skin · dentedINSPECTION TYPE:C, RT WING INBD AFT FLAP LWR SKIN FOUND DENTS. SKIN METAL HOT BOND INTERIM REPAIRED IAW HX RS NR R57-51-36778, REV A AND EO B747-5750-39125-A. THIS IS A MAJOR REPAIR WITH ALUMINUM SHEET : 2024T3-0020IN. REPAIR PATCH SIZE: 51.5" X 19". FINAL CUSDR IPXA0B61955Skin · dentedINSPECTION TYPE:C, LT WING INBD AFT FLAP LWR SKIN FOUND SEVERAL DENTS. SKIN METAL HOT BOND INTERIM REPAIRED IAW HX RS R57-51-36778 REV A AND EO B747-5750-39125-A. THIS IS A MAJOR REPAIR WITH ALUMINUM SHEET: 2024T3-0020IN. REPAIR PATCH SIZE: 36.5" X 19". FINSDR IPXA10B61508Panel · delaminatedINSPECTION TYPE:C, EMP - LT OTBD ELEVATOR UPPER PANEL DELAMINATION FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1)
FIG 5, REV 56.SDR IPXA10B61506Skin · delaminatedINSPECTION TYPE:C, EMP LT OTBD ELEVATOR UPPER SURFACE PANEL DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1) FIG 5, REV 56.SDR IPXA10B61501Panel · delaminatedINSPECTION TYPE:C, LT WING OTBD MID FLAP T/E COVE PANEL UPPER SURFACE DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1) FIG 5, REV 56.SDR IPXA10B61500Panel · delaminatedINSPECTION TYPE:C, LT WING OTBD MID FLAP T/E COVE PANEL UPPER SURFACE DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A (1) FIG 5, REV 56.SDR IPXA10B61909Skin · crackedINSPECTION TYPE:C, EMP LT OTBD ELEVATOR LWR SURFACE L/E FIXED PANEL CRACK AT ELE STA 281.8, CRACK LENGTH 2.3". STA 273-290 AREA L/E FIXED PNL REPAIRED IAW HX RS R55-20-36774, REV A & EO B747-5520-38940-A, ORG. MAT'L 0.032IN 6061-T6 CRACK LENGTH 2.3", FINAL CUSDR IPXA10B61891Frame · crackedINSPECTION TYPE:C EMP- TAIL COMPT STA 2598 LT BHD INNER CHORD CRACK AT LWR TORSION BOX AREA AS MARKED. (CHORD CRACK LENGTH 0.915"), ( WEB CRACK LENGTH 0.030" ) CHORD & WEB REPAIRED IAW HX RS R53-80-36775, REV A AND EO 747- 5310-38966-A, ORG MAT'L:BAC1505-1008SDR IPXA10B61513Wedge · delaminatedINSPECTION TYPE:C RT WING INBD FORE T/E WEDGE LWR SURFACE DELAMINATION FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1) FIG 5, REV 56.SDR IPXA10B61512Wedge · delaminatedINSPECTION TYPE:C, LT WING INBD FORE FLAP T/E WEDGE LWR SURFACE DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1) REV 56.SDR IPXA10B61510Wedge · delaminatedINSPECTION TYPE:C LT WING INBD FORE FLAP T/E WEDGE LWR SURFACE INBD AREA DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-50-07 PAR 5A(1) FIG 5, REV 56.SDR IPXA10B61507Panel · delaminatedINSPECTION TYPE:C, LT WING OTBD MID FLAP T/E COVE PANEL UPPER SURFACE DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1) FIG 5, REV 56.SDR IPXA10B61491Panel · delaminatedINSPECTION TYPE:C, LT WING OTBD MID FLAP T/E COVE PANEL UPPER SURFACE DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1), FIG 5, REV 56.
Back to N581UP