N460UP
Service difficulty reports · 205
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 = 'N460UP' 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 = 'N460UP' 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 IPXA2026050849719Pump · faultedEMERGENCY DECLARED. L HYD SYS PRESS. BOTH L ENG DRIVEN & L ELECTRIC DRIVEN HYD PUMPS DEACTIVATED WITHIN 90 SECS OF EICAS MSGS R&R L ENG HYD SUPPLY HOSE TO EDP IN REF TO AMM 29-11-05. PERFORMED L ENG RUN IN REF TO AMM 71-00-00. OPS CK AND LEAK CK GOOD.SDR IPXA2026050749719Filter · faultedEMERGENCY DECLARED, LT HYD SYS PRESS. BOTH L ENG DRIVEN & L ELECTRIC DRIVEN HYD PUMPS DEACTIVATED WITHIN 90 SECS OF EICAS MSGS R&R L ENG EDP CASE DRAIN FILTER AND PRESSURE FILTER ELEMENT IN REF TO AMM 29-11-17. STILL REQUIRES LEAK CK.SDR IPXA2026033023913Skin · dentedREMOVED PREVIOUS REPAIR ON THE RT, INBD MAIN FLAP PANEL. 3.5" DIA CUTOUT, 12.5" OTBD OF INBD EOP, 96" INBD OF OTBD EOP, 19. 3/4" FWD OF T/E. IAW SRM 51-70-10-2R-0 PARA. 7 OC . APPLIED BOEGEL AND PRIMER P/N 21401842 BATCH 4451891 IAW B757 SRM 51-70-10-2R-0 PARSDR IPXA2026031739174Crease Beam · corrodedDURING MAIN CABIN BS 1200 FLOORBEAM REPAIR, AFTER REMOVAL OF RT OTBD WEB, BS 1180-1210, RBL 65. CREASE BEAM WAS FOUND WITH CORROSSION. REMOVED ONE CRACKED ANGLE & ONE WEB IAW SRM 51-40-02. INSTALLED NEW CHANNEL AND INSTALLED WEB IN LT MLG WW, BS 1180, THROUGSDR IPXA2026030239174Crease Beam · corrodedMAJOR REPAIR. DURING MAIN CABIN FLOOR BS 1200, FLOORBEAM REPAIR, AFTER REMOVAL OF RT OTBD WEB, BS 1180 - 1210, RBL 65 CREASE BEAM WAS FOUND WITH CORROSSION. WORK ACCOMPLISHED IAW EO-96522-REQ 1, & EA 757-5360-27-A4343 REV-.SDR IPXA2026030318640Skin · dentedMAJOR REPAIR. SEVERAL SMALL DENTS ON TOP SKIN OF RT INBD FLAP. OUTER SKIN OF RT WING INBD MAIN FLAP ASSY WAS FOUND WITH ONE DENT OUT OF SRM 57-53-01-1A-1 ALLOWABLE LIMITS. THE DENT WAS TRIMMED OUT. CATEGORIZED AS A MAJOR REPAIR.SDR IPXA2026030291662Strap · corrodedSTR ACCESS DOOR313AL LOWER STRAP HAS CORROSION BETWEEN RBL 9 AND LBL 12. REMOVED COVER STRAP FOR ACCESS AND STRAP CORRODED IAW SRM 51-40-02-0G-0 INSTALLED AND PAINTED LOWER STRAP ACCESS DOOR 313AL BETWEEN RBL 9 AND LBL 12 IAW SRM 51-40-02SDR IPXA2026030282338Frame · dentedMAJOR REPAIR. FWD CARGO BS 800 RT SIDE FRAME DENTED. WORK ACCOMPLISHED IAW EO-96553-REQ 1 & EA 757-5330-27-A4327, REV-.SDR IPXA2026022079132Skin · dentedSLAT NR 5 WITH SEVERAL DENTS IN THE UPPER SURFACE. REMOVED DAMAGE AND PREPARED AREA AT SLAT NR 5 2EA DENTS IAW B757-200 SRM 51-70-10-2R-0.SDR IPXA2026021949700Angle · puncturedCREW ENTRY DOOR, INNER SIDE, LOWER SILL, CLOSE TO LT STA 297, ANGLE SUPPORT HAS A HOLE. REMOVED FROM CREW ENTRY DOOR, INNER SIDE, LOWER SILL, BETWEEN LH STA 297 TO 333.45, ANGLE SUPPORT WITH A HOLE (MISDRILLED HOLE) IAW SRM 51-40-02 INSTALLED NEW ANGLE SUPPOSDR IPXA2026021950684Channel · crackedLH WW MLG, BULKHEAD 1180, UNDER PANEL 143XAL, VERTICAL BRACKET SUPPORT AT JOGGLE AREA HAS A CRACK. REMOVED LH WW MLG, BULKHEAD 1180, UNDER PANEL 143XAL, VERTICAL BRACKET SUPPORT IAW SRM 51-40-02-0G-0 INSTALLED NEW BRACKET SUPPORT LH WW MLG, BULKHEAD 1180, UNDSDR IPXA2026022350890Channel · crackedRH WW MLG, BULKHEAD 1180, UNDER PANEL 144XAR, VERTICAL BRACKET SUPPORT AT JOGGLE AREA HAS A CRACK. REMOVED RH W/W MLG BULKHEAD 1180 UNDER PANEL 144XAR ANGLE SUPPORT TO GAIN ACCESS IAW SRM 51-40-02-0G-0 INSTALLED NEW BRACKET SUPPORT ON RH WW MLG, BULKHEAD 118SDR IPXA2026030244157Floorbeam · corrodedMAJOR REPAIR. MAIN CABIN FLOORBEAM, STA 1200 RBL 45-65 CORRODED. WORK ACCOMPLISHED IAW EO-96554-REQ 1, & EA 757-5360-27-A4326, REV-.SDR IPXA2026021744310Seat Track · corrodedMAJOR REPAIR. MAIN CABIN FLOOR STRUCTURE, STA 1160-1200 BL 0 SEAT TRACK CORRODED. DOT 28-28 REMOVED CORROSION IN SEAT TRACK I.A.W. B757-200 SRM 51-10-02 INSTALLED REPAIR PARTS IAW B757-200PF SRM 53-00-52-2R-7 STEP 10 AND B757-200PF SRM 51-40-02-0G-0SDR IPXA2026022243116Skin · corrodedMAJOR REPAIR, L/H PYLON INBD INNER SKIN BETWEEN BETWEEN PANELS 433JR ANS 433HR HAS EVIDENCE OF CORROSION AT LOWER AREA. MARKED IN RED PERFORMED BLENDOUT OF DAMAGE ON L/H PYLON INBD INNER SKIN BETWEEN PANELS 433JR AND 433HR, IAW 757-200PF SRM 51-10-02. ACCOMPSDR IPXA2026021734376Floorbeam · corrodedMAIN CABIN FLOOR STRUCTURE, FLOOR BEAM STA 1680 RBL 25-65 HAS (3EA) AREAS WITH EXFOLIATION. REMOVED DAMAGE IAW SRM 51-10-02. REQUEST NDT TO VERIFY DAMAGE FREE. HEFC AND ROTO. RE-ACCOMPLISHED DECK PLATE REPAIR USING SRM REV 124 CHAPTER 53-60-51-2R-8 REPAIR 8.SDR IPXA2026022344163Seat Track · corrodedF MAIN CABIN FLOOR STRUCTURE, STA 1160-1200 LBL 45 SEAT TRACK CORRODED. REMOVED CORROSION IN SEAT TRACK I.A.W. B757-200 SRM 51-10-02 AND EVALUATED I.A.W. B757-200 SRM 53-00-52-1A-1. REMOVED SEAT TRACK FROM LBL 45 STA 1180 TO STA 1320 IAW B757 SRM 51-40-02. SDR IPXA2026021927248Bracket · crackedFAULT-STR-ZONE 200: AIR COND. DUCT AT CABIN CEILING STA 1680 SUPPORT BRACKET IS CRACKED. REMOVED MAIN CABIN SUPPORT BRACKET IAW B757-200PF SRM 51-40-02 INSTALLED NEW BRACKET IAW SRM 51-40-02SDR IPXA2026023834460Seat Track · dentedMAIN CARGO COMPARTMENT FLOOR STRUCTURE, BL 0 SEAT TRACK HAS (1EA) DENT. REMOVED DAMAGED SECTION OF SEAT TRACK IAW SRM 53-00-52-2R-7 STEP 2 AND SRM 51-40-02-0G-0 INSTALLED REPAIR PARTS IAW SRM 53-00-52-2R-7, STEP 10, AND SRM 51-40-02-0G-0.SDR IPXA2026021939888Support Angle · corrodedMAIN CABIN FLOOR STRUCTURE, STA 1720 LBL 20 LOWER NUTPLATE ANGLE SUPPORT CORRODED. REMOVED LOWER NUTPLATE ANGLE SUPPORT CORRODED I.A.W. B757-200 SRM 51-40-02-0G-0 INSTALLED LOWER NUTPLATE ANGLE SUPPORT I.A.W. 757-200 SRM 51-40-02-0G-0..SDR IPXA2026021939793Support Angle · corrodedMAIN CABIN FLOOR STRUCTURE, STA 1720 LBL 45 LOWER NUTPLATE ANGLE SUPPORT CORRODED. DOT 28-05 .REMOVED LOWER NUTPLATE ANGLE SUPPORT CORRODED I.A.W. B757-200 SRM 51-40-02-0G-0 INSTALLED LOWER NUTPLATE ANGLE SUPPORT I.A.W. 757-200 SRM 51-40-02-0G-0.SDR IPXA2026021940348Support Angle · corrodedMAIN CABIN FLOOR STRUCTURE, STA 1720 RBL 10 LOWER NUTPLATE ANGLE SUPPORT CORRODED. REMOVED LOWER NUTPLATE ANGLE SUPPORT CORRODED IAW SRM 51-40-02-0G-0 INSTALLED LOWER NUTPLATE ANGLE SUPPORT IAW SRM 51-40-02-0G-0.SDR IPXA2026021241625Deck Plate · corrodedMAIN CABIN FLOOR STRUCTURE, DECK PLATE STA 1700-1720 BL0 -RBL 50 HAS 15EA AREAS WITH CORROSION. REMOVED CORROSION IN 15 AREAS. MAIN CABIN FLOOR STRUCTURE, DECK PLATE BS 1700-1720, BL0 -RBL 50.IAW SRM 51-10-02 TABLE 101. RESTORED SURFACE PROTECTION IAW.SRM 5SDR IPXA2026021874039Bracket · corrodedACCESS DOOR 313AL LH AND RH LATCH STOPS AT THE CUT-OUT, 4EA BRACKETS ARE CORRODED. REMOVED 4EA BRACKETS WITH CORROSION I.A.W. SRM 51-40-02-0G-0. INSTALLED 4EA BRACKETS ACCESS DOOR 313AL LH AND RH LATCH STOPS AT THE CUT-OUT IAW B757-200 SRM 51-40-02.SDR IPXA2026021188165Skin · crackedAFT CARGO DOOR EXTERNAL SKIN HAS A 2" CRACK APPROX. AT THE LOWER AFT SECTION. DOT 21-01 THIS REQUIRES SUPPLIMENTAL INSPECTION AT THRESHOLD OF 37,500 FC REPEAT INSPECTION WITHIN 3000 FC DEFERRED IAW B757-200PF SRM 52-30-2R-4, REPAIR 4.SDR IPXA2026022369212Skin · crackedLT WING FIXED L/E UPPER COMPOSITE SKIN HAS CRACKS UNDER SLAT NR 4. EVALUATED LT WING FIXED L/E UPPER COMPOSITE SKIN UNDER SLAT NR 4. FOUND OUT OF LIMITS, IAW SRM 57-41-01-1A-1, TABLE 1 FIGURE 101 ACCOMPLISHED REPAIR PER EO-96538-REQ1 AND VT-MAE EA 757-5741-SDR IPXA2026021699522Seat Track · damagedWHEN TRYING TO REMOVE THE UPPER BUSHING OF THE BROKEN LINK P/N 143N5096-2 WHICH FOUND SEIZED ON ASSY. 143N5405-920, TRACK ASSY AFT HOLE FOUND ELONGATED. SEE ATTACHED PICS. REMOVED ASSY 143N5405-920 WITH HOLE ELONGATED I.A.W. B757-200 SRM 51-40-02-0G-0 INSTALLSDR IPXA2026072066283Floor Panel · damagedMAJOR REPAIR, MCD FLOOR PANEL 242XEF DAMAGED INSTALLED FLOOR PANEL 242XEF REF AMM 53-01-01SDR IPXA2026012666283Floor Panel · damagedMAJOR REPAIR. MCD FLOOR PANEL 242XEF DAMAGED REF ATTACHED IMAGES. CRACK IS ON AFT SIDE TOP FACE OF PANEL. APPROX 15.5€? IN LENGTH. 1€?-1.5€? FROM AFT SIDE OF PANEL. 1.5€? FROM LEFT AND RIGHT SIDES OF PANELSDR IPXA2024112643725Flap System · malfunctioned*SUPPLEMENTAL SDR* * EMERGENCY DECLARED* TE FLAPS DISAGREE RAN QRH PROCEDURE AND LOWERED FLAPS TO 20 FOR LANDING NO HISTORY OF FLIGHT CONTROL ISSUE, PERFORMED OP TEST OF TE FLAPS PER 757 AMM 27-51-00-715-001. SYSTEM OP CHECKS GOOD AT THIS TIME NO CURRENT FAULSDR IPXA2024112243725Warning Light · false activationTE FLAPS DISAGREE RAN QRH PROCEDURE AND LOWERED FLAPS TO 20 FOR LANDING NO HISTORY OF FLIGHT CONTROL ISSUE, PERFORMED OP TEST OF TE FLAPS PER 757 AMM 27-51-00-715-001. SYSTEM OP CHECKS GOOD AT THIS TIME NO CURRENT FAULTS ON FSEU'S AT THIS TIME. OKAY TO CONTINSDR IPXA2024111471839Window · failedATB, EMERGENCY DECLARED, FAINT FUMES IN COCKPIT PRECEDING UNRELIABLE AIRSPEED L/H L 1 WINDSCREEN STARTED ARCING JUST PRIOR TO FUMES SMELL AND CONTINUED FOR APPROX 5 MINUTES WHILE IMC. REPLACED L1 WINDOW W/REF TO AMM 56-11-01 UP TO THE SECOND TORQUE,SDR IPXA2024032260994Skin Panel · corroded*SUPPLEMENTAL SDR* *MAJOR REPAIR* FAULT: EVIDENCE OF CORRISON ON INSIDE SURFACE OF #2 PYLON FWD OF PANEL 443CR. DOT 142-17. ACCOMPLISH EO-89829-REQ1 AND EA 757-5450-27-A3546. AUDIT COMPLETE.SDR IPXA2024032659729Latch · gouged*SUPPLEMENTAL SDR* FAULT - CREW ENTRY DOOR LATCHES UPPER AND LOWER APPEAR TO HAVE GOUGES . 89-237 BLENDED OUT CREW DOOR LATCHES UPPER AND LOWER IAW SREO-14721-REQ001. HFEC PERFORMED ON CREW ENTRY DOOR LATCHES UPPER AND LOWER. NO DEFECTS FOUDN IAW 51-00-21. T96SDR IPXA2024030459729Latch · gougedCREW ENTRY DOOR LATCHES UPPER AND LOWER APPEAR TO HAVE GOUGES . 89-237 APPROVED OPENSDR IPXA2023122865964Panel · dented**SUPPLEMENTAL SDR**LEFT WING LOWER INBD LE ACCESS PANEL #511HB HAS DENT APX 6 INCHES FROM FWD EDGE AND 10 INCHES FROM INBD EDGE.***SM26/LMX4*** INSTALLED NEW PANEL #511HB PER AMM 20-11-00-912-001SDR IPXA2023121365964Access Panel · unknown*SDR FILED OPEN* LEFT WING LOWER INBD LE ACCESS PANEL #511HB HAS DENT APX 6 INCHES FROM FWD EDGE AND 10 INCHES FROM INBD EDGE.***SM26/LMX4*** C/W EO. ITEM REQUIRES REPAIR OR REPLACEMENT WITHIN 10 DAYS WITH REPETITIVE INSPECTIONS AT INTERVALS NOT TO EXCEED EVERSDR IPXA2023050293086Battery · unknownINSPECTION TYPE:NAINTERIOR AND EXTERIOR EMER. LIGHTS WILL NOT ILLUMINATE WITH SWITCH IN "ON" POSITION.R&R EMERGENCY LIGHT BATTERY IAW AMM 33-51-07. OPS CHECK GOOD.SDR IPXA2023050293096Battery Pack · inoperativeINSPECTION TYPE:NAREF: THIS LP ITEM 2. EMERGENCY BATTERY NEEDS REPLACED DUE TO EXPIRED SHELF LIFE.REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-07-902. OPS CHECK NORMAL.SDR IPXA2023031391801Pbe · inoperativeINSPECTION TYPE:NAUNABLE TO REMOVED PBE FROM BRACKET IN LAV.OTDERED PART ON REQ 438809 AND REMOVED BRACKET PER MM 25-64-00-20. JG 0559012, 03\11/23. R/R VELCROW PER BOEING DRW 232N4019-1, REINSTALLED BRACKET AND PBE PER AMM 25-64-00.SDR IPXA2022031079962Skin · noneINSPECTION TYPE:SEG1#2 ENGINE PYLON I/B, EXFOLIATION CORROSION ON INSIDE LIP INSIDE PNL 443GLREPAIRED PER VT MAE EA 757-5450-27-A2856 REV -SDR IPXA2022031079956Skin · noneINSPECTION TYPE:SEG1#2 ENGINE PYLON O/B, EXFOLIATION CORROSION ON INSIDE LIP BEHIND PNL 443ARREPAIRED PER VT MAE EA 757-5450-27-A2856 REV -SDR IPXA2022031079952Frame · noneINSPECTION TYPE:SEG1PREVIOUS REPAIR FOUND DURING FRAME INSPECTION AT STA 1480, S26R.WORKED PER VT MAE EA 757-5360-27-A2845 REV -SDR IPXA2022031079955Skin · noneINSPECTION TYPE:SEG1#1 INBD PYLON INSIDE PANEL 433GR, STRUCTURE HAS EXFOLIATION CORROSION AT AFT LOWER EDGEREPAIRED PER VT MAE EA 757-5450-27-A2855 REV -SDR IPXA2022031079946Frame · noneINSPECTION TYPE:SEG1LOWER FRAME GOUGED AT STA 1380 R/H BY STR 26RREPAIRED PER VT MAE EA 757-5360-27-A2850 REV-SDR IPXA2020032553567Floorbeam · corrodedINSPECTION TYPE:SEGMCD FLOOR BEAM AT 1540 IS CORRODEDREPLACED IAW EO NO:B757- 5310-75846-ASDR IPXA2020032553536Slat · delaminatedINSPECTION TYPE:SEG3RT WING #8 SLAT HAS 4EA DENT DELAMINATIONSREPAIRED IAW SRM 57-43-02-2R-1 AND SRM 51-70-10-2R-2SDR IPXA2020032553548Skin · dentedINSPECTION TYPE:SEG3RH FUSELAGE STA 1540-1560 BETWEEN STR 22R-23R AREA ON FUSELAGE HAS OUTWARD DENTREPAIRED IAW SRM 53-00-01-2R-29SDR IPXA2020032553547Slat · delaminatedINSPECTION TYPE:SEG3LT WING #5 SLAT HAS DINGSREPAIRED IAW SRM 57-43-02-2R-1 AND 51-70-10-2RSDR IPXA2020032553545Slat · delaminatedINSPECTION TYPE:SEG3LT WING #3 SLAT HAS DELAMINATIONSREPAIRED IAW SRM 57-43-02-2R-1 AND SRM 51-70-10-2R-2
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