N394UP
Service difficulty reports · 74
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 = 'N394UP' 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 = 'N394UP' 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 IPXA2026052458954Channel · corroded- CORROSION - CHANNEL , R/H MAIN L/G SHOCK STRUT DOOR AFT LOWER CORNER INBD SIDE. INSTALL NEW CHANNEL I.A.W SRM 51-40-02-0G REV.55 AND DWG 113T8201 SH 4 REV: CSDR IPXA2026052436510Filler · corrodedFAULT - CORROSION - FILLER, AFT CGO DOOR FWD LOWER HOOK SUPPORT STRUCTURE, DOOR STA 175, BEAM NO. 10 (REPLACE) INSTALL NEW RADIUS FILLER I.A.W SRM 51-40-02-0G REV.55 AND BOEING DWG NO. 140T2610 SH 1 REV: BSDR IPXA2026052037295Fairing · debonded- DISBOND - PNL , AFT WING TO BODY FAIRING L/H PNL NO : 195PL. I.A.W AMM 53-66-01-404-003 REV.148 INSTALL PNL NO.195PL.SDR IPXA2026052439460Web · corrodedCORROSION - WEB, L/H WING FIXED T/E REAR SPAR STA WS248 FUEL JETTISON TRANSFER VALVE FIXED POINT. I.A.W AMM 28-31-04-404-004 REV 148 INSTALLED THE ACTUATOR OF THE TRANSFER VALVE.SDR IPXA2026052439830Bushing · wornWORN - BUSHING, NR 2 ENG R/H CORE COWL R/H SIDE PRESSURE RELIFE DOOR UPPER AND LOWER SIDE, TOTAL: 2EA. .INSTALL NEW BUSHING I.A.W SRM 51-40-02-0G REV.55 AND GOODRICH AEROSTRUCTURES CMM IPL 71-13-24 REV. 50SDR IPXA2026052237060Depressor · brokenFOUND M/D CGO DOOR AFT CUTOUT DISPRESSOR SEAL BROKEN (2EA). DUE TO TYPO FOUND IN CORRECTIVE ACTION 6, CORRECT REFERENCE SHOULD BE:<BR>INSTALLED THE DEPRESSOR SEAL I.A.W AMM 20-11-00-910-802 REV.148, TORQUED THE SCREW TO 25 IN-LB.SDR IPXA2026052137024Skin · debondedDEBONDED SKIN, RT WING OUTBD FLAP TE WEDGE. (REPAIR) PERFORMED NDT/UT FOR THE REWORKED AREA & PLUS 2" AROUND HEATED AREA ,PER 767 NDT MANUAL PART 1 51-01-01 REV:143 RESULT:NO DEFECT WAS FOUNDSDR IPXA2026052036566Strut · crackedCRACKED, UPPER AND LOWER CHORD, RT WING OUTBD FXD LE CAVITY RIB, OSS 531.71. INSTALLED NEW CHORD IAW SRM 51-40-02-0G REV.55 AND DWG 114T2206, SH 1, REV B, & DWG 112T2000, SH 1, REV G.SDR IPXA2026052039321Seal · brokenBROKEN - SPRING, NR 2 PYLON AFT FAIRING PANEL NR 446CL. INSTALLED NEW SEAL IAW SRM 51-40-02-0G, REV 55 AND DWG 311T2570, SH 1, REV N.SDR IPXA2026052039547Fairing · crackedCRACKED FILLET FAIRING, NO. 2 ENG R/H T/R TRANSLATING COWL INNER SIDE BETWEEN NO. 5 AND NO. 6 BLOCKER DOOR. REMOVED DAMAGE FAIRING BLOCKER I.A.W SRM 51-40-02-0G REV.55. INSTALLED NEW FAIRING BLOCKER I.A.W SRM 51-40-02-0G REV.55 AND IPC 78-32-32 REV.96.SDR IPXA2026052040024Rub Strip · crackedCRACKED RUB STRIP, NR 2 ENG RT CORE COWL INNER SIDE UPPER AREA. INSTALLED NEW WEAR STRIP I.A.W SRM 51-40-02-0G REV.55 AND CMM IPL 71-13-24 REV. 50SDR IPXA2026052040363Rub Strip · crackedCRACKED RUB STRIP, NO. 2 ENG L/H CORE COWL INNER SIDE UPPER AREA. I.A.W. AMM 71-11-06-714-013-H00 REV.148 INSTALLED THE CORE COWL. CONDITION CHECKED NORMAL AND JOB COMPLETED. INSTALL NEW WEAR STRIP I.A.W SRM 51-40-02-0G REV.55 AND GOODRICH AEROSTRUCTURESSDR IPXA2026051740055Bracket · chafedCHAFED BRACKET, NR 2 ENG RT T/R COWL LOWER FWD CLOSURE PANEL T/E. INSTALL A NEW BRACKET IAW SRM 51-40-02-0G, REV 55, AND ST ENGINEERING IPC 78-32-22 REV 96.SDR IPXA2026051739573Bracket · chafedCHAFED BRACKET, NR 2 ENG LT T/R COWL LOWER FWD CLOSURE DOOR T/E. INSTALL A NEW BRACKET IAW SRM 51-40-02-0G, REV 55, AND ST ENGINEERING IPC 78-32-21, REV.96.SDR IPXA2026051939604Adapter · gougedGOUGEED BRACKET, NR 2 ENG LT CORE COWL HOLD-OPEN ROD RECIVER. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G REV.55 AND CMM IPL 71-13-23, REV 47.SDR IPXA2026051939610Bracket · gougedGOUGED BRACKET, NR 2 ENG RT CORE COWL HOLD-OPEN ROD RECEIVER. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G REV.55 AND CMM IPL 71-13-24 REV. 50SDR IPXA2026051739973Duct · chafedCHAFED DUCT, NR 2 ENG RT CORE COWL INNER EXHAUST DUCT L/E AREA. REPAIRED DAMAGE AREA IAW ROHR SB 71-032 REV NR 2.SDR IPXA2026052424954Channel · corrodedCORRODED CHANNEL L/H MAIN L/G SHOCK STRUT FAIRING DOOR AFT LOWER CORNER. (REPLACE) Â INSTALL NEW CHANNEL I.A.W SRM 51-40-02-0G REV.55 AND BOEING DWG NO. 113T8201 SH 4 REV: CSDR IPXA2026052022086Seal · brokenBROKEN SEAL, NR 1 PYLON FAIRING PNL 436CL SPRING SEAL AREA. INSTALL NEW SEAL I.A.W SRM 51-40-02-0G REV.55 AND BOEING DWG NO. 311T2570 SH 1 REV: N.SDR IPXA2026052024998Spring · brokenBROKEN- SPRING, NR 2 PYLON AFT FAIRING PANEL NO. 446CR. INSTALLED NEW SEAL IAW SRM 51-40-02-0G REV.55 AND DWG 311T2570, SH 1, REV N.SDR IPXA2026051721345Longeron · chafedCHAFED LONGERON, NR 1 ENG LT CORE COWL EXTERNAL AFT LWR EDGE. INSTALLED A NEW LONGERON IAW SRM 51-40-02-0G, REV 55, AND CMM IPL 71-13-23, REV 47.SDR IPXA2026051721898Rub Strip · corrodedCORRODED RUB STRIP, NR 1 ENG, LT CORE COWL EXTERNAL L/E RUB STRIP, 8:00 - 9:00 POS. INSTALLED A NEW RUB STRIP IAW SRM 51-40-02-0G, REV 55, AND CMM IPL 71-13-23, REV 47.SDR IPXA2026051721983Bracket · chafedCHAFED BRACKET, NR 1 ENG, RT T/R FWD LWR CLOSURE DOOR T/E AREA. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 55, AND IPC 78-32-22, REV 96.SDR IPXA2026051722065Bracket · chafedCHAFED BRACKET, NR 1 LT T/R FWD LWR CLOSURE DOOR T/E AREA. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 55, AND IPC 78-32-21, REV 96.SDR IPXA2026051722098Angle · crackedCRACKED ANGLE, NR 1 PYLON AFT FAIRING INNER AFT BULKHEAD OTBD SIDE SUPPORT ANGLE. INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO:313T2303 SH 131 REV.- AND BOEING DWG NO: 313T2303 SH. 136 REV. -.SDR IPXA2026051722233Longeron · chafedCHAFED LONGERON NR 1 ENG RT CORE COWL INNER SKIN AFT LWR EDGE. INSTALLED A NEW LONGERON IAW SRM 51-40-02-0G, REV 55, AND CMM IPL 71-13-24, REV. 50.SDR IPXA2026051924905Guard · brokenFOUND LEFT WING INBOARD SLAT TORQUE TUBE GUARD BROKEN AT WBL 121.0. I.A.W AMM 20-11-00-910-802 REV 148 REPLACE LEFT WING INBOARD SLAT TORQUE TUBE GUARD AT WBL 121.0.SDR IPXA2026052012733Angle · crackedFOUND THE ANGLE CRACK AT STA 1578 RBL 80 OUTBOARD IN BULK CARGO COMPARTMENT RIGHT AREA. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV.55 AND BOEING DWG NO:657T1332 SH 5 REV.ASDR IPXA2026052012537Channel · chafedCHAFED CHANNEL, NR 1 ENG R/H T/R AFT LWR FAIRING L/E AREA. INSTALL NEW CHANNEL I.A.W SRM 51-40-02-0G REV.55 AND ST ENGINEERING IPC 78-32-02 REV.96SDR IPXA2026052012545Former · crackedCRACKED FORMER, RT WING OUTBD FXD LE NOSE SKIN, OSS 456.98. INSTALL NEW FORMER I.A.W SRM 51-40-02-0G REV.55 AND BOEING DWG 114T2202 SH 1 REV D AND UPS SREO-57209-REQ001 REV2SDR IPXA2026052012498Angle · crackedFOUND THE ANGLE CRACKED AT STA 1578 RBL 80 INBOARD IN BULK CARGO COMPARTMENT RIGHT AREA INSTALLED NEW ANGLE IAW SRM 51-40-02-0G REV.55 AND BOEING DWG 657T1332 SH 5 REV.A.SDR IPXA2026051912479Fireshield · chafedCHAFED FIRESHIELD, NR 1 ENG FAIRING PANEL 436BL INNER PLATE AREA. INSTALLED A NEW FIRESHIELD IAW SRM 51-40-02-0G, REV 55, & DWG 311T2570, SH 1, REV N.SDR IPXA2026052480150Skin · crackedDURING PERFORM EO-87307-JIC1 FOUND L1 DOOR AFT DOOR CORNER HOLE CRACK. (REPAIR) ACCOMPLISHED THE REPAIR I.A.W SRM 53-10-01-2R-1 REV. 55 AND EGAT WORK SHEET NO: 60372 AND UPS EO-87307-REQ7 REV2.SDR IPXA2026052080887Angle · crackedFOUND THE ANGLE CRACK AT STA 1578 LBL 80 OUTBOARD IN BULK CARGO COMPARTMENT LEFT AREA. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV.55 AND BOEING DWG NO:657T1332 SH 5 REV.ASDR IPXA2026052081117Angle · crackedFOUND THE ANGLE CRACK AT STA 1578 LBL 80 INBOARD IN BULK CARGO COMPARTMENT LEFT AREA. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV.55 AND BOEING DWG NO:657T1332 SH 5 REV.ASDR IPXA202605081013Pawl · wornTHE PAWL BEHIND THE CREW ENTRY DOOR EXTERNAL HANDLE IS WORN. OPENSDR IPXA2024052191404Skin Panel · corroded**SUPPLEMENTAL SDR** FAULT - CORROSION - SKIN, L/H WING INBD INSPAR SKIN WBL 97 (EVALUATE) ACCOMPLISHED REPAIR I.A.W EO-90375-REQ1 REV.1 AND BOEING DWG NO. 112T4000 SH 9 REV. B AND NO. 112T4000 SH 8 REV. JOB COMPLETED. PAPER CHECK OK.SDR IPXA2024052191453Skin · corrodedCORROSION - SKIN, R/H WING OUTBD INSPAR LWR SURFACE DRAIN HOLE CUTOUT AREA, WS 852 (EVALUATE) ACCOMPLISHED REPAIR I.A.W EO-90935-REQ1 REV.1. REVIEW COMPLETEDSDR IPXA2024052096856Support · corrodedCORROSION - CLIP, L/H ENVIRONMENTAL CONTROL BAY LOWER RIB SUPPORT, STA 924, LBL 19 (REPLACE) INSTALLED FABRICATED PART I.A.W SRM 51-40-02-0G REV. 49. AND BOEING DWG NO: 149T7370 SH.1 REV. F.SDR IPXA2024052199027None · none(FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) COMPLETED SDR.SDR IPXA2024052091487Skin Panel · corroded*** SUPPLEMENTAL SDR *** FAULT - EXISTING BLEND LEFT WING TRAILING EDGE OUTBOARD SKIN WS 1046 (EVALUATE) ACCOMPLISH REPAIR I.A.W EO-90394-REQ1 REV. 1. JOB COMPLETED.SDR IPXA2024051791453Skin · corroded**SDR FILED OPEN**FAULT - CORROSION - SKIN, R/H WING OUTBD INSPAR LWR SURFACE DRAIN HOLE CUTOUT AREA, WS 852 (EVALUATE) REVIEW COMPLETEDSDR IPXA2024051691487Skin Panel · corrodedEXISTING BLEND LEFT WING TRAILING EDGE OUTBOARD SKIN WS 1046 (EVALUATE) REVIEW COMPLETESDR IPXA2024050399027None · noneOPEN, FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R.SDR IPXA2024052076482Skin Panel · corrodedCORROSION - SKIN, L/H WING OUTBD VORTEX GENERATORS AREA, WS720 TO WS772. (EVALUATE) ACCOMPLISHED REPAIR I.A.W EO-90376-REQ1 REV.1 AND BOEING DWG NO. 112T3000 SH 16 REV. -.SDR IPXA2024052074092Fitting · corrodedFOUND BULK CARGO COMPARTMENT CEILING AREA FLOOR BEAM FITTING DAMAGED AT STA 1593 LBL 54.5. (REPLACE) I.A.W AMM 53-01-06-400-801 REV.142 INSTALL MAIN DECK CARGO FLOOR PANELS AND CONDITION CHECK NORMALSDR IPXA2024052074066Fitting · corrodedFOUND BULK CARGO COMPARTMENT CEILING AREA FLOOR BEAM FITTING DAMAGED, AT STA 1593 LBL 55. (REPLACE) 1. REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 49. 2. INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV. 49. AND BOEING DWG NO. 657T1332 SH. 7 REV. A. AND 657T133SDR IPXA2024052073956Skin Panel · corroded*** SUPPLEMENTAL SDR *** FAULT - CORROSION - SKIN, L/H WING TO BODY SPLICE LOWER SKIN LOWER SURFACE, STA 792, WBL 97.5. (EVALUATE) ACCOMPLISHED REPAIR I.A.W EO-90393-REQ1 REV.1 AND SRM 51-40-04-0G REV. 49 AND BOEING DWG NO. 112T4323 SH5 REV. C; NO. 112T5000 SHSDR IPXA2024051673956Skin Panel · corrodedCORROSION - SKIN, L/H WING TO BODY SPLICE LOWER SKIN LOWER SURFACE, STA 792, WBL 97.5. (EVALUATE) ACCOMPLISH REPAIR PER EO-90393-REQ1 AND EGAT EI F2024A57M-1171, REV. 4 (REF. T3F18E004H051) PRIOR TO FURTHER FLIGHT.SDR IPXA2024051639459Bulkhead · crackedFOUND NOSE W/W AFT BULKHEAD LH BL25 CHORD CRACK (REPAIR) ACCOMPLISHED REPAIR I.A.W SRM 51-70-12-OG-0 REV.49 AND EGAT WORK SHEET NO.40374. JOB COMPLETED.
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