N341UP
Service difficulty reports · 91
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 = 'N341UP' 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 = 'N341UP' 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 IPXA2026060273867Seal Depressor · deformedFOUND MAIN DECK SIDE CARGO DOOR UPPER - AFT SIDE DEPRESSOR SEAL DEFORM AND SCRATCH. INSTALLED THE DEPRESSOR SEAL. IAW AMM I.A.W AMM 20-11-00-910-802 REV.148.TORQUED THE SCREW TO 35 IN-LB. CONDITION CHECK NORMAL.SDR IPXA2026060256189Stiffener · crackedCRACKED BRACKET, NR .2 ENG LT T/R FWD TORQUE BOX SUPPORT FITTING NEAR 9:30 AND 10:00 POS. REMOVED DAMAGE BRACKET I.A.W SRM 51-40-02-0G REV. 95. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G REV. 95 AND IPC 78-32-21 REV. 96.SDR IPXA2026060257012Former · crackedRIGHT WING OTBD L/E, NOSE FORMER CRACK, OSS 499.60. REMOVED DAMAGE FORMER IAW SRM 51-40-02-0G REV.95. INSTALL NEW FORMER I.A.W SRM 51-40-02-0G REV.95 AND DWG 114T2161 SH 4 REV.- AND SREO-50900-REQ001 REV.SDR IPXA2026053056047Attach Bracket · crackedCRACK - BRACKET, L/H WING INBOARD L/E COMPARTMENT. (REPLACE) INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV. 95 AND BOEING DWG NO. 114T1240 SH. 6 REV. -.SDR IPXA2026053056997Attach Bracket · crackedRIGHT WING INBOARD L/E CAVITY, PANEL RIB ATTACH BRACKET CRACK, ISS 285. (REPLACE) INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV. 95 AND BOEING DWG NO. 114T1240 SH. 6 REV. -.SDR IPXA2026060158500Skin · crackedRIGHT WING OUTBOARD FLAP, INBOARD T/E END CAP SKIN, UPPER AND LOWER FOUND SKIN DAMAGE. I.A.W UPS SREO-70175-REQ001 REV. 1 PERFORM REPAIR .SDR IPXA2026052956860Support Angle · crackedCRACKED ANGLE , NR 2 PYLON AFT FAIRING INNER AFT FRAME OTBD SIDE SUPPORT ANGLE.SDR IPXA2026052957094Angle · crackedCRACKED ANGLE, NR 1 PYLON AFT FAIRING AFT INNER CAVITY INBD ANGLE CRACK. INSTALL NEW CLIP 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 IPXA2026052946995Angle · crackedTHE BULK CARGO INBOARD ANGLE AT STA 1578 RBL 80 IS CRACKED. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 95 AND BOEING DWG NO. 146T5650 SH. 5 REV. CSDR IPXA2026052947168Angle · unknownTHE BULK CARGO OUTBOARD ANGLE AT STA 1578 LBL 80 IS CRACKED. CONDITION CHECK NORMAL. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 95 AND BOEING DWG NO. 146T5650 SH. 5 REV. CSDR IPXA2026052947183Angle · unknownTHE BULK CARGO INBOARD ANGLE AT BS 1578 LBL 80 IS CRACKED. CONDITION CHECK NORMAL. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 95 AND BOEING DWG NO. 146T5650 SH. 5 REV. CSDR IPXA2026060536086Angle · crackedFOUND THE FIRE DETECTION LOOP FASTENER ANGLE CRACK AT STA 1562 LBL 76 IN BULK CARGO COMPARTMENT. INSTALLED FABRICATED ANGLE I.A.W SRM 51-40-02-0G REV. 95 AND BOEING DWG NO: 218T4100 SHEET 3 REV. B AND 218T4004 SH 23 REV F.SDR IPXA2026052424821Stiffener · crackedCRACKED STIFFENER, FLOOR SUPPORT STRUCTURE STA 785.9 RBL 11. ACCOMPLISH THE REPAIR I.A.W SRM 57-10-10-2R-2 REV. 95 AND EGAT WORK SHEET NO: 60431 AND EO-58151-REQ001 REV1.SDR IPXA2026052425094Stiffener · crackedCRACKED STIFFENER, FLOOR SUPPORT STRUCTURE STA 785.9 LBL 55. ACCOMPLISH THE REPAIR I.A.W SRM 57-10-10-2R-2 REV. 95 AND EGAT WORK SHEET NO: 60432 AND EO-58151-REQ001 REV1.SDR IPXA2026052425098Stiffener · crackedCRACKED STIFFENER, FLOOR SUPPORT STRUCTURE STA 785.9 RBL 55. ACCOMPLISH THE REPAIR I.A.W SRM 57-10-10-2R-2 REV. 95 AND EGAT WORK SHEET NO: 60430 AND EO-58151-REQ001 REV1.SDR IPXA2026052841073Floor Panel · damagedLOADER REPORT LOWER AFT CARGO R/H SIDE NEAR DOORWAY FLOOR PANEL EDGE DAMAGE 1. I.A.W. 767-300F SRM 53-00-50-2R-0 REV. 95 PERFORM REPAIR AS BELOW STEP. :CUT OUT THE DAMAGE AND CLEAN. MEASURE THE CUT OUT ( L : 3.7", W : 0.9", AT AFT EDGE, 3.5" FROM R/H EDGE ). SDR IPXA2024062474860Housing · missingINTERIOR EMG LT. COVER PLATE MISSING LIGHT HOUSING, FWD MAIN ENT DOOR. R/R EMG. EXIT SIGN IAW AMM 33-51-01-022 AND -402. OPS CKS GOOD.SDR IPXA2024052960336Angle · crackedCRACK - ANGLE BULK CARGO COMPARTMENT LEFT AREA STA 1578 LBL 60. I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV.142 RESTORED MAIN DECK CARGO HANDLING. JOB COMPLETED AND CONDITION CHECK NORMAL. REVIEW COMPLETEDSDR IPXA2024052960326Angle · crackedCRACK - ANGLE BULK CARGO COMPARTMENT RIGHT AREA STA 1578 RBL 60. I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV 142 RESTORED MAIN DECK CARGO HANDLING. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR IPXA2024052552655None · noneFUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R.SDR IPXA2024020712214Skin · damagedNR 6 SLAT DAMAGED- BROKEN SKIN SLAT CHANGE INSTALLED INBD SLAT #6 UP TO AND INCLUDING STEP H(15) PER AMM 27-81-01-424-143. C/W REMAINDER OF #6 L/E SLAT INSTALLATION REF AMM 27-81-01-424-143 ITEMS I-K(8). THIS COMPLETES SLAT INSTALL.SDR IPXA2023103012214Unknown · unknownMAJOR REPAIR* #6 SLAT DAMAGED- BROKEN SKIN ASSIGNED EO-88575-PRELIM1 FOR TEMPORARY REPAIR INSTRUCTIONS. OPENSDR IPXA2023091872638Light · inoperativeEMERGENCY LIGHTS INOP R&R EMER SUPPLY BATTERY PACK IAW 767 AMM 33-51-07-002-006. OPS CHECK GOOD. IPC 33-51-07-32SDR IPXA2022050681809Stiffener · crackedINSPECTION TYPE:C6CRACK ON CENTER WING TANK STIFFENER(P/N:111T2008-12)ON STA 785.9, RBL 33.REPAIR I.A.W 767-300F SRM. 83.01, UPS EO B767-5740-58151-C.SDR IPXA2022050881846Floor Panel · damagedINSPECTION TYPE:C6DAMAGE ON M/D CARGO FLOOR PANEL AT STA 287-412, LBL 11-RBL11.FABRICATE THE REPLACEMENT FLOOR PANEL PER EO NO. B767-5320-9693-ISDR IPXA2022041281120Light · inoperativeINSPECTION TYPE:NAEXTERIOR EMERGENCY LIGHT INOPRELAMPED EXTERIOR EMERGENCY LIGHT PER 767 MM 33-51-16-962-001. OPS CHECK NORMALSDR IPXA2020073108417Seal · damagedA LOUD HUMMING NOISE ORIGINATING CLOSE TO CREW ENTRY DOOR. STARTED AT 10000' ON CLIMB OUT AND EDED ABOUT 10000' ON DESCENT.CREW ENTRY DOOR SEALS INSPECTED AND CLEANED AMM 52-09-00. FOUND SMALL CUT IN AFT ACOUSTIC SEAL. SEAL REPAIRED IAW AMM 52-09-00-801. TASK SDR IPXA2020072978304Seal · cutINSPECTION TYPE:N/AA LOUD HUMMING NOISE ORIGINATING CLOSE TO CREW ENTRY DOOR. STARTED AT 10000' ON CLIMB OUT AND EDED ABOUT 10000' ON DESCENT.CREW ENTRY DOOR SEALS INSPECTED AND CLEANED AMM 52-09-00. FOUND SMALL CUT IN AFT ACOUSTIC SEAL. SEAL REPAIRED IAW AMM SDR IPXA2020080328554Seal · not seatedGEAR DOOR VIBRATION ON CLIMB ACCELERATING TO 310KTS LOUD HUMMING AND VIBRATION OCCURS. SLOWED CLIMB SPEED TO 280KTS AND NOISE-VIBRATION WENT AWAY. ON DESCENT AT 310 KTS NOISE - VIBRATION RETURNEDINSPECTED DROOP OF THE FWD NOSE GEAR DOORS IAW AMM 32-22-02, NO DSDR IPXA2019070744175Skin · dentedINSPECTION TYPE:N/A RIGHT WING INBOARD AFT FLAP LOWER SURFACE DENT REPAIR 58 FROM INBOARD EDGE AND 2" FROM TRAILING EDGE. 1/2" DIAMETER AND .043 DEPTH. REPAIRED PER EO B767-5750-72225B. TRANS TO NRC 620420 **SUPPLEMENTAL SDR**REMOVED DAMAGED ON AFT INBOARD FLASDR IPXA2018083133417Unknown · odorMUSTY ODOR FROM AIR CONDTIONING IN COCKPIT, WHEN PACKS WERE ON, AND CONDENSATION IN OUTLETS BOTH PACKS, BITE CHECKED IAW AMM 21.51.00.5 NO LEAKS, THEN PACKS OPERATED AND CYCLED FROM HOT TO COLD CONDENSATION REMOVED AS ACFT WAS IN STORMY WEATHER FOR A COUPLSDR IPXA2018030727224Sensor · out of limitsAIR TURNBACK DUE TO A FWD CARGO DOOR INDICATION. ACCOMPLISHED DMP 52-71-01-01 BY VERIFYING FWD LWR CARGO DOOR CLOSED, LATCHED, AND LOCKED. TROUBLESHOT IAW FIM 52-71-00-815-807, AND TC 52-000-101, FOUND S214 OUT OF SPECS. ADJUSTED , PRESSURIZED AIRCRAFT IASDR IPXA2017101622651Blower · inoperativeLEFT EVAS UNIT BLOWER INOPERATIVE. R & R THE EVAS UNIT IAW 25-69-00-401, OPS CHECKED GOOD.SDR IPXA2017092121941Escape Rope · looseWHEN OPENING THE CREW DOOR, THE EMERGENCY ROPE CAME OFF. THE DOOR WAS STUCK. INGRESS ROPE WAS PROPERLY FIXED AT CREW ENTRY DOOR LOCATION IAW AMM 25-61-04-402-013.SDR IPXA2016021699491Pawl · brokenCREW ENTRY DOOR HANDLE DIFFICULT TO MOVE, OPEN AND CLOSE, DOOR CLOSED IMPROPERLY, OUT OF SEQUENCE.REPOSITIONED UPPER PAWL AND UPPER CEILING PANEL. OPERATIONALLY CHECKED DOOR INSIDE AND OUT IAW AMM 52-12-00-201. OK FOR SERVICE.SDR IPXA2015101094628Shield · missingCAPT'S EVAS CONTAINER IS MISSING DRIP SHIELD. INSTALLED NEW EVAS SPLASH GUARD REF AMM 25-69-00.SDR IPXA2015061490136Floor Panel · damagedTWO DENTS, ONE INCH IN DIAMETER ON MCD FLOOR PANEL. FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693H.SDR IPXA2015061490140Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL, HAS A ONE INCH IN DIAMETER HOLE. FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693-H.SDR IPXA2015060889951Floor Panel · dentedMAIN CARGO DECK NR 2 AFT CENTER FLOOR PANEL HAS A ONE INCH SQUARE DENT. FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693-H.SDR IPXA2015060789909Floor Panel · dentedMAIN CARGO DECK NR 2R AFT OTBD FLOOR PANEL DENTED 14.5". FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693-H.SDR IPXA2015060789901Floor Panel · damagedMAIN CARGO DECK 2R AFT OTBD FLOOR PANEL DENTED 14.5" LONG BY 1" DEEP, FABRICATED A NEW FLOOR PANEL IAW EO B767-5320-9693H.SDR IPXA2015051989231Control Panel · inoperativeEMERGENCY LIGHTS INOPERATIVE, REF M33-51-1-1. REPLACED EMERGENCY LIGHT PANEL ASSY. OPS OK, REF AMM 33-51-08.SDR IPXA2014031482250Channel · damagedCREW ENTRANCE DOOR "SLIDE TAPE" RETENTION SLEEVE DAMAGED. R & R CREW DOOR INGRESS ROPE CHANNEL IAW AMM 25-61-04.SDR IPXA3679981Skin · damaged.8 INCH HOLE IN NR 8 SLAT T/E WEDGE UPPER SKIN 45.8" FROM OTBD END AND 7.5" FWD OF T/E. REPAIRED IAW EO B767-5750-51892-A.SDR IPXA2676481Controller · inoperativeNO CABIN PRESSURIZATION AFTER DEPARTURE. COMPLETED CHECKLIST. FOUND NR 1 AUTO CABIN PRESSURE INOPERATIVE, WOULD NOT SELF TEST. R & R NR 1 AUTO PRESSURE CONTROLLER IAW AMM 21-31-02 AND IPC 21-31-02-01C. SYS CHECKS NORMAL.SDR IPXA12674288Skin · dentedINSPECTION TYPE: 1C, FUSELAGE AT BS 1916 LBL 3" AREA DENT IS FOUND DURING DMI D478160 RECTIFICATION. REPAIRED IAW RS R53-81-37375 REV A & EO B767-5330-47814-A, ORIG MATL: 2024T3-0016" 2 LAYERS BONDED SKIN ASSY. FINAL CUTOUT SIZE: 2" X 2.625", CLASSIFIED AS SDR IPXA12674324Wedge · dentedINSPECTION TYPE: 1C, LT WING OTBD T/E FLAP, T/E WEDGE, LOWER SURFACE DENTED. COMPOSITE PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A (1), FIG 9, REV 52.SDR IPXA12674322Wedge · dentedINSPECTION TYPE:1C LT WING OTBD T/E WEDGE UPPER SURFACE DENTED. COMPOSITE PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1), FIG 9, REV 52.SDR IPXA12674318Wedge · dentedINSPECTION TYPE: 1C, LT WING OTBD T/E FLAP, T/E WEDGE, UPPER SURFACE DENTED. COMPOSITE PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1), FIG 9, REV 52.SDR IPXA12674316Skin · dentedINSPECTION TYPE: 1C, LT WING OTBD T/E FLAP, T/E WEDGE UPPER SURFACE DENTED. COMPOSITE PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1), FIG 9, REV 52.
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