N363UP

Service difficulty reports · 36

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 = 'N363UP' 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 IPXA2026072237604Adapter · chafedCHAFED BRACKET, NR 2 ENG LT CORE COWL OPEN ROD HOLD BRACKET. REMOVED DAMAGE BRACKETS IAW SRM 51-40-02-0G, REV 55. INSTALLED NEW BRACKETS IAW SRM 51-40-02-0G, REV 55, AND CMM IPL 71-13-23, REV 47.Jul 19, 2026 · N363UP · Boeing 737300 · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026072237841Bracket · chafedCHAFED BRACKET, NR 2 ENG RT CORE COWL OPEN ROD HOLD BRACKET. REMOVED DAMAGE BRACKETS IAW SRM 51-40-02-0G, REV 55. INSTALLED NEW BRACKETS IAW SRM 51-40-02-0G, REV 55, AND CMM IPL 71-13-24, REV 51.Jul 19, 2026 · N363UP · Boeing 767346 · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026072835996Drain Mast · crackedCRACKED MAST, NR 1 ENG LWR DRAIN MAST. IAW AMM 71-71-01-024-001-H00, REV 148, AND AMM 71-71-01-424-005-H00, REV.148, REPLACED THE DRAIN MAST OF NR 1 ENGINE.Jul 19, 2026 · N363UP · Boeing 767346 · Nacelle/Pylon, Main FrameSDR IPXA2026072035996Drain Mast · crackedCRACKED MAST, NR1 ENG LWR DRAIN MAST. (REPLACE)Jul 19, 2026 · N363UP · Boeing 767346 · Engine (Turbine/Turboprop)SDR IPXA2026072422572Skin · crackedCRACKED NR 2 PYLON FAIRING PANEL 447 ELX. ACCOMPLISH THE REPAIR IAW SRM 54-52-70-2R-4, REV 55, AND EGAT WORK SHEET 60557.Jul 18, 2026 · N363UP · Boeing 767346 · Nacelle/Pylon, Plate/SkinSDR IPXA2026072223130Support · crackedCRACKED SUPPORT, LEFT HORIZONTAL STAB BODY SEAL 313CLX LAST ONE FITTING. INSTALLED NEW SUPPORT IAW SRM 51-40-02-0G, REV 55, AND DWG 182T7119, SHT 1, REV D.Jul 18, 2026 · N363UP · Boeing 767346 · Horizontal Stabilizer Miscellaneous StructureSDR IPXA2026072223167Support · crackedCRACK SUPPORT, RIGHT HORIZONTAL STABILIZER BODY SEAL NO.314CRX LAST ONE FITTING. INSTALLED NEW SUPPORT IAW SRM 51-40-02-0G, REV 55, AND DWG 182T7119 SH 1, REV D.Jul 18, 2026 · N363UP · Boeing 767346 · Horizontal Stabilizer Miscellaneous StructureSDR IPXA2026072223255Seal · crackedCRACKED ZEE SEAL, NR 1 PYLON LT AFT FAIRING DOOR CUTOUT LWR, AFT SEAL AREA. INSTALLED FABRICATED ZEE SEAL IAW SRM 51-40-02-0G, REV 55, AND DWG 313T2380, SHT 68, REV A, & DWG 313T2303, SH 90, REV C, & SB 767-54-0109, REV 2.Jul 18, 2026 · N363UP · Boeing 767346 · Nacelle/Pylon, Main FrameSDR IPXA2026072707922Floor Panel · delaminatedTHE FLOOR PANEL IN THE AFT CARGO COMPARTMENT IS DELAMINATED. IAW AMM 53-01-05-404-004, REV 148, INSTALLED THE FLOOR PANEL. CONDITION CHKD NORMAL.Jul 17, 2026 · N363UP · Boeing 767346 · Fuselage Floor PanelSDR IPXA2026072204865Retainer · brokenMISSING ZEE SEAL , NR 2 ENG RT AFT FAIRING LOWER AFT AREA. INSTALLED NEW ZEE SEAL IAW SRM 51-40-02-0G, REV 55, AND DWG NR 313T2380 SH. 68 REV. A.Jul 17, 2026 · N363UP · Boeing 767346 · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026071803780Angle · crackedTHE BULK CARGO INBD ANGLE AT BS 1578, LBL 80 CRACKED. REMOVED DAMAGE ANGLE IAW SRM 51-40-02-0G, REV 55. INSTALLED FABRICATED ANGLE IAW SRM 51-40-02-0G, REV 55, AND DWG 657T1332, SHEET 5, REV A.Jul 17, 2026 · N363UP · Boeing 767346 · Fuselage Miscellaneous StructureSDR IPXA2026071807167Angle · crackedTHE BULK CARGO OUTBOARD ANGLE AT BS 1578 LBL 80 IS CRACKED. INSTALLED NEW ANGLE IAW SRM 51-40-02-0G, REV 55, AND DWG 657T1332, SHT 5, REV A.Jul 17, 2026 · N363UP · Boeing 767346 · Fuselage Miscellaneous StructureSDR IPXA2026072889610Splice Plate · brokenBROKEN SPLICE PLATE, UPPER FACE OF LT WING INBD T/E UPPER FIXED PANEL, WBL 127. INSTALLED NEW SPLICE PLATE IAW SRM 51-40-02-0G, REV 55, AND DWG 113T1900, SHT 1, REV C, AND DWG 113T1603, SHT 1. REV B.Jul 16, 2026 · N363UP · Boeing 767346 · Wing Main, Frame StructureSDR IPXA2026072889321Channel · corrodedLEFT APU DOOR HAS LIGHT CORROSION AT INBD INTERNAL SIDE. ACCOMPLISHED CORROSION DAMAGE REPAIR IAW EO-98128-REQ1, REV1, AND DWG 148T6551, SHEET 3, REV B. JOB COMPLETED.Jul 16, 2026 · N363UP · Boeing 767346 · Auxiliary Power Unit (APU) DoorsSDR IPXA2026072485434Fitting · crackedCRACKED FITTING, NR 1 ENG LT T/R FWD TORQUE BOX UPR ACTUATOR FITTING CRACK. INSTALLED NEW FITTING IAW SRM 51-40-02-0G, REV 55, AND IPC 78-32-21, REV 96.Jul 16, 2026 · N363UP · Boeing 767346 · Engine Thrust ReverserSDR IPXA2026072289584Beam · crackedCRACKED BEAM, NR 2 ENG RT AFT FAIRING LOWER BEAM AFT AREA. NSTALLED NEW BEAM IAW SRM 51-40-02-0G, REV 55, SB 767-54-0109, REV 1, DWG 313T2380, SHT 88, REV A, DWG 313T2303, SHT 90, REV C, DWG 313T2303, SHT 94, REV C, & DWG 313T2303, SHT 95, REV C.Jul 16, 2026 · N363UP · Boeing 767346 · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026072051088Battery Pack · no testFOUND EMERGENCY BATTERY PACK FAILED TO ILLUMINATE FOR 15 MINUTES. IAW AMM 33-51-07-022-001, AND 33-51-07-422-012, REV 148. REPLACED EMERGENCY LIGHT BATTERY PACK.Jul 14, 2026 · N363UP · Boeing 767346 · Emergency LightingSDR IPXA2026071551088Battery Pack · inoperativeFOUND EMERGENCY BATTERY PACK FAILS TO ILLUMINATE FOR 15 MINUTES. (REPLACE).Jul 14, 2026 · N363UP · Boeing 767346 · Emergency LightingSDR 2025FA0000792Rudder Pedal · obstructedFIRST OFFICER’S RUDDER PEDALS STIFF AND REQUIRE EXTRA FORCE. IAW AMM 27-21-05-214-033. RUDDER PEDALS OPERATED THROUGH FULL TRAVEL RANGE, NO OBVIOUS STIFFNESS NOTED. PEDALS MOVED FREELY THROUGH THEIR FULL RANGE WITH RUDDER OPERATING CORRECTLY WITH THE POSITIONov 30, 2025 · N363UP · Boeing 767346 · Rudder Control SystemSDR IPXA2025102909684Window · crackedAIR TURN BACK PRESSURIZATION LEAK AFTER APPROXIMATELY 60 MINUTES ENROUTE-INCREDIBLY LOUD SQUEAL MADE COMM DIFFICULT/ATC+ BETWEEN FLT CREW. NOISE STOPPED BELOW 17000 FEET. ACCOMPLISHED T/S AND INSPECTION IAW AMM 56-11-00-210-016 REV 146. FOUND CRACK APP 3 INCHOct 29, 2025 · N363UP · Boeing 767346 · Flight Compartment WindowsSDR IPXA2025092946537Apu · odorWITH APU ON - TURNING ON FIRST PACK WE ARE HAVING HEAVY OIL SMELL FUMES IN COCKPIT. TS PERFORMED FOR OIL SMELL FUMES IN THE COCKPIT IAW FIM 21-00-21/201 REV 146. OIL SMELL FUMES NOT OBSERVED. AIR CONDITIONING SYSTEM OPERATIONAL TEST PERFORMED WITH APU BLEED IASep 25, 2025 · N363UP · Boeing 767346 · Airborne Auxiliary Power Unit (APU) SystemSDR IPXA2025092546537A/C Pack · odorWITH APU ON, TURNING ON FIRST PACK WE ARE HAVING HEAVY OIL SMELL FUMES IN COCKPIT.Sep 25, 2025 · N363UP · Boeing 767346 · Cabin Cooling SystemSDR IPXA2025062778700Cover · damagedMAIN ENTRY DOOR ARMING LEVER HINGED DOOR COVER DAMAGED REPLACED CREW ENTRY DOOR HINGE COVER IAW. AMM 52-12-02 PB 401 REV. 145. THIS CLOSES DMI. PLACARD REMOVED.Apr 22, 2025 · N363UP · Boeing 767346 · Fuselage, Door HingeSDR IPXA2025042278700Cover · damagedMAIN ENTRY DOOR ARMING LEVER HINGED DOOR COVER DAMAGED DEFERRED PER MEL 52-11-2. DI LOG UPDATED. PLACARD INSTALLED. BROKEN COVER PUT IN PFM WITH HARDWARE ATTACHED.Apr 22, 2025 · N363UP · Boeing 767346 · Passenger/Crew DoorsSDR IPXA2025020393810Windshield · hazeENTIRE RIGHT (FO) WINDSHIELD APPEARS FOGGY/HAZY IE DELAMINATION. ACCOMPLISHED RII FOR WINDOW HEAT CONTROL TERMINAL CONNECTION IAW. GMM 04.02.01 REV. 10.Jan 30, 2025 · N363UP · Boeing 767346 · Flight Compartment WindowsSDR IPXA2024120409724Slat System · malfunctionedLE SLAT ASYM PSEU BITE PERFORMED SATIS IAW FIM 32-09 FT 803 AND OPS CHECKED SATIS IAW AMM 27-81-00/501. NO FAULTS FOUND. PLEASE MONITORDec 3, 2024 · N363UP · Boeing 767346 · Leading Edge Slat Control SystemSDR IPXA2024120243168Slat System · warning messageAFTER TAKEOFF RECEIVED €ŒLE SLAT ASYM EICAS€? T/S C/O IAW FIM 32-09-00/101 FAULT TREE 803 REV 143, PSEU BITE TEST SATIS NO FAULT FOUND. CONNECTOR D4434 CLEANED IAW SWPM 20-10-04 REV 87 & SENSOR S279 MEASURED BETWEEN PIN 9 & 10 GOT 18 OHM, CONNECTOR D4486 CLENov 28, 2024 · N363UP · Boeing 767346 · Leading Edge Slat Control SystemSDR IPXA2024081995256Channel · crackedFAULT - CRACK - SUPPORT AND ANGLE, AFT CGO L/H STA 1153-1175 LBL 77.5 (REPLACE) FABRICATE P/N: 212T3416-4 PER BOEING DWG NO: 212T3416 SH 2 REV."-"; PL REV."B"; PSDL REV."-" AND P/N: 212T3418-1 PER BOEING DWG NO: 212T3418 SH 2 REV."-"; PL REV."C"; PSDL REV."-" Aug 10, 2024 · N363UP · Boeing 767346 · Fuselage Miscellaneous StructureSDR IPXA2024081754222Floor Panel · damagedFOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 814T3538-20. (REPAIR) I.A.W. UPS EO-91096-REQ1 REV.1 COMPLETE THE FAULT.Aug 8, 2024 · N363UP · Boeing 767346 · Fuselage Floor PanelSDR IPXA2024081754196Floor Panel · damagedFOUND MAIN DECK FLOOR PANEL DAMAGE, P/N: 814T3538-68. (REPAIR) I.A.W. UPS EO-91096-REQ1 REV.1 COMPLETE THE FAULT .Aug 8, 2024 · N363UP · Boeing 767346 · Fuselage Floor PanelSDR IPXA2024081431948Drain · none*** SUPPLEMENTAL SDR *** MAJOR REPAIR *** ADD SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) COMPLETED SDR.Aug 7, 2024 · N363UP · Boeing 767346 · Standard Practices/StructuresSDR IPXA2024080731948Drain · noneFUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R. OPENAug 7, 2024 · N363UP · Boeing 767346 · Standard Practices/StructuresSDR IPXA2023101060108Flap System · warning message"FLAP ASYM" LIGHT AND EICAS MSG DURING CLIMB OUT SENSOR 279, TARGET CLEARANCE ADJUSTED, AMM SUBTASK 27-88-01-822-160, REV NO. / DATE : 140 / 11 SEP 2023, OUTBOARD AND INBOARD SLAT AUXILIARY TRACK ROLLERS AND SIDE BRACE LINKS LUBRICATED, REFERENCE: AMM TASK 12-Oct 7, 2023 · N363UP · Boeing 767346 · Trailing Edge FlapsSDR IPXA2018071331627Frame · crackedINSPECTION TYPE:C, CRACK FOUND APPROX 0.2" LENGTH DURING HFEC INSPECTION ON RT STA 903.5 BL 89 BELOW WL 200 AT FRAME INNER CHORD TRANSITION RADIUS. FRAME INNER CHORD TRANSITION RADIUS AT STA 903 RBL 89 CARRIED OUT REPAIR AS PER EO B767-5310-68072-A APPENDIX B.Jul 13, 2018 · N363UP · Boeing 767346 · Fuselage Main, FrameSDR IPXA2018070931455Doubler · corrodedINSPECTION TYPE:C1, FUSELAGE KEELBEAM MANHOLE DOUBLER FROM STA 810-840 FOUND CORROSION. REMOVED DOUBLER AND ANGLE NUT PN: BACN10JN3 FOR ACCESS CORROSION BLENDED OUT REWORK AREA SMOOTHEN SIZE OF RWK L=1.0"X W=0'5" ORIGINAL THK =0'080" MATERIAL REMOVED =0'003" Jul 7, 2018 · N363UP · Boeing 767346 · Fuselage Miscellaneous StructureSDR IPXA201804309058Skin · corrodedINSPECTION TYPE: C4, SURFACE CORROSION FOUND ON THE LOWER FASTENER HOLE OF THE SKIN AT BS 955 TEE FITTING. REMOVED THE SURFACE CORROSION.Apr 25, 2018 · N363UP · Boeing 767346 · Fuselage Main, Plate/Skin
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