N304UP
Service difficulty reports · 245
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 = 'N304UP' 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 = 'N304UP' 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 IPXA2026071310637Strip · missingFOUND LIFE RAFT STOWAGE BIN CAP STRIP-EDGE MISSING. INSTALLED CAP STRIPE EDGE IAW DWG 232T4150, SHEET 1, REV A, AND PSDL 232T4150, SHEET DL, REV -.SDR IPXA2026070610637Strip · missingFOUND LIFE RAFT STOWAGE BIN CAP STRIP-EDGE MISSING.SDR IPXA2026070694047Rub Strip · chafedCHAFED RUB STRIP, NR 2 ENG RT CORE COWL INNER FACE T/E UPPER SIDE. REMOVED DAMAGE RUB STRIP IAW SRM 51-40-02-0G, REV 95. INSTALLED A NEW RUB STRIP IAW SRM 51-40-02-0G, REV 95, AND CMM IPL 71-13-24, REV 50.SDR IPXA2026070395239Former · crackedCRACKED FORMER, RT WING LE NR 9 SLAT INBD TRACK, OSS 565. INSTALL NEW FORMER IAW SRM 51-40-02-0G, REV 95, SREO-50900-REQ001, REV 2 AND DWG 114T2512, SH 1, REV D.SDR IPXA2026070395238Former · crackedCRACKED FORMER, RT WING NR 8 SLAT OTBD TRACK, OSS 499. INSTALL A NEW FORMER IAW SRM 51-40-02-0G, REV 95, AND SREO-50900-REQ001, REV.2 AND DWG 114T2511, SH 1, REV D.SDR IPXA2026070294028Bracket · chafedCHAFED BRACKET, NR 1 ENG LT CORE COWL OPEN ROD HOLD BRACKET. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 95, AND CMM IPL 71-13-23 REV. 47.SDR IPXA2026070886027Panel · debondedDEBONDED AT RIGHT SIDE HST LEADING EDGE FIXED PANEL INTERNAL SURFACE FROM FS STA 157 TO FS STA 194.SDR IPXA2026070684487Bracket · deformedDEFORMED BRACKET, NR 1 ENG L1 CORE COWL UPPER FLANGE. REMOVED DAMAGED BRACKET IAW SRM 51-40-02-0G, REV 95. INSTALLED THE NEW BRACKET IAW SRM 51-40-02-0G, REV 95, AND CMM IPL 71-13-23, REV 47.SDR IPXA2026070686680Flange · chafedCHAFED FLANGE, NR 1 ENGINE LT THRUST REVERSER LOWER FWD FAIRING AFT SIDE. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G, REV 95. INSTALLED THE NEW BRACKET IAW SRM 51-40-02-0G, REV 95, AND IPC 78-32-21, REV 96.SDR IPXA2026070684503Bracket · chafedCHAFED BRACKET, NR 1 ENG RT CORE COWL OPEN ROD HOLD BRACKET. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G, REV 95. INSTALLED THE NEW BRACKET IAW SRM 51-40-02-0G, REV 95, AND CMM IPL 71-13-24, REV 51.SDR IPXA2026070384542Angle · crackedCRACK ANGLE, RT WING LE CAVITY OSS 531. INSTALL A NEW ANGLE IAW SRM 51-40-02-0G, REV.95, AND DWG 114T2206, SH 1, REV B.SDR IPXA2026070384515Rib · crackedCRACKED RIB, LT WING OTBD L/E UPPER RIB LOWER ANGLE, OSS 549.75. INSTALLED THE NEW RIB ANGLE IAW SRM 51-40-02-0G, REV. 95 AND DWG 114T2207, SH 1, REV B.SDR IPXA2026070283407Wedge · crackedCRACKED WEDGE, RT WING OUTBD FLAP INBD WEDGE. REMOVE THE CRACK MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 220 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG. I.A.W UPS SREO-70175-REQ001 REV.1SDR IPXA2026070866895Angle · wornWORN ANGLE ASSY AND BEARING, NR 2 PYLON LT FAIRING DOOR NR 3 HINGE. REMOVED DAMAGED ANGLE IAW SRM 51-40-02-0G REV. 95. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G REV. 95 AND DWG 313T3310 SHT 2, REV G.SDR IPXA2026070867122Angle · wornWORN ANGLE ASSY BEARING, NR 2 PYLON RT FAIRING DOOR NR 4 HINGE. REMOVED DAMAGE ANGLE IAW SRM 51-40-02-0G REV. 95. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 95 AND DWG 311T3310, SHT 1, REV L.SDR IPXA2026070666884Channel · crackedCRACKED CHANNEL, NR 2 PYLON LOWER FAIRING T/E OTBD SIDE. REMOVED DAMAGED CHANNEL IAW SRM 51-40-02-0G, REV 95. INSTALLED THE NEW CHANNEL IAW SRM 51-40-02-0G, REV 95, DWG 313T3380 SH. 5 REV. H, AND DWG 313T3360, SH 15, REV B.SDR IPXA2026070267641Bracket · wornWORN OUT BRACKET ASSY , NR 2 ENG LT CORE COWL HOLD OPEN ROD STOWAGE. INSTALLED THE NEW BRACKET IAW SRM 51-40-02-0G, REV 95, AND CMM IPL 71-13-23, REV 47.SDR IPXA2026070267274Bracket · wornWORN OUT BRACKET ASSY, NR 2 ENG RT CORE COWL HOLD OPEN ROD STOWAGE. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV 95 AND CMM IPL 71-13-24, REV 50.SDR IPXA2026072622413Strut · damagedFOUND THE LT MLG OUTER CYLINDER INNER SURFACE SCRATCH AND THE GLAND NUT THREADS CORROSION. TASK CARD MXP-32-045-02-1-JIC T3F18E00983AV ISSUED TO REPLACE LT MAIN LANDING GEAR, REMOVAL AND INSTALLATION OF LT MAIN GEAR HAS BEEN COMPLETED AND DOCUMENTED ON THISDR IPXA2026070819890Channel · crackedTHE U CHANNEL ON THE AFT MAIN DECK CARGO DOOR AT BS 632 WAS CRACKED. IAW DWG 453T7019, SHT 1 REV A. REMOVED & REPLACED THE U CHANNEL IAW AMM 20-11-00-910-802, REV 148.SDR IPXA2026070822555Angle · crackedFOUND FIRE DETECTION LOOP FASTENER ANGLE CRACKED AT BS 1562, LBL 96 IN BULK CARGO BAY. REMOVED THE DAMAGED ANGLE IAW SRM 51-40-02-0G, REV 95. INSTALLED A FABRICATED ANGLE IAW SRM 51-40-02-0G, REV 95, & DWG 218T4100, SHT 3, REV B.SDR IPXA2026070121828Antenna · erodedFOUND V.S.T HF ANTENNA (321E) EROSION. REMOVE THE EROSION MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260 F FOR 130 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG.SDR IPXA2026070222600Angle · corrodedFOUND FLOOR SUPPORT CORRODED IN THE AREA AFT OF BULK CARGO BAY AT BS 1588, LBL 33. REMOVED THE DAMAGED ANGLE IAW SRM 51-40-02-0G REV. 95. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G REV 95, DWG 146T5650, SHT 2 REV A AND 146T5650, SHT 3, REV A.SDR IPXA2026070121913Bumper · missingTHE BUMPER IS MISSING FROM THE CREW ENTRY DOORWAY LINING. (REPLACE) INSTALL THE BUMPER IS FROM THE CREW ENTRY DOORWAY LINING. IAW PSDL 411T2240 SH DL REV.A AND DWG 411T2036 SH1 REV.H.SDR IPXA2026062421913Bumper · missingTHE BUMPER IS MISSING FROM THE CREW ENTRY DOORWAY LINING.SDR IPXA2026082598212Pawl · worn*** SUPPLEMENTAL SDR *** FAULT - THE PAWL BEHIND THE CREW ENTRY DOOR EXTERNAL HANDLE IS WORN. (REPLACE) REPLACED THE PAWL BEHIND THE CREW ENTRY DOOR EXTERNAL HANDLE. I.A.W AMM 52-11-26-004-001 REV.148 AND AMM 52-11-26-404-003 REV.148. TORQUED THE SCREW TO 35 ISDR IPXA2026062398212Pawl · wornTHE PAWL BEHIND THE CREW ENTRY DOOR EXTERNAL HANDLE IS WORN.SDR IPXA2026062915824Fan Cowl · dentedRIGHT ENGINE OTBD FAN COWL OUTER SKIN TWO DENTS AT 1 O'CLOCK POSITION IAW AMM 71-11-04-714-002-H00, REV 148, INSTALLED THE FAN COWL OF NR 2 ENGINE. CONDITION CHECKED IS SATISFACTORY.SDR IPXA2025052801275Crank Assy · inoperative**SUPPLEMENTAL SDR** CAPT #2 WINDOW CRANK IS BINDING WHEN TRYING TO OPEN FOUND AFT OUTBOARD GEARBOX TO BE SERVICEABLE, RE-INSTALLED SAME AFT OUTBOARD GEARBOX, FINISHED INSTALLING FORWARD GEARBOX AND INSTALLED A SERVICEABLE AFT INBOARD GEARBOX WITH A NEW RUBBERSDR IPXA2025052101275Roller · out of adjust*** SDR FILED OPEN *** CAPT #2 WINDOW CRANK IS BINDING WHEN TRYING TO OPEN ADJUSTED AFT LINK ARM AND AFT UPPER ROLLER CLUSTER PER AMM 56-11-02. CRANK CLUTCH STILL BREAKING OVER WHEN CLOSING.SDR IPXA2024071613354Skin · gougedMAJOR REPAIR - GOUGES - SKIN, R/H WING NO.8 SLAT INNER SURFACE UPPER SIDE. (REPAIR) REPAIR I/A/W B767-300F (REV. 89) SRM 51-70-10-2R-4 AND 51-70-10-2R-0 PER SRM 57-43-02-2R-1 (DETAIL III).SDR IPXA2024072905616Spline · crackedFOUND ENTRY DOOR FWD SIDE DOORWAY LINING SPLINE - TRIM CRACK IAW AMM 52-12-02-004-001 REV.142 AND AMM 52-12-02-404-025 REV.142 REPLACED DOORWAY SPLINE TRIM. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR IPXA2024071505616Liner · crackedFOUND ENTRY DOOR FWD SIDE DOORWAY LINING SPLINE - TRIM CRACK. OK TO WORK. OPENSDR IPXA2024072975073Hinge · deformedFOUND MAIN ENTRY DOOR DOORWAY ARMING LEVER HINGE ASSY DEFORM. (REPLACE) I.A.W AMM 52-12-02-404-025 REV.142 INSTALLED DOORWAY LINING. I.A.W AMM 33-51-01-402-030 REV.142 PERFORM EXIT SIGN LAMP TEST WAS NORMAL. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR IPXA2024072677503Stringer · corroded*SUPPLEMENTAL SDR* FAULT - CORROSION SKIN AFT CARGO COMPARTMENT LOWER AT STA 1175~STA 1197+11, S-36R. (REPAIR) ACCOMPLISHED REPAIR I.A.W UPS EO-98978-REQ1 REV.1 AND EGAT EI NO.F2024A53M-1771 REV.2. REVIEWEDSDR IPXA2024072076571Bracket · crackedCRACKED BRACKET MEC INTERIOR COMPARTMENT LH FWD UPPER FLIGHT DECK COCKPIT FLOOR BEAM SUPPORT AT STA 246 LBL 50. (REPLACE) 1.FABRICATE P/N(141T5146-16) PER BOEING DWG NO.141T5146 SH 15 REV."B";PL REV."F";PSDL REV."-"AND ORIGINAL PART AS A SAMPLE I.A.W. GMM-MTX SDR IPXA2024071976451Angle · crackedCRACKED ANGLE BULK CARGO COMPARTMENT RIGHT AREA STA 1578 LBL 60. (REPLACE) REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.89. INSTALLED NEW PARTS I.A.W SRM 51-40-02-0G REV.89 AND BOEING DWG NO:146T5650 SH 5 REV.C. I.A.W AMM 25-59-01-404-019 REV 142 INSTALLED MSDR IPXA2024071976402Angle · crackedCRACKED ANGLE BULK CARGO COMPARTMENT RIGHT AREA STA 1578 RBL 60. REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.89. INSTALLED NEW PARTS I.A.W SRM 51-40-02-0G REV.89 AND BOEING DWG NO:146T5650 SH 5 REV.C. I.A.W AMM 25-59-01-404-019 REV 142 INSTALLED MAIN DECK SDR IPXA2024071877503Skin · corrodedCORROSION SKIN AFT CARGO COMPARTMENT LOWER AT STA 1175~STA 1197+11, S-36R. (REPAIR) PERFORM NDT INSPECTION I.A.W EGAT EI NO.F2024A53M-1771 SEQUENCE B PARTA STEP 1.2)~1.4)SDR IPXA2024071276599Floor Panel · dentedFOUND MAIN DECK FLOOR PANEL DENT, PANEL NO: 231DFF, P/N: 143T5876-37. (REPAIR) FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.3. I.A.W AMM 53-01-06-400-801 REV.142 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL. I.A.W AMM 25-57-03-404-SDR IPXA2024071276585Floor Panel · dentedFOUND MAIN DECK FLOOR PANEL DENT, PANEL NO: 231CFF, P/N: 143T5876-39. (REPAIR) FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.3. I.A.W AMM 53-01-06-400-801 REV.142 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL. I.A.W AMM 25-57-02-404-SDR IPXA2024071275073Hinge · deformedFOUND MAIN ENTRY DOOR DOORWAY ARMING LEVER HINGE ASSY DEFORM. (REPLACE) OK TO WORKSDR IPXA2024071276610Floor Panel · dentedFOUND MAIN DECK FLOOR PANEL DENT, PANEL NO: 252WFF, P/N: 146T5869-55. (REPAIR) FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.3. I.A.W AMM 53-01-06-400-801 REV.142 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL. I.A.W AMM 25-57-02-404-SDR IPXA2024071259276Floor Panel · dentedFOUND MAIN DECK FLOOR PANEL DENT. PANEL NO.251SFF, P/N:146T5869-37 (REPAIR) FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.3. I.A.W AMM 25-57-05-404-006 AND AMM 25-58-01-404-005 AND AMM 25-58-03-404-004 REV 142 RESTORED MAIN DECK CARGO HANDLING. I.A.WSDR IPXA2024071259270Floor Panel · dentedFOUND MAIN DECK FLOOR PANEL DENT. PANEL NO.231QFF, P/N:143T5876-19 (REPAIR) FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.3. I.A.W AMM 53-01-06-400-801 REV.142 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL. I.A.W AMM 25-58-04-404-015SDR IPXA2024071259282Floor Panel · dentedFOUND MAIN DECK FLOOR PANEL DENT, PANEL NO.232AFF, P/N: 143T5876-40 (REPAIR) FABRICATE A NEW FLOOR PANEL I.A.W. SREO-9693-REQ001 REV.3. I.A.W AMM 53-01-06-400-801 REV.142 INSTALL MAIN DECK CARGO FLOOR PANEL AND CONDITION CHECK NORMAL. I.A.W AMM 25-57-02-404-01SDR IPXA2024071041602Inspection · none*SUPPLEMENTAL SDR* FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) C/W EO-82173.SDR IPXA2024070572572Light · inoperativeEMERGENCY LIGHT IN COCKPIT AND PRM CAME ON INFLIGHT. WE HAD NO EICAS MESSAGE. WE CYCLED THE EMERGENCY LIGHT OFF+ON SEVERAL TIMES. FINALLY THE LIGHTS WOULD STAY OFF IN THE ARMED POSITION. EMERGENCY OPERATION CHECK OK PER AMM33-51-00.SDR IPXA2022102187349Warning Message · illuminatedINSPECTION TYPE:N/A**ATB** **EMERGENCY DECLARED** C" HYDR SYS PRESS" CAUTION MESSAGER/R'D CENTER HYD PRESSURE SWITCH AND THEN CENTER HYD SYS OPS CHKD NML. HYD LEAK CHKD OK PER AMM 2911-09-401. AMM 05-51-33 PN ON: 211C223-534, OFF: 211C223-301 SN ON : J019718ACSDR IPXA2022100386790Skin · crackedINSPECTION TYPE:C14CORROSION AND CRACK DAMAGE WAS FOUND ON FUSELAGE SKIN(P/N:146T3241-14) BETWEEN STA 1395-STA 1417,S-38R-S-39R.REPAIR I.A.W BOEING SRID:4-5611978450 AND UPS EO B767-5330-84909-A.
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