N354UP
Service difficulty reports · 39
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 = 'N354UP' 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 = 'N354UP' 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 IPXA2026100856727Skin · debondedFAULT - DISBOND - END CAP, R/H WING T/E OUTBD FLAP INBD. MEASURE THE DAMAGE AREA (L:1.5", W:0.1", D:2PLIES, 7" FROM AFT EDGE, AT INBD EDGE). 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-RSDR IPXA2026100857298Skin · crackedFAULT - CRACK - SKIN, R/H WING T/E INBD MAIN FLAP INBD UPPER. (REPAIR). MEASURE THE DAMAGE AREA (DIA:1", 16.5" FROM INBD EDGE, 3.5" FROM AFT EDGE). BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 220 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG I.A.W. 767-300FSDR IPXA2026100553573Former · brokenBROKEN FORMER, LT WING OUTBD L/E FOLDING NOSE INNER SIDE AT OSS 441.60, ADJACENT NR 5 SLAT INBD AUX TRACK. REMOVED DAMAGE FORMER IAW SRM 51-40-02-0G, REV 96. INSTALL NEW FORMER IAW SRM 51-40-02-0G, REV 96, DWG 114T2241, SH 4, REV -, AND SREO-54290-REQ1, RSDR IPXA2026100503114Skin · dentedFAULT - DENT - SKIN , NO.1 ENG NOSE COWL INLET AT 9 O'CLOCK POSITION. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.2", 18.2" FROM L/E, AT 9 O'CLOCK ON THE INNER BARREL OF NO.1 ENG INLET COWL ). FILL THE CUT OUT WITH ADHESIVE CURED AT 200°F FOR SDR IPXA2026100503125Skin · dentedFAULT - DENT - SKIN , NO.1 ENG NOSE COWL INLET AT 3 O'CLOCK POSITION. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.25", 20.5" FROM L/E, AT 3 O'CLOCK ON THE INNER BARREL OF NO.1 ENG INLET COWL ). FILL THE CUT OUT WITH ADHESIVE CURED AT 200°F FORSDR IPXA2026100603239Skin · dentedFAULT - DENT - SKIN , NO.2 ENG NOSE COWL INNER BARREL AT 8 O'CLOCK. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.3", 8.2" FROM T/E, AT 8 O'CLOCK ON THE INNER BARREL OF NO.2 ENG INLET COWL ). FILL THE CUT OUT WITH ADHESIVE CURED AT 200°F FOR 1 SDR IPXA2026100603252Skin · dentedDENTED SKIN , NR 2 ENG NOSE COWL INNER BARREL AT 5 O'CLOCK. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.3", 7" FROM T/E, AT 5 O'CLOCK ON THE INNER BARREL OF NO.2 ENG INLET COWL ). BOND THE SPACER WITH FILM ADHESIVE CURED AT 250°F FOR 2 HOURS SDR IPXA2026100465120Stiffener · crackedMAJOR REPAIR, STIFFENER CRACK AT CENTER FRONT BS 785.9 RBL 33. ACCOMPLISH THE REPAIR I.A.W SRM 57-10-10-2R-2 REV.96 AND EGAT WORK SHEET NO.60769 AND UPS SREO-58151-REQ001 REV2.SDR IPXA2026100465056Stiffener · crackedSTIFFENER CRACK AT CENTER FRONT BS 785.9 LBL 55. ACCOMPLISH THE REPAIR I.A.W SRM 57-10-10-2R-2, REV 96 AND EGAT WORK SHEET NR 60770 AND SREO-58151-REQ001 REV 2.SDR IPXA2025110634788Landing Gear · vibrationHEAVY VIBRATIONS FROM EITHER NOSE GEAR OR MAIN GEAR ON T/O ROLL. INTENSIFIED AS SPEED INCREASED. VERY NOISY AFTER WT OFF WHEELS UNTIL GEAR RETRACTED JACKED NOSE GEAR AND ROTATED NOSE TIRES, FOUND BOTH NOSE TIRES OUT OF ROUND, WORN EXCESSIVELY MORE ON ONE SIDE SDR IPXA2025110521634Switch · brokenEMERGENCY LIGHT SWITCH PANEL, KORRY SWITCH BROKEN €˜UNARMED€? ANNUNCIATOR KORRY LIGHT BROKEN. NIL SPARE AVAILABLE. REMOVED AND REPLACED EMERGENCY LIGHTS CONTROL PANEL IAW AMM 33-51-08 / 401, REV 146. FUNCTION CHECKS SATIS.SDR IPXA2025070103289Gasket · leakingEMERGENCY DECLARED, LEFT HYD QTY ICAS MESSAGE QTY AT.45. PILOT STATED IT DID GO TO ZERO. REMOVED AND REPLACED YDS ELECTROHYDRAULIC SERVOVALVE AND SOLENOID VALVES GASKET PLATES AND PACKINGS PER AMM 22-21-03. OPS AND LEAK CHECK GOOD PER AMM 22-21-03. NO LEAKSSDR IPXA2024092758498Drain · none(FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R) COMPLETED SDR.SDR IPXA2024092360016Angle · crackedFOUND THE ANGLE CRACK AT STA 1578 RBL 80 INBOARD IN BULK CARGO COMPARTMENT RIGHT AREA (REPLACE) REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV. 90. INSTALL NEW PART I.A.W SRM 51-40-02-0G REV. 90 AND BOEING DWG NO.146T5650 SH. 5 REV. C. JOB COMPLETED.SDR IPXA2024092358669Angle · crackedFOUND THE ANGLE CRACK AT STA 1578 LBL 80 OUTBOARD BULK CARGO COMPARTMENT LEFT AREA (REPLACE) I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV.142 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL.SDR IPXA2024092359974Angle · crackedFOUND THE ANGLE CRACK AT STA 1578 RBL 80 OUTBOARD IN BULK CARGO COMPARTMENT RIGHT AREA (REPLACE) I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV.142 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMALSDR IPXA2024091860300Floor Panel · crackedMAJOR REPAIR. FOUND MAIN DECK FLOOR PANEL WITH CRACK DAMAGE, PANEL NO.251XFF, P/N: 146T5869-135 (REPAIR) I.A.W AMM 25-57-05-404-006, AMM 25-58-01-404-005, AMM 25-57-02-404-016 AND AMM 25-58-04-404-015 REV.142 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CSDR IPXA2024091858498None · no discrepancy**SDR FILED OPEN** ADD SDR FOR EO-82173-JIC001 (FUSELAGE DRAIN HOLES INSPECTION AND INSTALLATION AFT OF BS 1725.5 BETWEEN S-36L AND S-36R)SDR IPXA2024091860330Floor Panel · crackedMAJOR REPAIR. FOUND MAIN DECK FLOOR PANEL WITH CRACK DAMAGE. PANEL NO.252UFF, P/N: 146T5869-134 (REPAIR).SDR IPXA2024091860270Floor Panel · dentedMAJOR REPAIR. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE. PANEL NO.231FFF, P/N: 143T5876-99 (REPAIR) I.A.W AMM 25-57-03-404-005, AMM 25-58-01-404-018, AMM 25-57-02-404-016 AND AMM 25-58-03-404-017 REV.142 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHESDR IPXA2024091860190Floor Panel · dentedMAJOR REPAIR. FOUND MAIN DECK FLOOR PANEL WITH DENT DAMAGE. PANEL NO.231VFF P/N: 143T5876-27 (REPAIR) I.A.W AMM 25-57-05-404-006 AND AMM 25-58-04-404-015 REV. 142 INSTALLED MAIN DECK CARGO HANDLING AND CONDITION CHECK NORMAL.SDR IPXA2023041092794Light · inoperativeINSPECTION TYPE:NAEMER LIGHTS COVER SPRING DOES NOT CLEAR TOGGLE SWITCHADJUSTED TOGGLE COVER SPRING ON EMERGENCY LIGHTS CONTROL PANEL OPS CHECK GOOD AT THIS TIME IN REFERENCE TO 767 AMM 33-51-08-404-010SDR IPXA2023010989756Battery Pack · no testDURING PDC FOUND EMG LIGHTS INOP. R & R EMG LIGHT BATT IAW AMM 33-51-07. OPS CHECK SAT.SDR IPXA2020111362324Ecu · failedINSPECTION TYPE: NA ATB-AC OUT OF SERVICE. EMERGENCY DECLARED, LANDED W/OUT INCIDENT, NO EMERGENCY EQUIPMENT USED. APU FAULT, APU SHUTDOWN WHICH RESULTED IN AN AIR TURNBACK. DOWN TO ONE GEN, AS FAULT LIGHT NEVER WENT OUT. APU ECU BITE CHECK SHOWED "DC POWESDR IPXA2020081258951Warning Message · illuminatedAIR TURNBACK. GEAR DISAGREE NOSE AFTER TAKEOFF. NOSE GEAR PIN IN PLACE WITHOUT A STREAMER ATTACHED TO PIN. (NO LOGBOOK ENTRY) REMOVED PIN AS REQUIRED. REMOVED NLG DOWNLOCK, PER AMM 32-00-20-201.SDR IPXA2020052765828Engine · smokeINSPECTION TYPE:N/AWHILE STARTING THE LEFT ENGINE, THE MECHANIC CALLED FOR US TO SHUTDOWN THE LEFT ENGINE DUE TO EXCESSIVE FLUID AND SMOKE COMING FROM THE ENGINE. SHORTLY AFTER WE GOT THE L HYD QTY EICAS AND MASTER CAUTION LIGHT. SHUTDOWN LEFT ENGINE AND RANFOSDR IPXA2018102935437Floor Panel · damagedDAMAGE FOUND ON THE M/D CARGO FLOOR PANEL 251MF AT BS 1208 -1313, LBL 11 - LBL 33. FABRICATED A REPLACEMENT FLOOR PANEL IAW EO B767-5320-9693-I.SDR IPXA2018052129809Compressor · damagedWHILE AIRBORNE, AT THE TOP OF DECENT, THE RIGHT ENGINE THRUST REDUCED TO IDLE POWER ABNORMALLY. AT IDLE THRUST, THE LEFT AND RIGHT ENGINES DIFFERED IN PARAMETERS SIGNIFICANTLY. THE RIGHT THROTTLE WAS UNRESPONSIVE FOR THE REMAINDER OF THE FLIGHT. STALL ISDR IPXA2017061918390Evas Unit · failedCAPTAIN`S EVAS UNIT BLOWER CHECK FAILED IAW MM 25-69-00 PB 401. INSTALLED A SERVICEABLE UNIT BATTERY, BLOWER CHECKED GOOD.SDR IPXA2017050816882Strut · inoperativeFOUND LIFE RAFTS STOWAGE GAS STRUT INOPERATIVE. THE GAS STRUT WAS REPLACED IAW AMM 20-11-00-201, REV 121.SDR IPXA2017033115700Bracket · bentFWD ENTRY DOOR EICAS MESSAGE. FOUND THE BRACKET FOR FWD ENTRY DOOR PROXMITY SENSOR BENT. REPLACED THE BRACKET AND ADJUSTED THE PROXIMTIY SWITCH IAW AMM 52-71-00. PERFORMED DOOR WARNING SENSOR TEST IAW AMM 52-71-00-735-072.SDR IPXA2017030714858Warning System · false activationL FWD ENT DOOR EICAS AFTER BLOCK OUT. ACCOMPLISHED FIM 52-71-00-815-805 AND 32-09-03-815-808 SYS OPS CK NORMAL.SDR IPXA2017010912500Floor Panel · damagedINSPECTION TYPE: C2, M/D CARGO FLOOR PANEL AT BS 654 - 676, DAMAGED. FABRICATES A REPLACEMENT FLOOR PANEL IAW EO B767-5320-9693-I.SDR IPXA2015122196934Light · unknownEXTERIOR EMERGENCY LIGHT INOPERATIVE. CHECKED EXTERIOR EMERGENCY LIGHT, OPS CHECKED OK.SDR IPXA2015080391898Skin · dentedFUSELAGE SKIN DENTED AT BS 632 BETWEEN STRINGERS 34-35L. REPAIRED IAW EO B767-5330-57724B.SDR IPXA2015030586693Lamp · inoperativeEMERGENCY LIGHT BELOW ENTRY DOOR IS INOPERATIVE. RELAMPED EMERGENCY EXTERIOR LIGHT IAW AMM 33-51-16-962-001.SDR IPXA2014070983545Floor Panel · puncturedFLOOR PANEL PUNCTURE DAMAGE APPROXIMATELY .781 X .500 AT POS 6, AFT, RT OF CENTERLINE ACCOMPLISHED EO B767-5320-27379-B, 6 A AND OPENED DEFERRAL FOR RE-CHECK, NLT 81 DAYS, 650 HRS OR 305 CYC.SDR IPXA2014072883546Floor Panel · damagedFOUND A ONE INCH HOLE IN FLOOR PANEL AT 4 RT POSITION. DAMAGE FOUND TO BE MINOR. NO STRUCTURAL INTEGRITY LOST. REPAIRED IAW AMM 25-00-00-308-015.SDR IPXA2014022482030Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL DAMAGED AT FRAMES 9-10, RBL64. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-53448-A.
Back to N354UP