N545JN
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 = 'N545JN' 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 = 'N545JN' 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 2025F00243Fire Detector · failedDISCREPANCY: FIRE DET 2 FAIL.SDR 9WGA2025063054519Spar · corrodedDURING HEAVY CHECK SPARS LOWER VERTICAL STABILIZER INTERNAL STRUCTURE LH SIDE UPPER AREA NEAR STA 1986 THROUGH ACCESS 361BL WAS FOUND CORROSION SPOT. REMOVED CORROSION AT SPARS LOWER VERTICAL STABILIZER INTERNAL STRUCTURE LH SIDE UPPER AREA NEAR STA 1986 ACCESDR 9WGA2025063054518Spar · corrodedDURING HEAVY CHECK SPARS LOWER VERTICAL STABILIZER INTERNAL STRUCTURE LOWER SECTION BETWEEN STA 1927 AND STA 2486 ACCESS PANEL 361BL SUPPORT PLATE WAS FOUND WITH CORROSION SPOTS. REMOVED CORROSION AT SPARS LOWER VERTICAL STABILIZER INTERNAL STRUCTURE LOWER SESDR 9WGA2025063054517Skin · corrodedDURING HEAVY CHECK ON HORIZONTAL STAB AFT FUSELAGE LH UPPER SIDE FOUND LIGHT CORROSION FROM STA 2007 TO STA 2163. REMOVED LITE CORROSION AT HORIZONTAL STABILIZER AFT FUSELAGE LH UPPER SIDE FROM STA 2007 TO STA 2163, MATERIAL REMOVED 0.002, ALODINED AND PRIMEDSDR 9WGA2025072354522Pushrod · corrodedDURING HEAVT CHECK RH INBD/OUTBD ELEVATOR PUSH RODS HAVE CORROSION AS MARKED (REPLACE AS REQUIRED) (PUSH RODS OF ACTUATORS). MAINTENANCE REMOVED AND REPLACED RODS ON RH IB OB ELEVATOR PUSH RODS IAW MD-11 AMM 55-20-03. THE AIRCRAFT WAS APPROVED FOR RETURN TO SDR 9WGA2025072354521Hinge · corrodedDURING HEAVY CHECK RH OUTBD ELEV DETACHABLE HING HAS HARDWARE WITH CORROSION. MAINTENANCE REMOVED AND REPLACED NUTPLATE RH OUTBD ELEV IAW MD-11F SRM 51-31-01-06-0 (HINGE). THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 9WGA2025072354520Pushrod · corrodedDURING HEAVY CHECK RH INBD /OUTB ELEVATOR PUSH RODS HAVE CORROSION AS MARKED (REPLACE AS REQUIRED) (PUSH RODS OF ACTUATORS).SDR 9WGA2025062054516Hinge · wornDURING HEAVY CHECK R/H ELEVATOR HINGE PANELS 346HB, 346FB, 346DB, 346BB, 345FB BARE COMPOSITE MATERIAL. REPAIRED HINGE PANELS # 346HB, 346FB, 346BD, 346BB, 345FB AND 345DB AT R/H ELEVATOR HINGE IAW MD-11 SRM 51-62-01-06-0 PRIMED AND TOP COATED PANEL IAW MD-11SDR 9WGA2025061754513Hinge · roughDURING HEAVY CHECK RH OUTBD ELEV HINGE DAMONER HAS ROUGH MATERIAL (EVALUATE IF WITHIN LIMITS). REMOVED ROUGH MATERIAL AT RH OUTBOARD ELEVATOR HINGE DAMPER MATERIAL. REMOVED 0.001 IAW MD-11 SRM 51-21-01-06-0, ALODINED AND PRIMED AREA IAW MD-11 SRM 51-21-01-06SDR 9WGA2025061754512Rib · corrodedDURING HEAVY CHECK RH OUTB ELEVATOR FOUND CORROSION ON RIB INSTL BEHIND ACCESS PANEL 346BZ. CLEANED CORROSION AT RH OB ELEVATOR BEHIND ACCESS PANEL 346BZ, MATERIAL REMOVED 0.002, ALODINED AND PRIMED AREA IAW MD-11 SRM 51-21-01-06-0. THE AIRCRAFT WAS APPROVEDSDR 9WGA2025061754511Paint · wornDURING HEAVY CHECK RH LE INBOARD ELEVATOR PAINT/PRIMER LAYERS ARE WORN (BARE MATERIAL). RH LE IB ELEVATOR WAS PAINTED IAW MD11F SRM 51-21-02-06-0. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 9WGA2025061354510Rod · looseDURING HEAVY CHECK R/H INBOARD ELEVATOR ROD IS LOOSE. RESECURED HARDWARE R/H INBOARD ELEVATOR ROD IAW MD-11 AMM 20-50-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 9WGA2025070154520Support · crackedDURING HEAVY CHECK MAINTENANCE LT FLAP HINGE SUPPORT WAS FOUND TO BE CRACKED. LT OTBD FLAP HINGE BRACKET ASSY WAS REMOVED AND REPLACED IAW MD-11 AMM 57-53-01. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 9WGA2025070154519Support · crackedDURING HEAVY MAINTENANCE LH FLAP HINGE SUPPORT WAS FOUND CRACKED.SDR 9WGA2025062054515Thrust Reverser · delaminatedDURING HEAVY CHECK ENGINE #3 THRUST REVERSER INBOARD FIXED STRUCTURE (COWL-ASSY) DELAMINATED. REPAIRED AREA AT ENGINE #3 THRUST REVERSER I/B FIXED STRUCTURE IAW MD-11 SRM 51-62-01-06-0. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 9WGA2025062054514Cowling · corrodedDURING HEAVY MAINTENANCE ENGINE #3 THRUST REVERSER OUTBOARD FIXED STRUCTURE (COWL-ASSY) DELAMINATED. REPAIRED AREA AT ENGINE #3 THRUST REVERSER O/B FIXED STRUCTURE (COWL-ASSY) IAW MD-11 SRM 51-62-01-06-0. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 9WGA2025061054503Case · corrodedDURING HEAVY CHECK ENGINE #3 FAN CASE (OUTSIDE) AREA AROUND OF THE OGV'S BOLTS AND NUTS WITH CORROSION (RUSTY). CLEANED CORROSION (RUSTY) AT ENGINE #3 FAN CASE (OUTSIDE) AREA AROUND OGV'S BOLTS AND NUTS IAW MD-11 SRM 51-21-01. THE AIRCRAFT WAS APPROVED FOR RSDR 9WGA2025061054502Case · corrodedDURING HEAVY CHECKENGINE #1 FAN CASE (OUTSIDE) AREA AROUND OF THE OGV'S BOLTS AND NUTS WITH CORROSION. CLEANED CORROSION, APPLIED ALODINE, & PRIMER IAW MD-11 SRM 51-21-01 ON #1 ENGINE FAN CASE BY OGV'S AREA. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 9WGA2025061100004Door · crackedDURING HEAVY MAINTENANCE LEFT AIR CONDITIONING PACK 1 DOOR HAS CRACKED WEB. LEFT AIR CONDITIONING PACK 1 DOOR REPAIRED (WEB) IAW MD-11-F SRM 52-00-00-2R-0. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 9WGA2025061354509Rivet · corrodedDURING HEAVY CHECK ZONE 250 STA 1239 RIVETS WITH RUST (CORROSION) AROUND THE WINDOW. REPLACED RIVETS ZONE 250 STA 1239 THE WINDOW IAW MD-11F SRM 51-35-01-06-0. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 9WGA2025061354508Hinge · corrodedDURING HEAVY CHECK FWD CARGO DOOR HINGE WITH SLIGHT RUST (CORROSION). CLEANED SLIGHT RUST (CORROSION) AT FWD CARGO DOOR HINGE. PRIMED AND TOP COATED AREA IAW MD-11 SRM 51-21-01-06-0. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 9WGA2025061354507Hinge · corrodedDURING HEAVY CHECK MAIN DECK CARGO DOOR HINGE WITH SLIGHT RUST (CORROSION). CLEANED RUST (CORROSION) AT MAIN DECK CARGO DOOR HINGE. PRIMED AND TOP COATED AREA IAW MD-11 SRM 51-35-01-06-0. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 9WGA2025061254506Pressure Blkhd · corrodedDURING HEAVY CHECK FWDPRESSURE BULKHEAD STA 464 (INTERIOR SIDE) WAS FOUND LIGHT CORROSION AT STA R-52 TO R-40. REMOVED LIGHT CORROSION AT FWD PRESSUREBULKHEAD STA 464 R-52 TO R 40, MATERIAL REMOVED 0.001, FOUND WITHIN LIMITS. ALODINED, PRIMED AND TOP COATED SDR 9WGA2025061254505Pressure Blkhd · corrodedDURING HEAVY MAINTENANCE FWD PRESSURE BULKHEAD STA 464 (INTERIORSIDE) STIFFNER WAS FOUND WITH EXFOLIATED CORROSION AT STIFFENER FROM R-52 TO R-40. CLEANED AREA AT FWD PRESSURE BULKHEAD STA 464 (INTERIORSIDE) STIFFENER, AFTER FURTHER EVALUATION FOUND LIGHT CORSDR 9WGA2025060954501Pressure Panel · corrodedDURING HEAVY CHECK HORIZONTAL PRESSURE PANEL, STA 464 (CANTED) - 595 SPOTS OF CORROSION (LIGHT CORROSION) AT ZONES 113 AND 114. REMOVED LIGHT CORROSION AT HORIZONTAL PRESSURE PANEL STA. 464 (CANTED) 515 ZONES 113 AND 114, MATERIAL REMOVED 0.001, IAW MD-11 SRMSDR 9WGA2025100654523Spar · crackedDURING HEAVY CHECK TRANSFERRED FROM DMI# 26493 "PERMANENT REPAIR NEED WITHIN 60 DAYS ON CRACK IN AFT SIDE OF LH WING EXTENDING FROM #1 TANK XFER PUMP HOLE". PERMANENT REPAIR AT REAR SPAR ON AFT SIDE LH WING WAS PERFORMED I.A.W REP-11-545-259-WG AND BOEING REPSDR 2024FA0000800Compressor · stalledDISCREPANCY: ENGINE #2 SUSPECTED COMPRESSOR STALL DURING ROTATION. CA: OPENSDR 9WGA2023121754501Unknown · unknownDISCREPANCY: POSSIBLE TANK 1-2 XFR ON FINAL MAY HAVE CAUSED ENGINE 2 TO FLAME OUT ON FINAL. CORRECTIVE ACTION: AIRCRAFT REFUELED IAW AMM 12-11-02. PERFORMED FUEL SYSTEM TEST PER AMM 28-08-01, TEST SATIS. PERFORMED ENGINE RUN UP PER AMM 71-00-00-000-804, TEST SSDR 9WGA2023060554501Computer · inoperativeDISCREPANCY: AIR RETURN DUE TO AMBER IAS & ALT FOLLOWED BY LOSS OF FD, FOLLOWED BY LOSS OF AUTOTHROTTLE. LOST ABILITY SELECT ALT ON FCP, LEVELED OFF AT 3000. AIRSPEED UNRELIABLE CHECKLIST DISCONNECTED AFS PROBLEM WENT AWAY ENTIRELY. RESELECTED NEW ALT 10000, SSDR 9WGA2023053054502Control Unit · inoperativeAIR RETURN DUE TO UNRELIABLE AIRSPEED. SWITCHING CADC SIDE TO 2, OPS NORMAL. R & R CADC #1 IAW AMM 34-16-01. PERFORM LEAK CHECK ON #1 SYSTEM IAW AMM 34-11-00-700-801. OPS CHECK NORMAL, NO FAULTS NOTED AT THIS TIME.SDR 9WGA2023053054501Cadc · inoperativeDISCREPANCY: CADC 2 FAILURE ON TO. R & R #2 CADC PER AMM 34-16-01. CORRECTIVE ACTION: PERFORMED CADC LEAK CHECK PER AMM 34-11-00-700-801. OPS CHECK NORMAL. NO FAULT NOTED AT THIS TIME.SDR 9WGA2023052854501Unknown · unknownDISCREPANCY: AIR TURN BACK DUE TO, AFTER TAKE-OFF AROUND 1000 FEET AIRSPEED UNRELIABLE. ACCOMPLISHED APPROPRIATE CHECK LIST. PERFORMED FIM 34-11-02. PERFORMED CAPTAIN AND FO PITOT/STATIC LEAK CHECK PER AMM 34-11-00. NO DISCREPANCIES FOUND AT THIS TIME.SDR 9WGA2022011354501Anti-Ice System · blew outDISCREPANCY: CLIMBING OUT OF FL 180 @1000Z LEVEL 1 ENGINE 3 FADEC MAINT FOLLOWED BY A LOUD BANG, THEN N1 ROLLED BACK PAST 41 TO X. CORRECTIVE ACTION: REMOVED AND REPLACED INLET NOSE COWL ANTI-ICE DUCT FORWARD PORTION IAW MD-11 AMM 30-22-09.SDR 9WGA2021121554501None · noneLEVEL 2 FCC 2A DATA FAULT. QRH PROCEDURES PERFORMED.SDR 9WGA2021051154501Fire Detector · intermittentINTERMITTENT FIRE DETECT II FAIL.SDR 9WGA2021041854501Fire Loop · failedFIRE DET 1 LOOP FAIL INFLIGHT.SDR 9WGA2020111554501Fire Warning · illuminatedAIR RETURN DUE TO ENGINE 2 LVL 3 FIRE INDICATION.SDR 9WGA2020100354501Pump · inoperativeTANK 1 & 3 FORWARD PUMP OFF.SDR 9WGA20200120191Tire · leakingIN FLIGHT - L1 TIRE-DIFF PRESS AND TIRE PRESS LOW - THE #6 TIRE SLOWLY DROOP PRESSURE (OVER 30 MINS) TO 49 PSI AND TIRE FAIL L-2 ON #6 ALERT. WE RETURNED TO MIA AND LANDED. FOLLOWED TIRE FAIL CHECKLIST, THE #6 TIRE WAS FLAT BUT NO VISUAL DAMAGE TO AIRCRAFT. INSDR 9WGA52017110801Warning Message · multiple failAT 39,000 FEET, A WARNING ON PNEUMATIC MANIFOLD SYSTEM 3, CLOSED THE BLEED VALVE ON ENGINE 3. AFTER A CABIN RATE ANNUNCIATION, REQUESTED DESCENT TO 31,000 FT, FOLLOWED BY A SECOND RED WARNING ON SYSTEM 1, FOLLOWED BY A RAPID CABIN CLIMB, EVEN THOUGH THE SYSTEMSDR KO0R201705180016Web · crackedRIGHT WING FIXED TRAILING EDGE COMPARTMENT BOX WEB IS CRACKED.SDR KO0R201705180015Panel · crackedNR 3 PYLON PANEL 487AR VENT DUCT HAS A CRACKED CORNER.SDR KO0R201705180014Channel · crackedRIGHT WING FIXED TRAILING EDGE COMPARTMENT AT XORS 350 LOWER CHANNEL IS CRACKED IN 3 PLACES.SDR KO0R201705180013Fuel Tank · corrodedEVIDENCE OF CORROSION AT UPPER SURFACE OF CENTER FUEL TANK AT BS 1229, RBL 60.SDR 9WGA2016112501Regulator Valve · inoperativeENGINE NR 2 FIRE WARNING LEVEL 3 ALERT CLIMBING THROUGH FL190. ENGINE SHUT DOWN. FIRE EXTINGUISHER DISCHARGED. FOUND PRESSURE REGULATOR VALVE (PRV) INOPERATIVE. REPLACED PRV.SDR 9WGA5452016101301Fire Warning · false activationDURING CLIMB, NR 2 ENGINE FIRE WARNING ILLUMINATED. RETURNED TO DEPARTURE. DURING INSPECTION, NO EVIDENCE OF FIRE IN NR 2 ENGINE/PYLON AREA. TROUBLESHOOTING FIRE DETECTION SYSTEM.SDR 9WGA2016090101Fire Warning · false activationON APPROACH, NR 1 ENGINE FIRE DETECTOR ILLUMINATED. ACTIVATED FIRE EXTINGUISHING BOTTLES, 2 EACH AND LANDED UNEVENTFULLY. NO EVIDENCE OF ACTUAL FIRE.SDR 9WGA20151129001O-Ring · damagedENGINE NR 1 OIL LEAKAGE IN FLIGHT. OIL LEAK FROM DAMAGED O RING ON HYD PUMP LOCK OUT KIT, REFERENCE DMI 6588. REPLACED O RING IAW AMM 72-65-11. ENG RUN PERFORMED WITH NO LEAKS NOTED.SDR KO0R201503120027Hinge Fitting · corrodedRIGHT-HAND OUTBOARD FLAP INBOARD HINGE FITTING IS CORRODED.SDR KO0R201503120026Skin · corrodedCORROSION FOUND AT BS 1295 LBL 110 STRINGER 8 UPPER CENTER WING SKIN.
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