N226HA
Service difficulty reports · 25
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 = 'N226HA' 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 = 'N226HA' 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 ASAA2026010262645Smoke Warning · false activationSMOKE LAVATORY SMOKE 1 HOUR PRIOR TO LANDING. NO SIGN OF SMOKE OR FIRE IN ANY LAVATORY. GROUNDED - YES. RESET CIDS SDF AND PERFORMED OPS TEST OF ALL LAVATORY SMOKE DETECTION SYSTEMS PER AMM 26-17-00. OPS TEST OK. NO FAULTS NOTED. OK FOR SVC.SDR HALA20251015319Rod · damagedETOPS - RETURN TO GATE AFTER ENG. START DUE TO ENG.1 BLEED FAULT. FOUND FAN AIR VALVE ACTUATOR ROD DAMAGED. REMOVED AND REPLACED ACTUATOR ROD PER AMM 36-11-54-400-803-A. OPS CHECK OF FAN AIR VALVE ACTUATION GOOD W/IDLE RUN. NO FAULTS NOTED. OK FOR SVC.SDR HALA20250812245Control Valve · faultedDIV - AFT CABIN VERY WARM DIV TO OAK: AT TOC NOTICED PACK 2 AMBER ON PRESS PG, BLEED PG. SHOWING NO PRESSURE & IP VALVE CLOSED. MX TROUBLESHOOT IN AIR W/ X BLEED STILL NO PRESSURE, NO RESET. REMOVED & REPLACED #2 FLOW CONTROL VALVE (24HB) PER AMM 21-51-51. PERSDR HALA20250602157Igniter · faultedETOPS - APU AUTO SHUT DOWN TWICE CALLED MX, SHUT DOWN THRID TIME ALSO NOTICED FUEL SLOWLY DRIPPING FROM APU DRAIN MAST. REMOVED AND REPLACD APU IGNTIER PLUG PER AMM 49-41-41 AND APU IGNITION UNIT PER AMM 49-41-38. OPS AND LEAK CHK GOOD. OK FOR SVCSDR HALA20250317016Skin · corrodedCORROSION FOUND ON RHW AILERON AT UPPER EXTERNAL SKIN NEAR TRAILING EDGE AREA. PERFORMED REPAIR IAW RI-HAL-57-023. DAMAGE IS RAISED TO SPEAR DUE TO NO ADL OR REPAIR. SEE SPEAR REF NO. N226HA/B4836/SPEAR001. SEE SJC NR 8027 AND NR 20005, 20006. SILVER DOT APPLISDR HALA20250317015Skin · corrodedCORROSION FOUND ON LHW LOWER SURFACE OUTBOARD SIDE OF PYLON BETWEEN RIBS 8 AND 9. PERFORMED DAMAGE EVALUATION IAW A321N SRM 57-21-11-283-014 FIG 001 SHT 1 REV 35 DTD 01NOV24. REWORK EXTENDS OVER FASTENER HEAD, CONTACT AIRBUS. PERFORMED REPAIR IAW RI-HAL-57-022SDR HALA20250204049Fire Loop · shortedETOPS - ENG 1 FIRE LOOP A APPEARED DURING CLIMB AND ONCE IN FLIGHT. FOUND SHORT TO GROUND ON #1 ENGINE LOOP A HARNESS (4165KS) REMOVED & REPLACED HARNESS PER AMM 26-12-61. FDU 1 TEST OK, OK FOR SERVICE.SDR HALA20250127038Fire Loop · faultedETOPS - DURING CLIMB, WE GOT ECAM ENG 2 FIRE LOOP A FAULT TWICE. BOTH TIMES LASTED UNDER A MINUTE AND CLEARED ON ITS OWN. PERFORMED RESISTANCE TEST PER AMM 26-12-00-810-805-A. FOUND PINS J&K 1.490O, INSULATION RES. PIN J-GRD-0.00MO PINS K TO GRD - 0.00MO. REMOSDR HALA20250124033Overheat Loop · faultedETOPS - INFO TO MAINT: DURING CLIMB, WE GOT ECAM ENG 2 FIRE LOOP A FAULT TWICE. BOTH TIMES LASTED UNDER A MINUTE AND CLEARED ON ITS OWN. PERFORMED RESISTANCE TEST PER AMM 26-12-00-810-805-A. FOUND PINS J&K 1.490O, INSULATION RES. PIN J-GRD-0.00MO PINS K TO GRDSDR HALA20241216366Fire Loop · faultedETOPS - ENG 2 FIRE LOOP B FAULT. REMOVED AND REPLACED #2 ENG AGB FIURE DETECTOR B PER AMM 26-12-17-000-802-A & 26-12-17-400-802-A FAULT CLEARED AND BITE TEST PASS PER 26-12-00-710-002 AC OKAY TO CONTINUESDR HALA20241125332Oil System · leakingATB - ENG 1 OIL DISCREASE DURING FLIGHT. PERFORMED INSP OF THE NO. 4 BEARING SCAVENGE OIL TUBE ASSY ( LR111) PER 772-21-01-31. REMOVED AND REPLACED OIL FILTER AND SERVICED SYSTEM PER AMM 79-21-06. PERFORMED HIGH POWER ENG RUN PER AMM 71-00-00-720-816-A. NO LEASDR HALA20240913045Smoke Detector · no discrepancyINFO TO MX INFLIGHT LAVATORY SMOKE ECAM MSG. NO FIRE OR SMOKE NOTED UPON INSPECTION SUSPECTED PAX VAPING. INFO NOTED BY MX, PERFORMED BITE TEST OF LAV SMOKE WARN TESTS OK, NO DEFECTS NOTED A/C OK TO CONT. REF TSM 26-17-00-710-11--A0SDR HALA20240814224Pump · low pressureETOPS - MULTIPLE HYD Y ENG 2 PUMP LO PR SPURIOUS ALERTS. REMOVED AND REPLACED ENG2 PUMP PRESSURE SWITCH PER AMM 29-13-17. LEAK CK AND OPS CHECK GOOD OK FOR SVC.SDR HALA20240509129Fuel Line · leakingETOPS - APU FUEL LINE LEAKING NEAR AFT LOWER AREA OF APU. PN:3889352-1. IPC 49-21-84-30A ITEM #400. REPLACED APU ACTUATOR SUPPLY PIPE PN:3883952-1 PER AMM 49-32-11 & 49-23-51. OPS CHECK & LEAK CHECK OF OF APU OK.SDR HALA20240506123Filter · missingETOPS - FOUND #1 GREEN HYD CASE DRAIN FILTER ASSY MISSING. INSTALLED #1 GREEEN HYD CASE DRAIN FILTER ASSY PER AMM 29-11-43-803-A. PENDING OPS AND LEAK. OPS & LEAK CHECK OK. OK FOR SVC.SDR HALA20240506122Wire Harness · missingETOPS - ENGINE 2 ESN P770479 MISSING A LOOP HARNESS 4165KS AND MISSING A LOOP ELECTRIC RAIL ASSEMBLY. INSTALLED ENGINE 2 A LOOP ELECTRIC RAMP ASSY PER AMM 26-12-61. OPS CK GOOD.SDR HALA20221229321Seal · not reportedETOPS-#2 ENG #3 BEARING AFT SEAL NESTING.SDR HALA2022090100254None · noneETOPS - ECAM: ANTI ICE ENG 1 SYS FAULT, ENG 1 A-ICE MONG FAULT ILLUMINATED IN DESCENT 1-2 MINUTES // REMOVED AND REPLACED NAI PRESSURE TRANSDUCER (4002DN) REF AMM 30-21-23. OPS TEST GOOD. NO FAULTS NOTED. OK FOR SERVICE.SDR HALA2022071400130Wire Harness · failedETOPS - ENG 2 FADEC SYS FAULT ALERT IN CRUISE. REMOVED AND REPLACED WO3 EEC WIRING HARNESS PER AMM 73-21-63. OPS CHECK GOOD. OK FOR SERVICESDR HALA2022052300103None · noneETOPS - #1 ENGINE HIGH VIB - ENGINE REPLACED PER ENGINEERING REQUEST // REMOVED AND REPLACED #1 ENGINE PER HAL TASKCARD J321-72-WHI-02SDR HALA2022031500077None · noneETOPS - DMI # 204854 ENG 2 FIRE LOOP A FAULT ( ENGINE FIRE DETECTION SYSTEMS LOOP A (EXCEPT FOR ER OPERATIONS BEYOND 120 MINUTES, ONE MAY BE INOPERATIVE ON EACH ENGINE PROVIDED: ASSOCIATED LOOP B IS OPERATIVE / THE ENGINE FIRE TEST IS PERFORMED BEFORE EACH DESDR HALA2021031800037Power Supply · inoperativeEMER EQ - FOUND EMEREGENCY LIGHT SWITCH IN THE ARM POSIOTION WITH NO POWER TO AIRCRAFT. NUMERIOUS EMR LIGHTS THROUGHOUT CABIN INOP. // REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (EPSU) BATTERIES PER AMM 33-51-38. BITE TESE PASSED. OPS CHK GOOD. OK FOR SESDR HALA2021020800013Balance Weight · out of balanceETOPS - #2 N1, HIGH VIBRATION DURING FUNCTION TEST. AMM 71-00-00-710-807-A // REMOVED AND INSTALLED FAN TRIM BALANCE (CA) WEIGHTS AT LOCATIONS 11,13,15 AND 19 AND C2 WEIGHT AT LOCATION 17 (5897) FUNCTION TEST (FAN TRIM BALANCE) PENDING. PERFORMED #2 ENG FUNCTSDR HALA2021011900006Flow Divider · looseETOPS, NR 2 ENGINE HAS FUEL LEAK. FOUND FUEL LINE FROM FLOW DIVIDER LOOSE, TIGHTENED LINE. GROUND RUN AND LEAK CHECK OK. OK FOR SERVICE.SDR HALA2021011200004Sensor · defectiveETOPS, AIR BLEED CLASS 2 ON ECAM PAGE. REMOVED & REPLACED DELTA PRESSURE SENSOR (18HA2), PER AMM 36-11-18.
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