N591NW
Service difficulty reports · 166
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 = 'N591NW' 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 = 'N591NW' 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 DALA13051065811Bulb · inoperativeSEVERAL EMERGENCY PATH SEAT LIGHTS BURNED OUT. REPLACED BULB. OPS GOOD.SDR DALA13027675811Unknown · odorCREW REPORTED ACRID ODOR IN THE CABIN AND COCKPIT. PILOTS FOLLOWED QRH AND ODOR WENT AWAY THEN ODOR RETURNED. FLIGHT DIVERTED AS A PRECAUTION. MX REMOVED LT AND RT RECIRCULATION FAN FILTERS. FOUND PIECES OF FILTER IN DUCT ON BOTH SIDES. CLEANED DEBRIS AND RSDR DALA12011475811Support · crackedFCB CEILING PANEL SUPPORT IS CRACKED BELOW BS 720 FLOORBEAM, LBL 24, WL 200. FCB CEILING PANEL SUPPORT IS CRACKED BELOW BS 720 FLOORBEAM, LBL 24, WL 200 C/W PRI 508084-14 REV 2 AND ER/A 508084-14 REV ORIGINAL.SDR DALA12011085811Floor Support · crackedMX DISCOVERED THE FLOOR SUPPORT CRACKED ON LOWER FLANGE AT AFT END OF BS 364.5 LBL 24. R & R CRACKED FLOOR SUPPORT AT BS 364.5, LBL 24, WL 206 IAW SRM 51-40-02.SDR DALA1153355811Connector · looseDURING A SERVICE CHECK, MAINTENANCE FOUND THE EMERGENCY PATHLIGHT AT SEAT 23C INOPERATIVE. MAINTENANCE RESECURED THE CONNECTOR. OPERATIONAL CHECK WAS GOOD.SDR DALA1027955811Skin · damagedDURING LINE CHECK FOUND DAMAGE TO FUSELAGE SKIN AT BS 305 S22R. REPAIRED PER ERA 486183-14 SECTION I, SECTION II OF ERA 486183-14 TO PER ACCOMPLISHED NO LATER THAN 15OCT11 PENDING BOEING DTA APPROVAL.SDR DALA1027335811Panel · delaminatedDURING L-CHECK FOUND DELAMINATION ON THE TOP SIDE OF PANEL 431AT. REPAIRED PER ERA 401869-14.SDR DALA1027345811Skin Panel · crackedDURING L-CHECK FOUND CRACK ON LEFT WING UPPER SURFACE FIXED LEADING EDGE PANEL OSS 438. REPAIRED PER ERA 483182-14.SDR DALA1026695811Skin Panel · damagedDURING L-CHECK FOUND RIGHT WING FIXED LEADING EDGE SKIN PANEL BULGING AND CRACKED AT OSS 436. REPAIRED PER ERA 486181-14.SDR DALA1021005811Support Angle · crackedLT PYLON VERTICAL SUPPORT ANGLE ABOVE SKATE ANGLE CRACKED. R & R CRACKED ANGLE IAW SRM 51-10-02.SDR DALA1020995811Angle · crackedPYLON TO FAIRING FIRESEAL ANGLE CRACKED JUST AFT OF AFT ENG MOUNT. VERIFIED WITH EDDY CURRENT (CRACKS BY 3 FASTENERS FROM OTBD END) REPLACED CRACKED ANGLE IAW SRM 51-10-02.SDR DALA1021065811Angle · crackedPYLON TO FAIRING FIRESEAL ANGLE CRACKED JUST AFT OF AFT ENG MOUNT. VERIFIED WITH EDDY CURRENT (CRACKS BY 3 FASTENERS FROM OTBD END) REPLACED CRACKED ANGLE IAW SRM 51-10-02.SDR DALA1020645811Brake Assy · fireWHILE TAXIING INTO THE GATE, THE BELOW-THE-WING PERSONNEL NOTICED THAT THERE WERE FLAMES COMING FROM THE NR2 AND NR6 BRAKES. ACS EXTINGUISHED FIRE ON BRAKES USING DRY CHEMICAL. FOUND UPPER PISTON PUCK ON NR 1 BRAKE SEPARATED FROM PISTON. INSPECTED AXLES FOR DISDR NWAA073545811Brake Assy · fireDURING ROLL UP TO GATE, NR 1 BRAKE CAUGHT FIRE AND THEN SPREAD TO NR 2 BRAKE. GROUND PERSONNEL USED FIRE EXTINGUISHERS TO EXTINGUISH THE FIRE. THERE WERE NO INJURIES. MAINTENANCE REMOVED AND REPLACED BOTH BRAKES AND TIRES, ALSO CLEANED AND INSPECTED THE MAISDR 0501705811Cartridge · inoperativeNR 1 LEFT OVERWING SLIDE SQUIB LIGHT INOP. FOUND SQUIB BLOWN, REPLACED SQUIB AND RETURNED AIRCRAFT TO SERVICE.SDR 0401645811Line · chafedTHE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). THE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EO 2822-01068-01. OPERATIONA
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