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 = 'N495WN' 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 = 'N495WN' 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 SWAA2026083189724Exhaust Duct · fireNR 1 ENG. TAIL PIPE FIRE REPORTED BY ANOTHER AIRCRAFT. EXTINGUISHED AFTER ENGINE SHUTDOWN. FLAMES FOUND TO BE CANDLE FIRE PHENOMENA IN THE EXHAUST PLUG. C/W INSPECTION IAW AMM 71-00-00 NO DEFECTS NOTED. SUBSEQUENT ENGINE RUN NORMAL A/C OK FOR SERVICE..SDR SWAA2026080328107Bolt · looseFWD ENTRY DOOR ASSIST HANDLE WAS LOOSE. TIGHTENED BOLTS ON FED ASSIST HANDLE IAW AMM 52-11-31-400-802, STEP 3.G. (2).SDR SWAA2026080375433Light · inoperativeEMERGENCY LIGHT ON BIN AT ROW 7 - 8 DEF INOPERATIVE. REMOVED & REPLACED EMERGENCY LIGHT ON BIN AT ROW 7 - 8 DEF AND PERFORMED GOOD OPS TEST IAW AMM 33-51-03-960-801.SDR SWAA2026080390865Lamp · burned outRIGHT OVERWING LOWER EMERGENCY EXIT SIGN HAS BURNED OUT BULBS. R & R RT OVERWING LOWER EMERGENCY SIGN LAMPS IAW AMM 33-51-01-960-801.SDR SWAA2026080433329Stiffener · corrodedCORROSION FOUND ON LT L/E STIFFNER COMMON TO NR 4 TAI DUCT TAB AT OFSS 308 SS 73. REMOVED LT L/E STIFFNER COMMON TO NR 4 TAI DUCT TAB AT OFSS 308 SS 73 IAW SRM 51-40-02-0G-0. INSTALLED LT L/E STIFFNER COMMON TO NR 4 TAI DUCT TAB AT OF SS 308 SS 73 IAW SRM 51-4SDR SWAA2026080486563Stiffener · corrodedCORROSION WAS FOUND ON STIFFNER COMMON TO NR 6 TAI DUCT TAB AT OFSS 421 SS 186 [MARKED] REMOVED AND REPLACED STIFFNER COMMON TO NR 6 TAI DUCT TAB AT OFSS 421 SS 186 IAW SRM 51-40-02-0G-0 AND AIPC 57-40-00-17.SDR SWAA2026080371392Stringer Clip · crackedCRACKED STRINGER CLIP, BS 727A, S7L. REMOVED, FABRICATED, AND INSTALLED THE STRINGER CLIP IAW SRM 51-40-02-0G-0, AND DWG 146A1101, SHEET 15, REV -.SDR SWAA2026080369769Stringer Clip · crackedCRACKED STRINGER CLIP, BS 727A, S6L. REMOVED, FABRICATED, AND INSTALLED THE STRINGER CLIP IAW SRM 51-40-02-0G-0, AND DWG 146A1101, SHEET 15, REV -.SDR SWAA2026080388192Stringer Clip · crackedCRACKED STRINGER CLIP, BS 727B, S7L. REPLACED THE STRINGER CLIP IAW SRM 51-40-02-0G-0, AND DWG 146A1102, SHEET 15, REV -.SDR SWAA2026080393981Stringer Clip · crackedCRACKED STRINGER CLIP AT BS 727E, S3L. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02, AND DOCUMENT NR 146A1112, DWG 0009, REV-.SDR SWAA2026080328655Stringer Clip · crackedCRACKED STRINGER CLIP AT PAX CABIN, BS 727B, S6L. REMOVED, FABRICATED, AND INSTALLED THE STRINGER CLIP IAW SRM 51-40-02-0G-0, AND DWG 146A1102, SHEET 15, REV -.SDR SWAA2026080388797Stringer Clip · crackedCRACKED STRINGER CLIP AT BS 727E, S4L. REMOVED, FABRICATED, AND INSTALLED THE STRINGER CLIP IAW SRM 51-40-02-0G-0, AND DWG 146A1112, SHEET 09, REV -.SDR SWAA2026080388195Stringer Clip · crackedCRACKED STRINGER CLIP, BS 727E, S5L. REMOVED, FABRICATED, AND INSTALLED THE STRINGER CLIP IAW SRM 51-40-02-0G-0, & DWG 146A1112, SHEET 09, REV -.SDR SWAA2026080414529Strap · out of toleranceE/E COMPARTMENT, BS 328 BETWEEN S20R TO S22R, FRAME STRAP CONFIGURATION DOES NOT MATCH FIG. 15 PER EO 5311-I-17336-NG REF FAULT TTG8Q0157B6V AS PER EA 26-153-01902 THE CONFIGURATION IS ACCEPTABLE. VERIFIED CORRECTIVE ACTION 1SDR SWAA2026061111332Tailpipe · fireTAILPIPE FIRE REPORTED BY SEVERAL AIRCRAFT IN THE LEFT ENGINE WITH FLAMES VISIBLE, WHEN ENGINE WAS SHUTDOWN FLAMES DISAPPEARED BUT SMOKE STILL VISIBLE REPORTED BY FIRE DEPARTMENT; (CONT IN FAULT DESCR (CONT) UPON RETURN TO THE GATE FIRE DEPARTMENT REPORTED SMSDR SWAA2026051803655Screw · looseCREW REPORT L1 DOOR ESCAPE SLIDE MOUNT SCREW LOOSE. SECURED L1 DOOR ESCAPE SLIDE MOUNT SCREW IAW MT 725-61-06.SDR SWAA2026033082539Battery Pack · failedFWD GALLEY EMERGENCY BATTERY PACK RT M1674 FAILED CAPACITY CHECK. R&R CABIN EMERGENCY BATTERY PACK AT M1674 PER AMM 33-51-06;[02] C/W INSPECTIONSDR SWAA2026032380559Coalescer Bag · odorFLIGHT CREW SMELLED SMOKE IN THE COCKPIT AND FLIGHT ATTENDANTS SMELLED SMOKE IN THE CABIN. PERFORMED CONDITIONAL INSPECTION REMOVED AND REPLACED LEFT AND RIGHT COALESCED BAGS; AND REMOVED AND REPLACED CABIN RECIRCULATING AIR HEAP FILTER. PERFORMED ENG AND PASDR SWAA2026032380623Filter · odorFLIGHT CREW SMELLED SMOKE IN THE COCKPIT AND FLIGHT ATTENDANTS SMELLED SMOKE IN THE CABIN. PERFORMED CONDITIONAL INSPECTION REMOVED AND REPLACED LEFT AND RIGHT COALESCED BAGS; AND REMOVED AND REPLACED CABIN RECIRCULATING AIR HEAP FILTER. PERFORMED ENG AND PASDR SWAA2026032080287Computer · inoperativeENGINES WOULD NOT MAKE MAX POWER WITH AUTOTHROTTLE ENGAGE. PERFORMED AUTOTHROTTLE SYSTEM OPERATIONAL TEST IAW AMM 22-31-00. OPS CHECKS GOOD. NO FURTHER FAULTS NOTED. MEL CLEARED. REF LP# 3078430 FOR CAT III RECERTIFICATIONSDR SWAA2026032081730Servo · inoperativeENGINES WOULD NOT MAKE MAX POWER WITH AUTOTHROTTLE ENGAGE.SDR SWAA2025030400992Lamp · inoperativeLH MAIN SERVICE DOOR SLIDE EMERGENCY LIGHT INOP<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-04-960-801-NG (LH MAIN SERVICE DOOR SLIDE EMERGENCY LIGHT - LAMP REPLACEMENT - PERMANENT)]SDR SWAA2024112670914Light · looseSIDE WALL OVERWING EXIT SIGN (FO SIDE) FELL OFF DURING DEPLANING.<[01] REATT. SIDEWALL OVERWING EXIT LIGHT REF. S.I.P.SDR SWAA2024093041425Plate · damagedLH WING UPPER FIXED TRAILING EDGE WIGGLE PANEL COMMON TO 551CT; MOUNT TAB HOLES ELONGATED AND PULLED THRU.<[01] CW NDT INSPECTION OF CUTOUT REF NDT 51-00-00 PROCEDURE 23; NO DEFECTS NOTED AT THIS TIME.;[02] PERFORMED PERMANENT REPAIR ON LH WING FIXED TRAILING SDR SWAA2024092741368Strap · damagedFWD SERVICE DOOR SAFETY STRAP DETERIORATED .<[01] OK TO CONTINUE PER MEL 25-10-01. SP1B;[02] R/R WARNING STRAP ASSY PER SIPSDR SWAA2024092741369Strap · deterioratedFWD ENTRY DOOR SAFETY STRAP DETERIORATED .<[01] OK TO CONTINUE PER MEL 25-10-01. SP1B;[02] R/R WARNING STRAP ASSY PER SIPSDR SWAA2024092338657Handle · loosePAX CABIN FWD ENTRY DOOR LINING ASSISTANT HANDLE LOOSE 2024-489434<[01] CORRECTED INSTALLED PAX CABIN FWD ENTRY DOOR LINING ASSISTANT HANDLE IAW B737- 700 AMM 52-11-31-400-802 STEP 3.G.(2);[02] CERTIFIED WORK PERFORMED.SDR SWAA2024092338663Handle · loosePAX CABIN AFT SERVICE RIGHT DOOR AREA ; FWD CUT OUT ASSISTANT HANDLE LOOSE 2024-489451<[01] PAX CABIN AFT SERVICE RIGHT DOOR AREA FWD CUT OUT ASSISTANT HANDLE TIGHTENED IAW B737-700 AMM 25-21-25-420-801 STEP 3 B.(5);[02] CERTIFIED WORK PERFORMEDSDR SWAA2024091930026Window Frame · crackedCRACK WINDOW 3 FRAME LT SIDE AT COCKPIT 2024-489385<[01] PERFORMED A PERMANET REPAIR ON WINDOW 3 FRAME LT SIDE AT COCKPIT IAW EA- 24-153-02350-WIP1 [TTG8Q00VGP0W]; EA-24-153-02350-WIP2 [TTG8Q00VPE70]; 24-153-02350-WIP3 [TTG8Q00VT5E5]; 24-153-02350-WIP4 [TTG8Q0SDR SWAA2024092025383Web · crackedCRACK ON WEB LOCATED BTW BS 500D TO BS 520 AT LEVEL STR 28R AT FWD CARGO COMPARTMENT 2024-489315<[01] REPLACED WEB AND FASTENERS LOCATED BTW BS 500D TO BS 520 AT LEVEL STR 28R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G-0 ITEM 9;B737-700 SRM 51-40-02SDR SWAA2024092025381Angle · crackedCRACK ON SUPPORT ANGLE LOCATED AT FACE BS 500D AT LEVEL STR 28L AT FWD CARGO COMPARTMENT 2024-489311<[01] REPLACED ANGLE LOCATED AT FACE BS 500D AT LEVEL STR 28L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9 SRM 51-40-02 AND DRAWING 143A7902 SSDR SWAA2024091925379Stringer · crackedCRACK STRINGER 25L LOCATED BS 540 AT FWD CARGO COMPARTMENT 2024-489309<[01] TOOL USED: ULTRASONIC EQUIPMENT P/N 45MG S/N 13066401 DUE DATE: 05-OCT-24.;[02] TOOL USED ON STEP 9: EDDY CURRENT EQUIPMENT; P/N: NORTEC 600D; S/N:210138003; DUE DATE: 11-JUN-25.;[03] SDR SWAA2024091925380Stringer · crackedCRACK ON STRINGER 27L LOCATED BS 540 AT FWD CARGO COMPARTMENT 2024-489310<[01] TOOL USED: ULTRASONIC EQUIPMENT P/N 45MG S/N 13066401 DUE DATE: 05-OCT-24.;[02] TOOL USED: ULTRASONIC EQUIPMENT P/N 45MG S/N 13066401 DUE DATE: 05-OCT-24.;[03] TOOL USED ON STEP 8: SDR SWAA2024091925382Stringer · crackedCRACK ON STR 26L LOCATED BS 540 AT FWD CARGO COMPARTMENT 2024-489314<[01] TOOL USED: ULTRASONIC EQUIPMENT P/N 45MG S/N 13066401 DUE DATE: 05-OCT-24.;[02] TOOLS USED TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25 AND TEMPERATURESDR SWAA2024092325378Balance Arm · corrodedCUSTOMER REQUESTS CORROSION ON LE OF RUDDER BALANCE ARM AT VERTICAL STABILIZER 2024-489272<[01] REPLACED RUDDER BALANCE ARM WEIGHT IAW BOEING 737 CMM 55-40-09.SEE INDIVIDUAL STEPS SIGN OFF BELOW.;[02] REPLACED RUDDER BALANCE ARM WEIGHT IAW BOEING 737 CMM 55-40SDR SWAA2024092324801Angle · crackedCRACK ANGLE LOCATED BS 867 BETWEEN S-2R TO S-3R AT PASSENGER CABIN 2024-489238<[01] REPLACED ANGLE LOCATED BS 867 BETWEEN S-2R TO S-3R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02;SRM 51-40-02 AND DWG 146A7901 SHEET 58 REV -. MEASURE OF CRACK IS:L=0.035 INCH TSDR SWAA2024092324817Stringer · crackedCRACK TIE CLIP LOCATED BS 277 AND S-10R AT PASSENGER CABIN 2024-489249<[01] REPLACED TIE CLIP LOCATED BS 277 AND S-10R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; DWG 141A1110 SHEET 18 REV- AND DWG 141A8380 SHEET 14 REV-.<BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[0SDR SWAA2024092024810Access Panel · damagedELONGATED HOLE ACCESS PANEL 123YBC AT FWD CARGO COMPARTMENT 2024-489246<[01] FABRICATED PANEL 123YBC AT FWD CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 DWG 453A1210 SHEET: 6 REV:A MATERIAL USED PHENOLIC P/N:BMS8-223TY13CL2GRAB P/O:2022-121290.;[02] FABSDR SWAA2024092024815Access Panel · elongatedELONGATED HOLE ACCESS PANEL 123YCC AT FWD CARGO COMPARTMENT 2024-489248<[01] FABRICATED PANEL 123YCC AT FWD CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 DWG 453A1210 SHEET: 7 REV:A. MATERIAL USED PHENOLIC P/N:BMS8-223TY13CL2GRAB P/O:2022-121290.;[02] FASDR SWAA2024092024813Access Panel · damagedELONGATED HOLE ACCESS PANEL 123YAC AT FWD CARGO COMPARTMENT 2024-489251<[01] FABRICATED PANEL 123YAC AT FWD CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 DWG 453A1210 SHEET: 5 REV:A. MATERIAL USED PHENOLIC P/N:BMS8-223TY13CL2GRAB P/O:2022-121290.;[02] FASDR SWAA2024092024811Light · deterioratedDETERIORATED PHOTOLUMINESCENT STRIP LT AND RT SIDE AT PASSENGER CABIN 2024-489244<[01] REPLACED PHOTOLUMINESCENT STRIP LT AND RT SIDE AT<BR>PASSENGER CABIN IAW B737-700 AMM 33-51-15-400-802;[02] REPLACED PHOTOLUMINESCENT STRIP LT AND RT SIDE AT<BR>PASSENGER CASDR SWAA2024092024807Angle · crackedCRACK ANGLE - CLIP LOCATED STA500C AND STR26L FWD CARGO COMPARTMENT 2024-489239<[01] REPLACED CLIP LOCATED STA500C AND STR26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DRAWING 143A7505 SHEET 6 REV D.;[02] CORRECTED STEP 1 <BSDR SWAA2024092024808Angle · crackedCRACK ANGLE - CLIP LOCATED STA500C AND STR26R FWD CARGO COMPARTMENT 2024-489240<[01] REPLACED ANGLE - CLIP LOCATED STA500C AND STR26R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG# 143A7505 SHEET 6 REV. D;[02] TASK CARD COMPLETED <BR>REPLACED SDR SWAA2024091924821Web · crackedCRACK WEB FRAME BS 259.5 BETWEEN S-8R TO S-9R AT PASSENGER CABIN 2024-489252<[01] ON STEP 5; TOOL USED: EDDY CURRENT INSPECTION; PN: NORTEC 600D; SN: 60009161631; DUE DATE: 11-MAY-25;[02] PERFORMED A PERMANENT REPAIR ON WEB FRAME BS259.5 BETWEEN STR-6R TO STR-SDR SWAA2024091924820Web · crackedCRACK WEB FRAME BS 259.5 BETWEEN S-8L TO S-9L AT PASSENGER CABIN 2024-489254<[01] TOOL USED STEP 5 EDDY CURRENT EQUIPMENT PN: NORTEC 600D SN: 200053402 DUE DATE: 24-AUG-24;[02] REPAIRED FUSELAGE FRAME WEB AT BSTA 259.5 BTW WL 240 & WL 280 AND BTW LBL 20 AND LBSDR SWAA2024091924812Stringer · crackedCRACK STRINGER 7L LOCATED BS 294.5 AT PASSENGER CABIN 2024-489247<[01] TOOL USED : EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138003; DUE DATE: 11-JUN-25.;[05] PERFORMED PERMANENT REPAIR CATEGORY B. LOCATED AT STRINGER 7L AND BTW BS277 TO BS303.9 ASDR SWAA2024091924798Web · crackedCRACK WEB LOCATED RIB 5 AND RIB 6 FRONT SPAR AT RT HORIZONTAL STABILIZER 2024-489228<[01] EQUIPMENT USED P/N: NORTEC 600D; S/N: 220272512; DUE DATE: 08-JAN-25;[02] PERFORMED PERMANENT REPAIR ON WEB LOCATED RIB 5 AND RIB 6 FRONT SPAR AT RT HORIZONTAL STABILIZERSDR SWAA2024092024797Angle · crackedCRACK ON FWD ENTRY DOOR AFT UPPER TARGET ANGLE 2024-489223<[01] REPLACED FWD ENTRY DOOR AFT UPPER TARGET ANGLE IAW B737-700 SRM SRM 51-40-02 AND 51-10-02 ITEM 9;[02] REPLACED FWD ENTRY DOOR AFT UPPER TARGET ANGLE IAW B737-700 SRM SRM 51-40-02 AND 51-10-02 ITEMSDR SWAA2024092324288Strap · crackedCRACK STRAP LOCATED STA440 AND BETWEEN STR20R TO STR21R FWD CARGO COMPARTMENT 2024-489209<[01] REPLACED STRAP LOCATED STA440 AND BETWEEN STR20R TO STR21R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A8200 SHEET 44 REV -;[02] REPLACED STRAP LOCATESDR SWAA2024092024283Support · corrodedCORROSION SUPPORT ZEE LOCATED BETWEEN STA727A TO STA767 AND RBL21 WL156 AFT CARGO COMPARTMENT 2024-489195<[01] REPLACED SUPPORT ZEE AND FASTENERS LOCATED BETWEEN STA727 TO STA 767 AND RBL21 WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02;SRM 51-10-02 AND
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