N299WN
Service difficulty reports · 271
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 = 'N299WN' 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 = 'N299WN' 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 SWAA2025052774190Floor Panel · crackedAFT CARGO FLOORBOARD 140BF HAS CRACK<[01] REMOVED AND REPLACED AFT CARGO FLOORBOARD 140BF PER AMM 25-52-10SDR SWAA2024111859793Light · inoperativeL2 DOOR EMERGENCY EXTERIOR LIGHT INOP<[01] RELAMPED LH AFT SLIDE LIGHT IAW AMM 33-51-04SDR SWAA2024090332090Isolator · crackedAFT SERVICE DOOR EMERGENCY ESCAPE SLIDE FWD UPPER ISOLATOR CRACKED<[01] R&R AFT SERVICE DOOR EMERGENCY ESCAPE SLIDE FWD UPPER ISOLATOR IAW SRM 51-40-02.;[02] C/W INSPECTIONSDR SWAA2024082830231Bracket · brokenRT FWD SERVICE DOOR GIRT BAR HAS BROKEN BOLT<[01] R/R. BOTH RIVETS AT FWD SERVICE DOOR GIRT BAR SUPPORT BRACKET REF SRM 51-40-02. NO FURTHER DEFECTS NOTED AT THIS TIME.SDR SWAA2024081926827Shroud · damagedCREW REPORTS FWD SERVICE DOOR SLIDE SHROUD HAS METAL PULLING BACK AT LOWER AFT EDGE<[01] OK TO CONTINUE PER MEL 25-10-01 SP1B;[02] REPAIRED NICK AND CLEANED IAW AMM 20-10-34.SDR SWAA2024012242971Lamp · inoperativeAFT LH EXTERIOR EMERGENCY LIGHT #7 INOP<[01] REMOVED AND REPLACED AFT LH EMERGENCY EXTERIOR LAMP #7 IAW AMM 33-51-04. OPS CHECK GOOD AT THIS TIME.SDR SWAA2024012242970Lamp · inoperativeAFT LH EXTERIOR EMERGENCY LIGHT #5 INOP<[01] REMOVED AND REPLACED AFT LH EXTERIOR EMERGENCY LAMP #5 IAW AMM 33-51-04. OPS CHECK GOOD AT THIS TIME.SDR SWAA2023122133906Bracket · crackedFUSELAGE KEEL BEAM PANEL 192E FORWARD RIGHT MOUNTING BRACKET IS CRACKED.<[01] REMOVED AND REPLACED FUSELAGE KEEL BEAM PANEL 192E FWD RIGHT MOUNTING BRACKET IAW B737 SRM 51-40-02.SDR SWAA2023092101072Slide · out of adjustR2 DOOR SLIDE RUBBING HARD WHEN CLOSING<[01] READJUSTED R2 DOOR SLID GIRT AS PER AMM 25-66-01-400-803;[02] READJUSTED R2 DOOR SLID GIRT AS PER AMM 25-66-01-400-803 AND MT 725-61-06;[03] VERIFIED STEP # 2SDR SWAA2023092100108Battery Pack · inoperativeSEVERAL PASSENGER EMERGENCY LIGHTS INOPERATIVE.<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT POSITION M1673 (AFT R/H SIDE; CEILING) AS PER AMM REF 33-51-06-960-805. TESTED NORMAL AS PER WDM 33-51-14.;[02] REMOVED AND REPLACED EMERGENCY LIGHT BATTESDR SWAA2023092103023Battery Pack · inoperativeSEVERAL PASSENGER EMERGENCY LIGHTS INOPERATIVE.<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT POSITION M1673 (AFT R/H SIDE; CEILING) AS PER AMM REF 33-51-06-960-805. TESTED NORMAL AS PER WDM 33-51-14.;[02] REMOVED AND REPLACED EMERGENCY LIGHT BATTESDR SWAA2023092103024Battery Pack · inoperativeSEVERAL PASSENGER EMERGENCY LIGHTS INOPERATIVE.<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT POSITION M1673 (AFT R/H SIDE; CEILING) AS PER AMM REF 33-51-06-960-805. TESTED NORMAL AS PER WDM 33-51-14.;[02] REMOVED AND REPLACED EMERGENCY LIGHT BATTESDR SWAA2023092199511Fitting · corrodedR1 GIRT BARS FITTING PLATE CORRODED<[01] REPLACED R-1 GIRT BAR FITTING PLATE REF AMM 25-66-02-400-801;[02] VERIFIED STEP 1SDR SWAA2023092199201Panel · crackedPANEL 194E HAS 2EA FASTENER ATTACH HOLES CRACKED OUT; REQUIRES COMPOSITE REPAIR. (FASTENERS CIRCLED) PANEL 194E HAS 2EA FASTENER ATTACH HOLES CRACKED OUT REQUIRES COMPOSITE REPAIR. (FASTENERS CIRCLED)<[01] PREPARED AREA FOR REPAIR; ON WING TO BODY FAIRING PANESDR SWAA2023092194217Strip · corrodedAFT CARGO COMP CAP STRIP BETWEEN STA 767-727D LBL 21' CORRODED<[01] REMOVED CORROSION ON AFT CARGO COMPT CAP STRIP BETWEEN STA 727D TO STA 767 LBL 21 PER REF SRM 51-10-02-0G-0<BR>FOUND WITHIN LIMITS PER REF SRM 53-00-53-1A-1;[02] VERIFIED STEP 1SDR SWAA2023092593432Rib · crackedRIGHT HORIZONTAL STAB RIB #5 HAS A CRACK ON THE UPPER FWD I/B CORNER<[01] WORK WAS ACCOMPLISHED ON TASK CARD: (TTG8Q00N56VJ);[02] VERIFIED STEP 1SDR SWAA2023092193427Gusset · crackedFWD CARGO COMP GUSSET CRACKED AT STA 500D STA 19R<[01] REMOVED AND REPLACED FWD CARGO COMP GUSSET ANGLE AT STA 500D STR 19R PER SRM 51-40-02-0G-0 DWG# 143A7902.;[02] VERIFIED STEP 1SDR SWAA2023092192888Strip · corrodedAFT CARGO COMP CAP STRIP BETWEEN STA 767-847 LBL 21' CORRODED<[01] REMOVED CORROSION ON AFT CARGO COMPT CAP STRIP BETWEEN STA 767 TO STA 847 LBL 21 PER REF SRM 51-10-02-0G-0<BR>FOUND WITHIN LIMITS PER REF SRM 53-00-53-1A-1;[02] VERIFIED STEP 1SDR SWAA2023092192648Floor Panel · frayedMAIN CABIN FLOOR PANEL 221CF UPPER SURFACE FRAYING<[01] RECEIVED MAIN CABIN FLOOR PANEL AND WILL BE INSTALLED ON T/C TTG8Q00MKT4J;[02] CORRECTION: RECEIVED MAIN CABIN FLOOR PANEL 221CF AND WILL BE INSTALLED ON T/C TTG8Q00MKT4J;[03] VERIFIED; STEP # 2.SDR SWAA2023092192649Floor Panel · frayedMAIN CABIN FLOOR PANEL 222BF UPPER SURFACE FRAYING<[01] RECEIVED MAIN CABIN FLOOR PANEL 222BF AND WILL BE INSTALLED ON T/C TTG8Q00N0FKV;[02] VERIFIED STEP 1SDR SWAA2023092192650Floor Panel · frayedMAIN CABIN FLOOR PANEL 221AF UPPER SURFACE FRAYING<[01] RECEIVED MAIN CABIN FLOOR PANEL AND WILL BE INSTALLED ON T/C TTG8Q00MKT4N;[02] CORRECTION: RECEIVED MAIN CABIN FLOOR PANEL 221AF AND WILL BE INSTALLED ON T/C TTG8Q00MKT4N;[03] VERIFIED; STEP # 2.SDR SWAA2023092192651Floor Panel · frayedMAIN CABIN FLOOR PANEL 221DF UPPER SURFACE FRAYING<[01] RECEIVED MAIN CABIN FLOOR PANEL 221DF AND WILL BE INSTALLED ON T/C TTG8Q00MKT4G;[02] VERIFIED STEP 1SDR SWAA2023092192652Floor Panel · frayedMAIN CABIN FLOOR PANEL 242TF UPPER SURFACE FRAYING<[01] RECEIVED MAIN CABIN FLOOR PANEL AND WILL BE INSTALLED ON T/C TTG8Q00MKT3N;[02] CORRECTION: RECEIVED MAIN CABIN FLOOR PANEL 242TF AND WILL BE INSTALLED ON T/C TTG8Q00MKT3N;[03] VERIFIED; STEP # 2.SDR SWAA2023092192653Floor Panel · frayedMAIN CABIN FLOOR PANEL 242UF UPPER SURFACE FRAYING<[01] RECEIVED MAIN CABIN FLOOR PANEL 242UF AND WILL BE INSTALLED ON T/C TTG8Q00MKT3L;[02] VERIFIED STEP 1SDR SWAA2023092192654Floor Panel · frayedMAIN CABIN FLOOR PANEL 241XF UPPER SURFACE FRAYING<[01] RECEIVED MAIN CABIN FLOOR PANEL 241XF AND WILL BE INSTALLE ON T/C TTG8Q00MKSX0;[02] VERIFIED; STEP # 1.SDR SWAA2023092192655Floor Panel · frayedMAIN CABIN FLOOR PANEL 241ZF UPPER SURFACE FRAYING<[01] RECEIVED MAIN CABIN FLOOR 241ZF AND WILL BE INSTALLED ON T/C TTG8Q00MKSY3;[02] VERIFIED STEP 1SDR SWAA2023092192656Floor Panel · frayedMAIN CABIN FLOOR PANEL 241AAF UPPER SURFACE FRAYING<[01] RECEIVED MAIN CABIN FLOOR PANEL 241AAF AND WILL BE INSTALLED ON T/C TTG8Q00MKSY1;[02] VERIFIED; STEP # 1.SDR SWAA2023092192657Floor Panel · frayedMAIN CABIN FLOOR PANEL 241ABF UPPER SURFACE FRAYING<[01] RECEIVED MAIN CABIN FLOOR PANEL 241ABF AND WILL BE INSTALLED ON T/C TTG8Q00MKSXZ;[02] VERIFIED STEP 1SDR SWAA2023092192646Floor Panel · frayedMAIN CABIN FLOOR PANEL 241ACF UPPER SURFACE FRAYING<[01] RECEIVED MAIN CABIN FLOOR PANEL AND WILL BE INSTALLED ON T/C TTG8Q00MKSXX;[02] CORRECTION: RECEIVED MAIN CABIN FLOOR PANEL 241ACF AND WILL BE INSTALLED ON T/C TTG8Q00MKSXX;[03] VERIFIED; STEP # 2.SDR SWAA2023092192884Strip · corrodedAFT CARGO COMP CAP STRIP BETWEEN STA 727-727D RBL 21' CORRODED<[01] REMOVED CORROSION ON AFT CARGO COMPT CAP STRIP BETWEEN STA 727 TO STA 727D RBL 21 PER REF SRM 51-10-02-0G-0<BR>FOUND WITHIN LIMITS PER REF SRM 53-00-53-1A-1;[02] VERIFIED STEP 1SDR SWAA2023092192885Strip · corrodedAFT CARGO COMP CAP STRIP BETWEEN STA 767-727D RBL 21' CORRODED<[01] REMOVED CORROSION ON AFT CARGO COMPT CAP STRIP BETWEEN STA 727D TO STA 767 RBL 21 PER REF SRM 51-10-02-0G-0<BR>FOUND WITHIN LIMITS PER REF SRM 53-00-53-1A-1;[02] VERIFIED STEP 1SDR SWAA2023092192886Strip · corrodedAFT CARGO COMP CAP STRIP BETWEEN STA 727-727D LBL 21' CORRODED<[01] REMOVED CORROSION ON AFT CARGO COMPT CAP STRIP BETWEEN STA 727 TO STA 727D LBL 21 PER REF SRM 51-10-02-0G-0<BR>FOUND WITHIN LIMITS PER REF SRM 53-00-53-1A-1;[02] VERIFIED STEP 1SDR SWAA2023092192887Strip · corrodedAFT CARGO COMP CAP STRIP BETWEEN STA 7767-727D LBL 21' CORRODED<[01] ENTER IN ERROR AND IS BEING CORRECTED BY RAISING A NEW FAULTSDR SWAA2023092192645Gusset · crackedFWD CARGO COMP GUSSET CRACKED AT STA 500D STA 19L<[01] REMOVED AND REPLACED FWD CARGO COMP GUSSET AT STA 500D AND STA 19L PER REF BOEING 737-700 SRM 51-40-02-0G-0 AND DRAWING # 143A9485.;[02] VERIFIED STEP 1SDR SWAA2023092192637Intercostal · crackedMAIN CABIN INTERCOSTAL CRACKED AT BL 0 BETWEEN STA 380-400<[01] REMOVED AND REPLACED UPPER ANGLE AT MAIN CABIN INTERCOSTAL AT BL 0 BETWEEN STA380 TO 400 AND TREATED & PRIMER ALL FASTENERS HOLES AS PER B 737-700 SRM 51-40-02-0G-0 AND DWG # 143A5400; 51-20-01-0GSDR SWAA2023092192638Intercostal · crackedMAIN CABIN INTERCOSTAL CRACKED AT LBL 13' BETWEEN STA 380-400<[01] REMOVED AND REPLACED ANGLE AT MAIN CABIN LBL 13''STA 380 TO 400 SRM 51-40-02-0G-0 AND DWG 43A5400;[02] VERIFIED STEP 1SDR SWAA2023092192640Intercostal · crackedMAIN CABIN INTERCOSTAL CRACKED AT RBL 41' BETWEEN STA 380-400<[01] REMOVED AND REPLACED ANGLE AT MAIN CABIN RBL 41'' STA 380TO 400 DWG 43A5400 AN SRM 51-40-02-0G-0;[02] VERIFIED STEP 1SDR SWAA2023092192641Intercostal · crackedMAIN CABIN INTERCOSTAL CRACKED AT RBL 10' BETWEEN STA 380-400<[01] REMOVED AND REPLACED NEW UPPER ANGLE AT MAIN CABIN INTERCOSTAL AT RBL 10' BETWEEN STA 380 TO 400 AND TREATED & PRIMER ALL FASTENERS HOLES AS PER B 737-700 SRM 51-40-02-0G-0 AND DWG # 143A5400;5SDR SWAA2023092192639Floor Panel · frayedMAIN CABIN FLOOR PANEL 222CF UPPER SURFACE FRAYING<[01] RECEIVED MAIN CABIN FLOOR PANEL 222CF AND WILL BE INSTALLED ON T/C TTG8Q00MKT48;[02] VERIFIED STEP 1SDR SWAA2023092192643Floor Panel · crackedMAIN CABIN FLOOR PANEL 221GF FWD O/B END CRACKED<[01] RECEIVED MAIN CABIN FLOOR PANEL 221GF AND WILL BE INSTALLED ON T/C TTG8Q00MKT4A;[02] VERIFIED STEP 1SDR SWAA2023092192137Rib · crackedDORSAL FIN RIB #1; (MOST FWD) HAS A CRACK ON ITS LEFT SIDE ON LOWER ANGLE.<[01] REMOVED AND REPLACED DORSAL FIN RIB #1; (MOST FWD) AS PER SRM 51-40-02-0G-0;[02] VERIFIED.SDR SWAA2023092191979Slide · draggingL2 DOOR SLIDE FLAP DRAGGING WHEN DOOR IS OPEN<[01] SECURED L-2 DOOR SLIDE FLAP AS PER MT 725-61-06;[02] VERIFIED STEP 1SDR SWAA2023092191839Scuff Plate · crackedR1 DOOR SCUFF PLATE HAS CRACK AT THE CORNER; SEE DOT # 0015<[01] RECEIVED & VERIFIED NEW SCUFF PLATE P/N: 141A8431-3; PO# 2028887; ISSUE TAG: PW192. INSTALLATION OF PLATE TRANSFER TO CARD: TTG8Q0023FZ5.;[02] VERIFIED STEP 1SDR SWAA2023092192135Intercostal · crackedMAIN CABIN INTERCOSTAL CRACKED LBL 45' BETWEEN STA 312-328<[01] REMOVED AND REPLACED NEW INTERCOSTAL AT MAIN CABIN AT STA 312 TO 328 AND LBL 45' AND TREATED & PRIMER ALL FASTENERS HOLES IN REF B 737-700 SRM 51-40-02-0G-0; 51-20-01-0G-0 AND DWG#141A5400; AMM 51SDR SWAA2023092192136Intercostal · crackedMAIN CABIN INTERCOSTAL CRACKED LBL 45' BETWEEN STA 344-328<[01] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN STA 344 TO 328 AND LBL 45 IN REF B737-700 SRM 51-40-02-0G-0 AND DWG # 141A5400 AND TREATED ALL FASTENERS HOLES WITH ALODINE & PRIMER IN REF SRM 51-20SDR SWAA2023092192128Intercostal · crackedMAIN CABIN INTERCOSTAL CRACKED LBL 11' BETWEEN STA 344-360<[01] REMOVED INTERCOSTAL;LOCATED AND DRILLED NEW INTERCOSTAL ;INSTALLED NEW INTERCOSTAL AT MAIN CABIN LBL 11' BETWEEN STA 344-360 AS PER SRM 51-40-05-0G-0 AND DWG 141A5400.;[02] VERIFIED STEP 1SDR SWAA2023092191973Floor Panel · corrodedFWD CABIN FLOOR PANEL 221CF HAS CORRODED INSERTS.<[01] NEW FLOOR FANEL INSTALLED ON FAULT TTG8Q00N0FKT;[02] CORRECTION TO STEP #1: NEW FLOOR PANEL INSTALLED ON FAULT TTG8Q00N0FKT.;[03] VERIFIED STEP 2SDR SWAA2023092192132Floor Panel · corrodedAFT CABIN FLOOR PANEL 241AAF HAS CORRODED INSERTS<[01] THIS PANEL WILL BE REPLACED ON WORK CARD TTG8Q00N0FM9;[02] INSP. VERIFIED THE TT# ENTERD WILL PERFORM WORK REQUIERMENT.SDR SWAA2023092192133Floor Panel · corrodedAFT CABIN FLOOR PANEL 241ABF HAS CORRODED INSERTS<[01] THIS PANEL WILL BE REPLACED ON WORK CARD TTG8Q00N0FMC;[02] INSP./ VERIFIED AS TT# ENTERD WILL PERFORM WORK REQUIERD.SDR SWAA2023092192127Floor Panel · corrodedAFT CABIN FLOOR PANEL 242UF HAS CORRODED INSERTS<[01] THIS PANEL WILL BE REPLACED ON WORK CARD TTG8Q00N0FLV;[02] INSPECTION VERIFIED TT# ENTERD WILL PERFORM WORK REQUIERMENT.
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