N967WN
Service difficulty reports · 184
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 = 'N967WN' 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 = 'N967WN' 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 SWAA2026083151036Engine · fireUPON POST FLIGHT WALK AROUND, 5 MINUTES AFTER SHUTDOWN, FLAMES WERE OBSERVED INSIDE ENG#2 EXHAUST NOZZLE. EVENTUALLY, FLAMES WENT OUT BY THEMSELVES._ 02 - INSPECTED PER [AMM 71-00-00-800-803-F00-NG (INSPECTION AFTER AN ENGINE FIRE USE OF FIRE EXTINGUISHING AGESDR SWAA2026030976137Access Panel · damagedACCESS PANEL 194BL HAS ELONGATED FASTENER HOLE. PREPPED AND PAINTED ACCESS PANEL 194BL REF M/M 51-21-99. PANEL READY FOR INSTALLATION. REF TTG8Q01ARDBG FOR PANEL 194BL INSTALLATION.SDR SWAA2025102024311Cover · detachedEXIT LIGHT COVER CAME OFF. REPLACED FO SIDE EXIT WINDOW EXIT SIGN LIGHT COVER PER AMM 33-51-01.SDR SWAA2025101423667Slide · partial deployFWD ENTRY DOOR SLIDE PARTIALLY DEPLOYED. REINSTALLED FWD ENTRY DOOR SLIDE IAW MT 725-61-06. AC OK FOR SERVICE.SDR SWAA2025100319840Light · inoperativeAFT LAV EMERGENCY EXIT LIGHT HAS INOP SEGMENTS. RELAMPED INOP SEGMENTS ON AFT LAV EMERGENCY EXIT LIGHT AND PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51-01-960-801.SDR SWAA2025100319839Lamp · inoperativeL/H OVER WING EXIT EMERGENCY LIGHTS HAVE INOP SEGMENTS. REPLACED THE LAMPS IN THE SEGMENTS ON L/H OWE EMERGENCY EXIT LIGHT AND PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51-01-960-801.SDR SWAA2025100319843Light · inoperativeR/H OVER WING EXIT EMERGENCY LIGHT HAS INOP SEGMENTS. RELAMPED INOP SEGMENTS ON R/H OWE EMERGENCY EXIT LIGHTS AND PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51-01-960-801.SDR SWAA2025100318855Battery Pack · no testEMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1675 FAIL TEST. REMOVED AND REPLACED POWER SUPPLY - BATTERY PACK M1675 AND PERFORMED GOOD OPERATIONAL TEST PER AMM 33-51-06-960-805. CLOSE CARD.SDR SWAA2025100216902Latch · damagedFSD SLIDE COVER ASSY CLOSE-OUT LATCH (BLOCK ASSY) DAMAGED WILL NOT RE-ENGAGE. REMOVED AND REPLACED WITH NEW FSD SLIDE COVER ASSY CLOSE-OUT LATCH (BLOCK ASSY) IAW AIPC 25-66-00-14 AND SOPM 20-50-01.SDR SWAA2025100615793Stringer Clip · no discrepancyFUSELAGE STATION PSX STRINGER CLIP STA 727D; S-7R HAS CRACKED. UPON FURTHER INVESTIGATION FOUND FUSELAGE STATION PSX STRINGER CLIP NOT CRACKED, NDI VERIFIED.SDR SWAA2025100215791Stringer Clip · crackedFUSELAGE STATION PSX STRINGER CLIP STA 727D; S-6L HAS CRACKED. REMOVED AND REPLACED STRINGER CLIP STA 727D; S-6L PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 AND DWG 146A1111 REV: -.SDR SWAA2025100215790Stringer Clip · crackedFUSELAGE STATION PSX STRINGER CLIP STA 706; S-4L HAS CRACKED. FABRICATED; REMOVED AND REPLACED STRINGER CLIP STA 706; S-4L PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG 144A1125 REV: A; DWG 144A1107 REV -.SDR SWAA2025100215792Stringer Clip · crackedFUSELAGE STATION PSX STRINGER CLIP STA 747; S-5L HAS CRACKED.<[01] REMOVED AND REPLACED STRINGER CLIP STA 747; S-5L PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 AND DWG 146A1131 REV:-.;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2025100215786Stringer Clip · crackedSTRINGER CLIP STA 727E, S-6L HAS CRACKED. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-05-0G-0, SRM 51-40-02-0G-0, AND DWG 146A1112, REV -.SDR SWAA2025100215785Stringer Clip · crackedSTRINGER CLIP STA 727C; S-6L HAS CRACKED. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-05-0G-0, SRM 51-40-02-0G-0, AND DWG 146A1103, REV -.SDR SWAA2025100215787Stringer Clip · crackedFUSELAGE STATION PSX STRINGER CLIP STA 767; S-5L CRACKED. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0, AND DWG 146A1132, REV -.SDR SWAA2025100215788Stringer Clip · crackedFUSELAGE STATION PSX STRINGER CLIP STA 727E, S-6R CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-0G-0, SRM 51-40-05-0G-0, AND DWG 146A1112, REV -.SDR SWAA2025100614961Seat Track · corrodedCORROSION ON TOP AND IN WELL OF PAX CABIN SEAT TRACK AT BS 687 LBL 45 WL 208. REMOVED PASSENGER CABIN SEAT TRACK AT BS 540-727B LBL 45 WL 208. INSTALLED NEW SERVICEABLE SEAT TRACK AT BS 540-727B LBL 45 WL 208 PER BOEING DWG 144A5300 REV E AND SRM 51-40-02-SDR SWAA2025100214965Floorboard · delaminatedPASSENGER CABIN FLOORBOARD 241RF TOP SURFACE DELAMINATED.. REMOVED PASSENGER CABIN FLOORBOARD 241RF IAW AMM 53-21-00-000-801;IDENTIFIED FLOOR PANEL 241RF MATERIAL IAW SRM 53-00-50-0I-1, FIG 5, TABLE 5. FOUND DELAMINATION DAMAGE TO BE OUT OF ALLOWABLE DAMAGESDR SWAA2025100314368Bulkhead Web · crackedRH VAPOR BARRIER BULKHEAD WEB HAS CRACKED AT BS 663 RBL 26 WL 161 - 176. FAULT WILL BE RESOLVED ON ANOTHER FAULT; REFER TO TTG8Q0155JAJ.SDR SWAA2025100314370Attach Angle · crackedRH VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT BS 663 RBL 33 WL 176. INVESTIGATED FOR POSSIBLE CRACK AS PER SRM 51-10-02; UPON FURTHER INVESTIGATION AND ACCOMPLISHMENT OF NDI, NO CRACK WAS NOTED.SDR SWAA2025100314373Vapor Barrier · crackedR/H BS663 VAPOR BARRIER IS CRACKED RBL35 WL156. RIGHT BS663 VAPOR BARRIER WITH A CRACK AT RBL35 AND WL156 WAS REPAIRED IAW SRM 51-70-04-2R-10.SDR SWAA2025090811838Handle · looseL1 DOOR; UPPER ASSIST HANDLE LOOSE. SECURED L1 DOOR UPPER ASSIST HANDLE. REF AMM 52-11-41.SDR SWAA2025081198812Megaphone · damagedAFT. MEGAPHONE HANDLE IS DAMAGED.<[01] R/R THE AFT. MEGAPHONE; OP?S CHECKS IAW AMM 25-64-00.SDR SWAA2025060275765Vapor Barrier · crackedRIGHT WHEEL WELL FIBERGLASS VAPOR BARRIER HAS APPROXIMATELY 17' CRACK BETWEEN RBL 28 AND RBL 36 <[01]. C/W EA ON ATTACHED FAULT; [02] C/W EA 25-157-01402 ON ATTACHED FAULT.SDR SWAA2025021997631Battery Pack · inoperativeFWD CABIN LT SIDE EMERGENCY LIGHTS INOP<[01] 01 - REMOVED AND REPLACED L/H FWD PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]SDR SWAA2024102953971Bracket · brokenFWD SERVICE DOOR REAR GIRT BAR BRACKET BKN<[01] FOUND ONE RIVET ON AFT GIRT BAR BRAKET MISSING. INSTALLED NEW RIVET REF SRM 51-40-02.SDR SWAA2024031261693Valve · fluctuatesNUMBER 2 ENGINE FLUCTUATING INFLIGHT 50-65 % N1 WHILE IN SHALLOW DESCENT ;PULLED THRUST TO IDLE AND RECEIVED ENG FAIL INDICATION ON NUMBER 2 ENGINE ; THRUST LEVER CAME BACK UP AND ENGINE RETURNED TO NORMAL OPERATION FOR REMINDER OF FLIGHT<[01] REPLACED #THE 2 SDR SWAA2023100204692Battery Pack · inoperativeL/H EMERGENCY OVERWING EXIT SIGN AND DOOR LINING LIGHTS INOP<[01] BY REPLACING THE BATTERY PACK AT LOCATION M1668 ON CUSTOMER CARD TTG8Q00NNRKS ALSO FIX L/H EMERGENCY OVERWING EXIT SING AND DOOR LINING LIGHTS PERFORMED OPERATIONAL TEST NORMAL AS PER REF B737 3SDR SWAA2023100204691Battery Pack · inoperativeL/H OVERHEAD BIN ROW 6ABC EMERGENCY LIGHT INOP<[01] REMOVED AND REPLACED BATTERY PACK AT POSITION M1668 P/N AD-D717-01-100WA S/N WN2756 PERFORMED OPERATIONAL TEST NORMAL AS PER REF B737 AMM 33-51-06-960-805.;[02] VERIFIED REMOVAL AND REPLACEMENT AND OP TEST.SDR SWAA2023092899974Floor Panel · deterioratedMAIN CABIN FWD WET AREA CENTER FLOOR PANEL 221CF HAS 2 PREVIOUS REPAIR<[01] PANEL ASSY FABRICATED; AS PER DRAWING 141A5810 -9 DATE SEP 14; 2023; AND SRM 50-00-50-2R-1 MATERIAL USED # 4417A400001CC-10 PO#1784073 AND PO. PART # SLP5182A3-1 PO.2036998;[02] VERIFISDR SWAA2023092899973Floor Panel · peelingMAIN CABIN FWD WET AREA CENTER FLOOR PANEL 221EF TOP SKIN PEELING OFF<[01] REPLACED MAIN CABIN FWD CENTER FLOOR PANEL # 221EF REF. B737-700 AMM 53-21-00-400-801. FLOOR PANEL 221EF WILL BE INSTALL ON FAULT TTG8Q00MLR0U;[02] VERIFIED REPLACEMENT AND TTG8Q00MLR0USDR SWAA2023092897826Floor Panel · crackedMAIN CABIN AFT WET AREA RT SIDE FLOOR PANEL 242XF CRACKED CENTER AREA<[01] REPLACED MAIN CABIN AFT WET AREA FLOOR PANEL 242XF REF. B737-700 AMM 53-21-00-400-801. FLOOR PANEL 242XF WILL BE INSTALL ON FAULT TTG8Q00MLQXY;[02] VERIFIED STEP 1.SDR SWAA2023092897391Stiffener · crackedRT VAPOR BARRIER ANGLE STIFFENER CRACKED I/B OF RT ECS EXHAUST. CORRECTING DESCRIPTION: RT VAPOR BARRIER ANGLE STIFFENER CRACKED O/B OF RT ECS EXHAUST. [TTG8Q00N9LAW]<[01] REMOVED AND REPLACED STIFFENER AT RT VAPOR BARRIER STA 663.75 RBL25 O/B OF ECS EXHAUST PSDR SWAA2023092896641Rib · crackedLEFT HORIZONTAL STABILIZER FRONT SPAR FAIRING 331B CRACKED @ INTERNAL RIB # 4<[01] REMOVED AND INSTALLED NEW LEFT HORIZONTAL STABILIZER FRONT SPAR FAIRING INTERNAL RIB # 4 PER REF SRM 51-40-02-0G-0. AND DWG# 186A1304;[02] VERIFIED REPLACEMENT OF LEFT HORIZONTASDR SWAA2023092896383Intercostal · crackedAFT CARGO COMPARTMENT INTERCOSTAL WEB AT STA 947.5 RBL 21 CRACK.<[01] REMOVED AND REPLACED AFT CARGO COMPARTMENT INTERCOSTAL WEB AT STA 947.5 RBL 21 REF B737 SRM 51-40-02-0G-0 AND DWG 147A7500SDR SWAA2023092896265Floor Panel · deterioratedMAIN CABIN FWD WET AREA FLOOR PANEL 222BF HAS 2EACH PREVIOUS REPAIR<[01] REPLACED MAIN CABIN FWD WET AREA RT SIDE FLOOR PANEL 222BF REF. B737-700 AMM 53-21-00-400-801. PANEL 222BF WILL BE INSTALL ON FAULT #TTG8Q00MLPLH;[02] VERIFIED STEP 1SDR SWAA2023092894695Cap · damagedLEFT HORIZONTAL STAB. TIP FWD CAP WITH ELONGATED HOLES (MKD)<[01] REPLACED LEFT HORIZONTAL STAB. TIP. AND WILL BE INSTALLED ON ITEM TTG8Q002QRY2;[02] VERIFIED STEP 1.SDR SWAA2023092894272Floor Panel · peelingMAIN CABIN FWD WET AREA L/H SIDE FLOOR PANEL 221DF TOP SKIN SOME AREAS PEELING OFF MATERIAL<[01] FABRICATED MAIN CABIN FLOOR FWD WET AREA FLOOR PANEL 221DF BY OUTSIDE VENDOR (AERO MARINE) WITH P.O. 2035363 PER BOEING DRAWING 141A5810-235. FLOOR PANEL 221DF WILSDR SWAA2023092894273Floor Panel · peelingMAIN CABIN FWD WET AREA L/H SIDE FLOOR PANEL 221BF TOP SKIN SOME AREAS PEELING OFF MATERIAL<[01] FABRICATED MAIN CABIN FWD WET AREA FLOOR PANEL 221BF BY OUTSIDE VENDOR (AERO MARINE) WITH RO. #2035371 REF. BOEING DRAWING 141A5810-729. PANEL 221BF WILL BE INSTALSDR SWAA2023092893979Floor Support · corrodedCORROSION FOUND AFT CARGO FLOOR SUPPORT AT STA 947.5 FROM LBL 6 TO RBL 20 WL 155.5 HAS MULTIPLE SPOTS OF CORROSION.<[01] REMOVED AND REPLACED AFT CARGO FLOOR SUPPORT AT STA 947.5 REF B737 SRM 51-40-02-0G-0 AND DWG #149A8117SDR SWAA2023092694278Floor Support · crackedFWD CABIN CENTER FLOOR SUPPORT INTERCOSTAL UPPER CAP CRACKED AT BL-0 BETWEEN STA 380 AND 400 WL 208.1 MKD DOT<[01] C/W INSTRUCTIONSSDR SWAA2023092694277Floor Support · corrodedCORROSION AND HEAVY SCRATCHES AT AFT OF AFT CARGO COMPARTMENT BULKHEAD LOWER FLOOR SUPPORT ANGLE FROM S-26L TO S-26R STA 947.75<[01] REF TASK CARD TTG8Q00N2QKZ FOR TASK COMPLETION;[02] VERIFIED STEP 1 DUPLICATED FAULT TTG8Q00N2QKZSDR SWAA2023092893962Attach Angle · crackedR/H VAPOR BARRIER UPPER ATTACH ANGLE STA 663.75 RBL 7.5 HOLE WITH CRACK INDICATION.<[01] REPAIRED R/H VAPOR BARRIER UPPER ATTACH ANGLE STA 663.75 RBL 7.5 PER B737-700 SRM 57-10-10-2R-5 FIG. 202 DEDTAIL B; SHEET 4.;[02] VERIFIED FINAL STEP 1.SDR SWAA2023092893772Floor Support · crackedMAIN CABIN CENTER WING BOX FLOOR SUPPORT BREAK CRACKED AT FASTER'S TAIL @ LBL- 1 STA 540 MKD DOT<[01] REMOVED AND REPLACED MAIN CABIN CENTER WING BOX FLOOR SUPPORT BREAK STA 540 LBL-1 PER B737-700 SRM 51-40-02-0G-0 AND DRAWING 143A0060;[02] CERTIFIED FLOOR SUPSDR SWAA2023092893761Floor Panel · peelingMAIN CABIN AFT WET AREA FLOOR PANEL 242TF TOP SKIN PEELING OFF SEVERAL AREAS<[01] FABRICATED MAIN CABIN AFT WET AREA FLOOR PANEL 242TF BY OUTSIDE VENDOR (AERO MARINE). REF. DWG 147A5810-94 WITH PO # 2035184. PANEL ASSY WILL BE INSTALLED ON FAULT # TTG8Q00MLQYESDR SWAA2023092893541Floor Support · corrodedCORROSION *** FWD CABIN WET AREA FLOOR SUPPORT INTERCOSTAL UPPER CAP CORRODED THRU @ LBL 11 BETWEEN STA 294.5 AND STA 312 MKD DOT<[01] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN FLOOR STRUCTURE BETWEEN STA 294.5 AND STA 312 LBL 11 PER B737-700 SRM 51-40-02SDR SWAA2023092693768Support · crackedFWD CABIN L/H SIDE WALL FUSELAGE SUPPORT FRAME FLANGE CUTOUT HAS SMALL CRACK AT STA 312 ABOVE L-1 DOOR UPPER SILL CUTOUT S-6L MKD DOT<[01] ACCOMPLISHED EA M-22-153-01244 (737-NG - SWA - BS 312 FRAME UPPER CHORD CRACK DAMAGE AT LBL 33 BETWEEN S-5L AND S-6L) [TTSDR SWAA2023092693545Intercostal · crackedFWD CABIN WET AREA INTERCOSTAL UPPER CAP CRACKED BETWEEN STA 294.5 & STA 303.9 BL-0 MKD DOT<[01] REMOVED AND REPLACED INTERCOSTAL AT FWD CABIN WET AREA BETWEEN STA 294.5 & STA 303.9 BL-0 PER B737-700 SRM 51-40-02-0G-0 & DRWN# 141A5400.;[02] VERIFIED INTERCOSTASDR SWAA2023092693766Intercostal · crackedFWD CABIN WET AREA INTERCOSTAL UPPER CAP CRACKED AFT END @ STA 312 & RBL 31 MKD DOT<[01] REMOVED AND REPLACED FWD CABIN WET AREA INTERCOSTAL LOCATED AT STA 312 AND RBL 31 IAW SRM 51-40-02-0G-0.;[02] CORRECTION OF STEP 1: REMOVED AND REPLACED CABIN WET AREA INT
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