N207WN
Service difficulty reports · 380
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 = 'N207WN' 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 = 'N207WN' 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 SWAA2024111146264Retainer · corrodedRIGHT MAIN W/W CUTOUT AFT ALL BLADE SEAL RETAINERS MATING SURFACE CORRODED. REMOVED CORROSION AT RIGHT MAIN W/W CUTOUT AFT BLADE SEAL RETAINERS AS PER B-737 SRM 51-10-02-0G-0<BR>'EVALUATED REWORKED AREA OF CUTOUT AFT BLADE SEAL RETAINERS'<BR>ORIGINAL MATERIALSDR SWAA2024111145735Floor Support · crackedMAIN CABIN CENTER SECTION FLOOR SUPPORT BREAK CRACKED @ LBL 1 STA 540 MKD DOT<[01] REMOVED AND REPLACED SUPPORT BREAK AS PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0.;[02] VERIFIED STEP 1;[03] ADDING DWG USED 143A0060;[04] VERIFIED DWG ADDEDSDR SWAA2024111145732Floor Support · corrodedCORROSION SPOT ** MAIN CABIN CENTER SECTION FLOOR SUPPORT INNER CHORD UPPER SKIN FASTENER'S HEAD @ RBL 60 STA 695 MKD DOT<[01] REMOVED AND REPLACED CORRODED FASTENERS AT MAIN CABIN CENTER SECTION INNER CHORD ON RBL 60 STA 695 REF B737 SRM 51-40-02-0G-0 AND DWGSDR SWAA2024111148786Floor Panel · frayedMID CABIN FLR PNL 241EF UPPER SURFACE HAS FRAYED/LOOSENED FIBERS<[01] RECEIVED PANEL 241EF 144A5810-129 AS PER SRM 53-00-50-2R-0. REFER TO TASK CARD TTG8Q00VCCJJ FOR CLOSING.;[02] VERIFIED STEP 1SDR SWAA2024111145247Stringer · crackedFWD CABIN L/H FWD OF L-1 DOOR S-15L CRACKED BETWEEN STA 294.5 AND STA 303.9 MKD DOT<[01] QUALITY CONTROL (QC) PERFORMED A REVIEW OF THIS FAULT;[02] ACCOMPLISHED REMOVAL OF DAMAGED AT STR-15L BETWEEN STA 294.5 AND STA 303.9; FABRICATED AND INSTALLED REPAIR PARTSDR SWAA2024111145248Stringer · crackedFWD CABIN L/H FWD OF L-1 DOOR S-16L CRACKED BETWEEN STA 294.5 AND STA 303.9 MKD DOT<[01] ACCOMPLISHED REMOVAL OF DAMAGED AT STR-16L BETWEEN STA 294.5 AND STA 303.9; FABRICATED AND INSTALLED REPAIR PARTS (REPLACEMENT STRINGER SECTION; HAT SECTION SPLICE) IAW B-SDR SWAA2024111145245Seat Track · corrodedCORROSION** MAIN CABIN FLOOR SEAT TRACK L/H INB. @ LBL 24.75 STA 500+15' INC MKD DOT<[01] MAIN CABIN SEAT TRACK REPLACED ON TASK: TTG8Q00W8L6L.;[02] RII-VERIFIED REPLACEDSDR SWAA2024110848787Floor Panel · frayedMID CABIN FLR PNL 231XF UPPER SURFACE HAS FRAYED/LOOSENED FIBERS<[01] RECEIVED PANEL 231XF 144A5810-126 AS PER SRM 53-00-50-2R-0. REFER TO TASK CARD TTG8Q00VCCQS.;[02] RECEIVED PANEL 231XF 144A5810-126 AS PER SRM 53-00-50-2R-0. REFER TO TASK CARD TTG8Q00VCCQS SDR SWAA2024111145061Rib · crackedR/H HORIZONTAL STABILIZER FRONT SPAR L/E FAIRING 341B RIB # 3 CRACKED MKD DOT<[01] SUMMARY: REMOVED AND REPLACED RIB #3 P/N 186A1303-2 AT R/H HORIZONTAL STABILIZER L/E FAIRING 341B AS PER B-737 SRM 51-40-02-0G-0 AND DWG 186A1001;[02] VERIFIED COMPLETED JOBSDR SWAA2024111145065Rib · crackedR/H HORIZONTAL STABILIZER FRONT SPAR L/E FAIRING 341B RIB # 5 CRACKED MKD DOT<[01] SUMMARY :REMOVED AND REPLACED RIB #5 AT R/H HORIZONTAL .STAB L/E AS PER REF B/737 SRM 51-40-02-0G-0 AND DW #186A1001.;[02] VERIFIED STEP#1.SDR SWAA2024111145066Rib · crackedR/H HORIZONTAL STABILIZER FRONT SPAR L/E FAIRING 341B RIB # 9 CRACKED MKD DOT<[01] SUMMARY: REMOVED AND REPLACED RIB #9 P/N 186A1401-2 AT R/H HORIZONTAL STABILIZER L/E FAIRING 341B AS PER B-737 SRM-51-40-02-0G-0 AND DWG 186A1001;[02] VERIFIED THE JOB COMPLETEDSDR SWAA2024111145062Rib · crackedL/H HORIZONTAL STABILIZER FRONT SPAR L/E FAIRING 331B RIB # 3 CRACKED MKD DOT<[01] SUMMARY: REMOVED AND REPLACED RIB #3 P/N 186A1303-1 AT L/H HORIZONTAL STABILIZER L/E FAIRING 331B AS PER B-737 SRM 51-40-02-0G-0 AND DWG 186A1001;[02] VERIFIED STEP#1.SDR SWAA2024111145063Rib · crackedL/H HORIZONTAL STABILIZER FRONT SPAR L/E FAIRING 331B RIB # 4 CRACKED MKD DOT<[01] SUMMARY: REMOVED AND REPLACED RIB #4 AT L/H HORIZONTAL STABILIZER L/E FAIRING 331B AS PER B-737 SRM 51-40-02-0G-0 AND DWG 186A1001;[02] VERIFIED JOB COMPLETED.SDR SWAA2024111144376Angle · crackedFWD CARGO B/S 420 BETWEEN LEFT STRINGER 24 AND 25 INTER COSTAL CLIP IS CRACKED. ON FWD SIDE OF FRAME<[01] REMOVED AND REPLACED FWD CARGO INTERCOSTAL CLIP AT STA 420 STR 25 FWD SIDE OF FRAME PER SRM 51-40-02-0G-0 AND DWG#143A7500;[02] CORRECTION TO STEP 1 : REMSDR SWAA2024111144382Scuff Plate · crackedFWD CARGO DOOR CUTOUT LOWER SILL AFT SCUFF PLATE UPPER SKIN FWD AREA CRACKED MKD DOT<[01] RECIEVED NEW FWD CARGO DOOR CUTOUT LOWER SILL AFT SCUFF PLATE PN:143A8331-4.<BR>REF TASKCARD#TTG8Q005JAU7 FOR INSTALLATION.;[02] VERIFIED RECEIVEDSDR SWAA2024111144743Support Angle · crackedR/H FUS FWD BODY FAIRING SUPPORT ANGLE CRACKED AT FASTENER'S TAIL I/B KRUEGER FLAP # 3 MKD DOT<[01] REMOVED AND REPLACED R/H FUS FWD BODY FAIRING SUPPORT ANGLE IAW<BR>SRM 51-40-02-0G-0 AND DWG 116A3118;[02] VERIFIED STEP 1SDR SWAA2024111152316Panel · corrodedP15 REFUEL PANEL HAS MULTIPLE CORROSION SPOTS<[01] REMOVED AND REINSTALLED P15 REFUEL PANEL AS PER B737 AMM TASK 28-21-00-000-801 AND 28-21-00-400-801. REMOVED AND REINSTALLED INDICATORS FROM P15 REFUELING PANEL AS PER B737 AMM TASK 28-41-61-000-801 AND 28-41-SDR SWAA2024111144373Access Panel · damagedPANEL 661BB WITH ELONGATED ATTACHING HOLE ON IB SIDE.<[01] 1. ACCOMPLISHED PULSE-ECHO ULTRASONIC INSP. FOR DELAMINATION ON PANEL 661BB & ELONGATED HOLE'S; CRACKED AND BULGING HOLE'S WITH LOCATIONS IDENTIFIED. <BR><BR>2. ACCOMPLISHED 24 HOUR DRYOUT AT PANEL #66SDR SWAA2024091134931Battery Pack · no testEMERGENCY AISLE LIGHTS BULLNOSE OF OVERHEAD BAG BIN INOPERATIVE 17 CBA & 20 CBA<[01] REMOVED AND REPLACED CHARGER AND BATTERY PACK PER AMM 33-51-06 20 CBA LIGHT IS NOW OPERATING AND 17 REQUIRES LAMP HOUSING ASSEMBLY. NIS IN TPA;[02] OK TO CONTINUE PER MEL 33-1SDR SWAA2024050983914Megaphone · inoperativeFWD GALLEY MEGAPHONE INOP<[01] R&R FWD GALLEY MEGAPHONE AS PER AMM 25-64-00. OPS CHECK NORMALSDR SWAA2024012945035Skin · crackedLH O/B AFT FLAP HAS DISBONDED AREA AND CRACKS ON LOWER SURFACE<[01] REMOVED AND REPLACED LH OUTBOARD AFT FLAP IN REFERENCE WITH AMM 27-51-26.;[02] RII C/W; REMOVED AND REPLACED LH OUTBOARD AFT FLAP IN REFERENCE WITH AMM 27-51-26.;[03] REMOVED AND REPLACED LH OSDR SWAA2024012444279Skin · crackedLH O/B AFT FLAP HAS DISBONDED AREA AND CRACKS ON LOWER SURFACE. REFERENCE EA 24-157-00199 FOR PERMANENT REPAIR REQUIREMENTS.<[01] COMPLETED ON EA 24-157-00205.;[02] C/W INSP.;[03] C/W INSP.SDR SWAA2024012943883Skin · crackedLEFT O/B AFT FLAP HAS CRACKS ON LOWER SURFACE<[01] C/W EA 24-157-00199; REPAIR REQUIRED WITHIN 5 FLIGHT CYCLES. OK TO CONTINUE ON TLD PER EA 24-157-00199. AIRCRAFT OK FOR SERVICESDR SWAA2023100406149Panel · delaminated193B PANEL HAS A CAVITY IN THE PANEL LAYERS AROUND FASTENER HOLE #16 THAT APPEARS TO EXTEND MORE THAN HALF WAY THROUGH THE THICKNESS OF THE PANEL AND FASTENER HOLE #18 HAS DELAMINATION. 193B PANEL HAS A CAVITY IN THE PANEL LAYERS AROUND FASTENER HOLE #16 THAT SDR SWAA2023072781453Plate · crackedFOUND LOWER TRAILING EDGE PANEL WIGGLE PLATE CRACKED IN 3 PLACES. CRACKS LOCATED BELOW #12 GROUND SPOILER. 1ST CRACK IS LOCATED BELOW INBD EDGE OF #12 SPOILER. 1ST CRACK BEGINS AT RIVET HOLE & GOES TO FWD EDGE OF WIGGLE PLATE. CRACK IS .320 LONG. CRACK INCLUDESDR SWAA2023080181451Plate · looseFOUND TRAILING EDGE PANEL WIGGLE PLATE LOOSE AND HOLES ELONGATED. HOLES IN WING STRUCTURE ARE NOT ELONGATED. WIGGLE PLATE IS LOCATED 22 FROM INBD EDGE OF #12 GROUND SPOILER.<[01] REPAIRED PER EA 23-157-02318.SDR SWAA2023072781452Plate · crackedFOUND CRACK IN TRAILING EDGE PANEL WIGGLE PLATE WITH PLATE LOOSE AND HOLES ELONGATED. WING STRUCTURE HOLES ARE NOT ELONGATED. CRACK IS LOCATED 28 FROM INBD EDGE OF #12 SPOILER AND IS .320 IN LENGTH. CRACK GOES FROM RIVET HOLE TO FWD EDGE OF WIGGLE PLATE.<[01] SDR SWAA2023072581455Bracket · damagedSUPPORT BRACKET BROKEN BETWEEN WING STRUCTURE AND SUPPCHANNEL ON TRAILING EDGE OF LOWER TRAILING EDGE PANEL. LOCATED UNDERNEATH #12 SPOILER DIAGONAL SUPPORT ROD ATTACHES TO THIS SUPPORT BRACKET. REMOVED AND REPLACED SUPPORT BRACKET BELOW #12 GROUND SPOILER PESDR SWAA2023050131113Battery Pack · inoperativeRIGHT EMERGENCY EXIT ROW EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AT LOCATION M1669 PER AMM 33-51-06SDR SWAA2023040723520Girt Bar · looseFWD ENTRY DOOR AFT GIRT BAR HOLDER LOOSE<[01] ADJUSTED FWD ENTRY DOOR GIRT BAR HOLDER CLIPS PER SIP.SDR SWAA2023040723510Slide · looseFWD ENTRY DOOR SLIDE LOOSE NEEDS TO BE RE-SECURED<[01] ACCOMPLISHED SLIDE REPACK PER AMM 25-66-01SDR SWAA2023021501859Battery Pack · inoperativeAFT CABIN/ GALLEY AREA EMERGENCY LIGHTS ARE INOP<[01] INSTALLED BATTERY PACKS ON AFT CABIN/GALLEY AREA AND ACCOMPLISHED OPS CHECK I.A.W. AMM 33-5106-960-805. OPS CHECK GOOD.;[02] REPLACED BATTERY PACKS ON AFT CABIN/GALLEY AREA AND ACCOMPLISHED OPS CHECK I.A.W.SDR SWAA2023021599596Floor Panel · pulledDOT A-24-04 CENTER CABIN FLOOR PANEL 231ZF UPPER SKIN HAS PULLED COMPOSITE FIBERS.<[01] EVALUATED PANEL 231ZF AND FOUND AREA OF PULLED FIBERS ON UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR 1A. CLEAN AND PREP. IAW B737-700 SRM 53-0SDR SWAA2023021599594Floor Panel · pulledDOT A-24-02 CENTER CABIN FLOOR PANEL 231YF UPPER SKIN HAS PULLED COMPOSITE FIBERS.<[01] EVALUATED AND FOUND DAMAGE TO UPPER SURFACE TO BE REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1<BR>CLEANED AND PREPPED AREA FOR REPAIR IAW SRM 53-00-50SDR SWAA2023021599597Floor Panel · pulledDOT A-24-05 CENTER CABIN FLOOR PANEL 231XF UPPER SKIN HAS PULLED COMPOSITE FIBERS.<[01] EVALUATED AND FOUND MISSING PLIES ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PREPPED IAW SRM 53-00SDR SWAA2023021599598Floor Panel · pulledDOT A-24-06 CENTER CABIN FLOOR PANEL 241AF UPPER SKIN HAS PULLED COMPOSITE FIBERS.<[01] EVALUATED AND FOUND MISSING PLIES ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PREPPED IAW SRM 53-00SDR SWAA2023021599599Floor Panel · pulledDOT A-24-07 CENTER CABIN FLOOR PANEL 232SF UPPER SKIN HAS PULLED COMPOSITE FIBERS.<[01] EVALUATED PANEL 232SF AND FOUND AREA'S OF PULLED FIBERS ON UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR 1. CLEAN AND PREP FOR REPAIR. IAW B737-SDR SWAA2023021599600Floor Panel · pulledDOT A-24-08 CENTER CABIN FLOOR PANEL 242AF UPPER SKIN HAS PULLED COMPOSITE FIBERS.<[01] EVALUATED AND FOUND MISSING PLIES ON UPPER SURFACE THE LENGTH OF BOARD. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PSDR SWAA2023013196722Girt Bar · out of adjustFWD SERVICE DOOR GIRT BAR BRACKET IS LOOSE<[01] INSP. FWD SVC DOOR GIRT BAR BRACKET NO DEFECTS FOUND IAW AMM 52-05-03SDR SWAA2022111569801Lamp · inoperativeR2 DOOR EXTERIOR EMERGENCY LIGHT INOP. / [01] RELAMPED R2 DOOR EXTERIOR EMERGENCY LIGHT AS PER REF B737 AMM 33-51-04-960-801. TEST OK.;[02] VERIFIED STEP 1.SDR SWAA2022111569804Slide · out of positionR2 DOOR SLIDE SKIRT RUBBING ON SCUFF PLATE WHEN OPENING AND CLOSING DOOR. / [01] REPOSITIONED R-2 DOOR SLIDE SKIRT; OPENED AND CLOSED DOOR; NO DEFECT NOTED. REF:B-737 AMM 25-66-01-400-804.;[02] VERIFIED.SDR SWAA2022111569431Battery Pack · inoperativeSEVERAL PASSENGER CABIN EMERGENCY LIGHTS INOP. / [01] REMOVED AND REPLACED BATTERY PACKS AT LOCATION M1674 AND M1675 AS PER REF B737 AMM 33-51-06-610-802;[02] PERFORMED INSTALLATION TEST NORMAL AS PER REF B737 AMM 33-51-06-960-805;[03] CORRECTION FOR STEP 1 - SDR SWAA2022111568624Strip · corrodedCORROSION - FWD CARGO COMP. R/H SIDE CAPSTRIP BETW. STA 500A THRU 500D RBL26 / [01] REMOVED CORROSION AT FWD CARGO COMP. R/H SIDE CAPSTRIP BETW. STA 500A THRU STA 500D PER B737-700 SRM 51-10-02-0G-0;[02] AFTER REMOVED CORROSION AT FWD CARGO COMP. R/H SIDE CAPSSDR SWAA2022111665369Bulkhead Web · crackedBULKHEAD BS 663.75, LBL 25 I/B OF L/H A/C AIR EXIT EXHAUST DUCT DOULBER APPEAR CRACKED BELOW FASTENER HEAD. REMOVED BULKHEAD FWD VAPOR BARRIER DOUBLER IAW SRM 51-40-02-0G-0. PERFORMED HFEC INSP ON VAPOR BARRIER WEB IAW NDT PART 6, 51-00-00, PROCE 23. CRACKSDR SWAA2022111562408Channel · corrodedCORROSION FOUND FWD CARGO R/H 'Z' CHANNEL FROM STA 492.4 THRU STA 500 / [01] REMOVED CORROSION AT FWD CARGO COMP. R/H 'Z' CHANNEL (SHIELD) BETW. STA 492.4 THRU STA 500 PER B737-700 SRM 51-10-02-0G-0.;[02] PERFORMED UT THICKNESS INSP ON REWORKED AREA IAW B737 NSDR SWAA2022111661846Floor Panel · brokenCABIN FLOOR PANEL 221BF, AFT OTBD EDGE WAS BROKEN BS 280. MAIN CABIN FLOOR PANEL 221BF WILL BE REPLACED ON FAULT TTG8Q00FECMR.SDR SWAA2022111661270Channel · corrodedCORROSION FOUND FWD CARGO RT ZEE CHANNEL, BS 492.4-500 AROUND FASTENER HOLES. REMOVED C0RROSION IAW SRM 51-10-02-0G. ACCIMPLISHED ON TTG8Q00FLB9G.SDR SWAA2022111661272Channel · corrodedCORROSION FOUND FWD CARGO RT ZEE CHANNEL, BS 500A - 500D AROUND FASTENER HOLES. REMOVED CORROSION IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS ON REWORKED AREA IAW NDTM PART 4, 51-00-00, PROCEDURE 3. FOUND OUT LIMITS IAW SRM 53-00-53-1A-2. REMOVED THE CHANSDR SWAA2022111661273Channel · corrodedCORROSION FOUND FWD CARGO LT ZEE CHANNEL, BS 400 - 500D AROUND FASTENER HOLES. REMOVED CORROSION IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS ON REWORKED AREA IAW NDTM PART 4, 51-00-00, PROCEDURE 3. AFTER CORROSION REMOVAL ON CHANNEL, FOUND OUT LIMITS IAWSDR SWAA2022111661274Shield · corrodedCORROSION FOUND FWD CARGO DOOR CUT-OUT FWD SHIELD, SPOTS OF CORROSION AROUND FASTENER HOLES. REMOVED CORROSION IAW SRM 51-10-02-0G. PERFORMED UT THICKNESS ON REWORKED AREA IAW NDTM, PART 4, 51-00-00, PROCEDURE 3. MINIMUM FOUND: 0.019'. AFTER REMOVAL OF C
Back to N207WN