N570WN
Service difficulty reports · 179
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 = 'N570WN' 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 = 'N570WN' 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 SWAA2022021471109None · crackedCRACK ON L/H LOWER T. CLIP / [01] REMOVED AND REPLACED L/H LOWER T-CLIP PER SRM 51-40-05<BR> AND SRM 51-47-02SDR SWAA2022021471111Panel · elongated193 D PANEL HAS ELONGATED AND PULLED HOLES IN PANEL / [01] INSTALLED NEW 193D PANEL. REF SRM 51-40-02.SDR SWAA2022021471112Panel · elongated194 E PANEL HAS ELONGATED AND PULLED HOLES IN PANEL / [01] REPLACED DAMAGED PANEL PER SRM 51-40-02;51-40-08 AND 51-40-05SDR SWAA2021092118125Slide · out of positionQA WALK L2 DOOR ESCAPE SLIDE SKIRT RUBS SCUFF PLATE WHEN CLOSING. / [01] REPOSITIONED L2 DOOR ESCAPE SLIDE SKIRT PER B737 AMM 25-66-01-400-803; [02] VERIFIEDSDR SWAA2021092118122Slide · out of positionQA WALK R2 DOOR ESCAPE SLIDE SKIRT RUBS SCUFF PLATE WHEN CLOSING. / [01] REPOSITIONED R2 DOOR ESCAPE SLIDE SKIRT PER B737 AMM 25-66-01-400-803; [02] VERIFIEDSDR SWAA2021092018126Pin · looseL2 DOOR ESCAPE SLIDE COVER HAS SAFETY PIN LOOSE. / [01] RE-SECURED L2 DOOR ESCAPE SLIDE SAFETY PIN AS PER B-737 AMM 25-66-01-400-803; [02] VERIFIEDSDR SWAA2021092112595Web · crackedRIGHT HORIZONTAL STABILIZER LEADING EDGE HAS #3 RIB CRACKED. ; / [01] REMOVED #3 RIB ASSEMBLY FROM R/H HORIZONTAL STAB LEADING EDGE AS PER B737-700 SRM 51-40-02-0G-0.; [02] VERIFIED #3 RIB REMOVAL.; [03] REMOVED WED #3 RIB AT R/H H/STAB L/E.IAW B733 SRM 51-40-SDR SWAA2021092121324Rib · crackedRIGHT HORIZONTAL STABILIZER LEADING EDGE HAS #3 RIB CRACKED. ; / [01] REMOVED #3 RIB ASSEMBLY FROM R/H HORIZONTAL STAB LEADING EDGE AS PER B737-700 SRM 51-40-02-0G-0.; [02] VERIFIED #3 RIB REMOVAL.; [03] REMOVED WED #3 RIB AT R/H H/STAB L/E.IAW B733 SRM 51-40-SDR SWAA2021092112597Rib · crackedRIGHT HORIZONTAL STABILIZER LEADING EDGE HAS #5 RIB CRACKED. ; / [01] REMOVED RIB #5 FOR RT HORIZONTAL STAB AS PER B737-7 SRM 51-40-02-0G-0 STEP 4.; [02] VERIFIED STEP 1.; [03] LOCATED AND DRILLED RIB AND ASSEMBLY AT #4RIB FROM R/H H/STAB L/E IAW B737 SRM51-40SDR SWAA2021092112598Doubler · broken#2 ENGINE I/B FAN COWL AFT IDG DOOR PLATE HAS CORNER BROKEN. ; / [01] REMOVED AND REPLACED ENGINE #2 I/B FAN COWL AFT IDG FINGER DOUBLE IN REFERENCE B-737 SRM 51-40-01-0G-0; [02] REMOVED AND REPLACED ENGINE # 2 I/B COWL AFT IDG DOOR DOUBLER IN REFERENCE B-373 SDR SWAA2021092112596Web · crackedRIGHT HORIZONTAL STABILIZER LEADING EDGE HAS #4 RIB CRACKED. ; / [01] REMOVED RIB #4 FOR RT HORIZONTAL STAB AS PER B737-7 SRM 51-40-02-0G-0 STEP 4.; [02] LOCATED AND DRILLED NEW RIB FOR TRANSFERRING OF EXISTING WEB AS PER B737-7 SRM 51-40-05-0G-0. FIG 3 TABLE SDR SWAA2021092109299Floor Panel · crackedAFT WET AREA FLOOR PANEL 242TF ASSY CRACKED R/H FWD EDGE. ; / [01] DRILLED HOLE .125 DIAMETER AND CLEANED REPAIR AREA TO INJECT BMS 8 -121; TYPE IV. REF B737-700 SRM 53-00-50-2R-8 PARAGRAPH 3 C;D.; [02] VERIFIED STEP 1; [03] APPLIED REPAIR AT AFT WET AREA FLOOSDR SWAA2021082308744Angle · corrodedFWD CARGO FLOOR SUPPORT Z ANGLES UPPER SURFACE SHOWS BARE METAL ; / [01] BARE METAL TREATED AND PRIMER APPLIED. B-737 <BR>REF: SRM 51-20-01-0G-0; AMM 51-21-72-370-804; [02] VERIFIED 1SDR SWAA2021092107654Angle · chafedVERTICAL STAB. FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLES HAVE CHAFED ; WEAR MARKS ; / [01] ORIGINAL MAT THICKNESS 0.063' MINIMUM MAT FOUND 0.032' NO ALLOWABLE MAT LIMITS FOUND; [02] REMOVED 98% OF L/H SKATE ANGLE AS PER B737-700 SRM 51-40-02-0G-0; [03] REMSDR SWAA2021092108335Floor Panel · delaminatedPANEL 242UF DELAMINATED ; / [01] MEASUREMENTS; [02] REMOVED DAMAGE DELAMINATED PLIES; PREPARED DAMAGE AREA FOR REPAIR; PERFORM DRY OUT NO WATER FOUND AS PER B737 SRM 53-00-50-2R-7; [03] VERIFIED 1 & 2<BR>OK TO INSTALL REPAIR; [04] REPAIRED AT FLOOR PANEL 242 USDR SWAA2021092108086Floor Panel · delaminatedPANEL 241ABF DELAMINATED ; / [01] REMOVED DAMAGE AND PREPARED FOR REPAIR AT FLOOR PANEL 241 ABF AS PER B737- SRM 53--00-50-2R-7; [02] VERIFIED DAMAGE REMOVAL.; [03] REPAIRED AT FLOOR PANEL 241 ABF AS PER B737 SRM 53-00-50-2R-7MATERIAL USED PO.1150387 AND PO. 1SDR SWAA2021092108085Floor Panel · delaminatedPANEL 241 ADF DELAMINATED ; / [01] MEASUREMENTS; [02] REMOVED DAMAGE PLIES ON TOP SURFACE OF FLOOR PANEL 241ADF PREPARED DAMAGE AREAS FOR REPAIR; PERFORMED DRY OUT. FOUND NO WATER AS PER B737 SRM 53-00-50-2R-7; [03] VERIFIED STEP 1 & 2. OK TO INSTALL REPAIR; [SDR SWAA2021092107741Floor Panel · delaminatedPANEL 241AEF DELAMINATED ; / [01] MEASUREMENTS; [02] REMOVED DAMAGED PLIES PREPARED AREA FOR REPAIR ;PERFORMED DRY OUT FOUND NO WATER ON FLOOR PANEL #241AEF AS PER B737 SRM 53-00-50-2R-7; [03] OK TO INSTALL REPAIR; [04] REPAIRED TOP SURFACE. DELAMINATION ON MASDR SWAA2021092107137Intercostal · crackedMAIN CABIN FWD WET AREA FLOOR STRUCTURE INTERCOSTAL CRACKED BETWEEN BS 328 AND BS 312 RBL-30. MKD 126/1. ; / [01] REMOVED FLOOR STRUCTURE INTERCOSTAL AT MAIN CABIN FWD WET AREA BETWEEN STA 312 - STA 328 RBL-30. REF: 51-40-02-0G-0.; [02] LOCATED AND DRILLED NEWSDR SWAA2021092107138Intercostal · crackedMAIN CABIN FWD WET AREA FLOOR STRUCTURE INTERCOSTAL CRACKED BETWEEN BS-312 AND BS 328 LBL-46 ; / [01] REMOVED FLOOR STRUCTURE INTERCOSTAL AT MAIN CABIN FWD WET AREA BETWEEN STA 312- STA 328 LBL 46. REF: 51-40-02-0G-0; [02] LOCATED AND DRILLED NEW INTERCOSTAL ASDR SWAA2021092107139Intercostal · crackedMAIN CABIN FWD WET AREA FLOOR STRUCTURE INTERCOSTAL CRACKED BETWEEN BS-344AND BS 328 LBL-46 ; / [01] REMOVED STRUCTURE INTERCOSTAL AT MAIN CABIN FWD WET AREA BETWEEN STA 328- STA 344 LBL 46. REF: SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED NEW INTERCOSTAL AS PSDR SWAA2021092107141Intercostal · crackedMAIN CABIN FWD WET AREA FLOOR STRUCTURE INTERCOSTAL CRACKED BETWEEN BS-344 AND BS 360 BL-0 MKD 126-4 ; / [01] REMOVED FLOOR STRUCTURE INTERCOSTAL AT MAIN CABIN FWD WET AREA BETWEEN STA 344 - STA 360 BL-0. REF: SRM 51-40-01-0G-0.; [02] LOCATED AND DRILLED NEW ISDR SWAA2021092107145Frame · crackedFWD CAB BS 311 FRAME CRACKED ABOVE L-1 DOOR FWD UPPER CUT-OUT ..MKD 126-6. ; / REMOVED DAMAGED AREA IN REFERENCE B-737 SRM 53-10-07-2R-1 PERFORMED HFEC ON REPAIR CUTOUT AT FWD CABIN BS 311 FRAME ABOVE L-1 DOOR FWD UPPER CUT-OUT IAW NDTM PART 6;51-00-00 PROCEDUSDR SWAA2021092107156Support Beam · corrodedCORROSION>>>>>>>CABIN FLOOR PANEL SUPPORT BEAM WITH WITH SURFACE CORROSION AROUND SCREW HOLES BS 986.5 RBL-24.5 TO RBL-45.5 ; / [01] REMOVED CORROSION ATAFT CABIN FLOOR SUPPORT BEAM AT BS 986.5 TORBL-45.5 AS PER B 737-7 SRM 51-10-02-0G-0; [02] (RII) VERIFIED CSDR SWAA2021092106267Gusset · crackedRH GUSSET CRACKER AT STA 500D; WL 200; STR 19R ; / [01] REMOVED RH GUSSET AT STA 500D WL 200 STR 19R. REF. BOEING 737-700 SRM 51-40-02-0G--; [02] VERIFIED 1; [03] LOCATED AND DRILLED NEW GUSSET AT STA 500D STGR 19R. REF. BOEING 737-700 SRM 51-40-05-0G-0; [04] SDR SWAA2021092106268Gusset · crackedLH GUSSET CRACKER AT STA 500D; WL 200; STR 19L ; / [01] REMOVED LH GUSSET AT STA 500D; WL 200; STR 19L. REF. BOEING 737-700 SRM 51-40-02-0G-O.; [02] LOCATED AND DRILLED NEW GUSSET AT STA 500D; WL 200; STR 19L. REF. BOEING 737-700 SRM 51-40-05-0G-0; [03] VERIFISDR SWAA2021092105823Scuff Plate · crackedAFT ENTRENCE CTR SCUFF PLATE HAS CRACK. ; / [01] RECEIVED REPAIRED AFT ENTRANCE CENTER SCUFF PLATE. IAW B 737-7 SRM 53-70-15-2R-1; [02] VERIFIED STEP 1SDR SWAA2021092105414Doubler · crackedFWD FUSELAGE EXTERNAL POWER SUPPLY COMPARTMENT CUTOT AFT EDGE DOUBLER CRACKED MKD DOT ; / COMPLETED INSTALLATION OF NEW EGPR DOUBLER PER B737-700 SRM 51-40-02-0G-0 AND DRAWING # 141A0640SDR SWAA2021092105170Floor Panel · delaminatedMID CABIN FLOOR PANEL # 241DF TOP SURFACE LAYERS DELAMINATED ; / [01] EVALUATED DAMAGED AREA AT FLOOR PANEL #241DF; FOUND DAMAGE MORE THAN 2 INCHES IN LENGTH . FLOOR PANEL OUT LIMITS REF B737-800 SRM 53-00-50-1A-1 PARAGRAPH 4 B(2).; [02] VERIFIED 1; [03] FABRISDR SWAA2021092105171Floor Panel · delaminatedMID CABIN CENTER AISLE FLOOR PANEL # 241AF TOP SURFACE LAYER DELAMINATED ; / [01] EVALUATED DAMAGED AREA AT FLOOR PANEL #241AF; FOUND DAMAGE MORE THAN 2 INCHES IN LENGTH. FLOOR PANEL OUT LIMITS REF B737-700 SRM 53-00-50-1A-1 PARAGRAPH 4 B (2).; [02] VERIFIED SSDR SWAA2021092105172Floor Panel · delaminatedMID CABIN FLOOR PANEL # 231XF TOP SURFACE LAYERS DELAMINATED ; / [01] EVALUATED DAMAGED AREA AT FLOOR PANEL #231XF; FOUND DAMAGE MORE THAN 2 INCHES IN LENGTH. FLOOR PANEL OUT LIMITS REF B737-700 SRM 53-00-50-1A-1 PARAGRAPH 4 B (2).; [02] VERIFIED 1; [03] OK TOSDR SWAA2021092104628Bracket · crackedRT WING AT DEFLECTOR CONTROL RIB THERE IS A CRACKED SEAL RETAINER BRACKET. LOWER SEAL. ; / [01] REMOVED SEAL RETAINER BRACKET AT RT WING DEFLECTOR CONTROL RIB AS PER B737-700 SRM 51-40-02-0G-0; [02] LOCATED AND DRILLED NEW SEAL RETAINER BRACKET AS PER B737-700SDR SWAA2021092104608Bulkhead · crackedAFT CARGO FWD BULKHEAD LINER 142NWA CRACKED ; / [01] FABRICATED NEW AFT CARGO BULK HEAD LINER 142NWA IAW B 737-7 AMM 25-52-01-201-801; [02] CORRECTION FOR STEP #1 RECEIVED NEW B/H PANEL # 142NWA TO BE INSTALLED ON WORK CARD # TTG8Q005KPRU; [03] SUMMERY CORRECTSDR SWAA2020010740168Slide · unsecureL2 DOOR SLIDE OUT OF PACK. / SECURED PACK PER MT.SDR SWAA2019120939386Battery · inoperativeFLIGHT ATTENDANT REPORTS ONE AFT EMERGENCY FLASHLIGHT INOPERATIVE. / R&R BATTERY PER MM.SDR SWAA2019072935322Sign · unsecureFORWARD GALLEY EMERGENCY EXIT SIGN FELL OFF. REINSTALLED SIGN PER SIP.SDR SWAA2019061733715Connector · disconnectedEMERGENCY EXIT LIGHT AFT OF R/H OVERWING EMERGENCY DOOR NOT CONNECTED. CONNECTED LIGHT IAW AMM.SDR SWAA201906133629Light · inoperativeFORWARD RECESSED PANEL EMERGENCY LIGHT INOP. R&R LIGHT PER AMM.SDR SWAA2022031068036Strip · crackedAFT CARGO BAY LH AFT FLOOR PNL CAP STRIP IS CRACKED / REMOVED DAMAGED FLOOR PNL CAP STRIP; LOCATED AND DRILLED AND INSTALLED NEW CAP STRIP IAW DWG 453A2611 89282U 07JUN19SDR SWAA2019061133488Wire · pulledL/H SIDEWALL EMERGENCY EXIT LIGHT JUST FORWARD OF OVERWING EXIT DOOR HAD WIRE PULLED OUT OF QUICK DISCONNECT. / TERMINATED L01189 CONNECTOR D03672 WIRE PER WDM & AMM.SDR SWAA2022030868016Angle · crackedBS 663 RH VAPOR BARRIER VERTICAL ANGLE IS CRACKED AT RBL 25 W/L 148 / REMOVED & REPLACED VERTICAL ANGLE AT B.S 663 RBL 25 W.L 148 IAW SRM 51-40-02 DWG 111A1000 REV A 59594U 21MAY19SDR SWAA201906133650Angle · crackedFORWARD CARGO BAY INTERCOSTAL CLIP CRACKED AT BS. 500C, LBL 25. R&R CLIP PER SRM AND DWG.SDR SWAA201906133628Stiffener · crackedR/H HORIZONTAL STABILIZER RIB STIFFENER CRACKED IN THE LOWER RADIUS OF THE 1ST STIFFENER FROM FRONT STAB. STA. 120.30. / REPAIRED STIFFENER PER SRM.SDR SWAA2019061133487Fitting · crackedR/H HORIZONTAL STABILIZER RIB FORWARD FITTING CRACKED AT STA. 120.3. / R&R FITTING PER SRM & DWG.SDR SWAA2022030968007Floor Panel · pulledAFT FLOOR PANEL 241AAF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. / DUE TO EXTENT OF DAMAGE ON UPPER SKIN ON AFT FLOOR PANEL 241AF; BEGAN FABRICATED NEW PANEL USING BMS 5-107 LOT# AK8KD4895K IAW SRM 53-00-52-2R-0 PARA 1A (NOTE) AND DWG 147A5810-8. 59049USDR SWAA201906133649Seat Track · damagedTOP OF SEAT TRACK MECHANICAL DAMAGED BETWEEN BS. 480 TO BS. 520, LBL 45. R & R SEAT TRACK PER DWG & SRM.SDR SWAA201906133627Seat Track · damagedTOP OF SEAT TRACK MECHANICALLY DAMAGED BETWEEN BS. 480 TO BS. 520, LBL 25. R&R SEAT TRACK PER MM, DWG, AND SRM.SDR SWAA2022030967969Floor Support · crackedFLOOR PANEL SUPPORT IS CRACKED AT B.S. 540; B.L. 0-L .B.L 24.5; W.L. 208.1. / REMOVED AND INSTALLED A NEW FLOOR PANEL SUPPORT AT B.S 540 BL0- LBL 24.5 WL 208.1 IAW SRM 51-40-05; SRM 51-40-02; DWG 143A0060SDR SWAA2022030967970Floor Support · crackedFLOOR PANEL SUPPORT IS CRACKED AT B.S. 540; B.L. 0-R .B.L 24.5; W.L. 208.1. / REMOVED AND INSTALLED A NEW FLOOR PANEL SUPPORT AT B.S 540 BL0- RBL 24.5 IAW SRM 51-40-05; SRM 51-40-02 ; DWG 143A0060SDR SWAA2022030967973Support Angle · crackedCRACK IN BULKHEAD SUPPORT ANGLE BRACKET STA 847+18 LBL 10 WL 165 (MARKED) / REMOVED DAMAGED BULKHEAD SUPPORT ANGLE BRACKET STA .847+18 WL165; AND INSTALLED NEW BRACKET PER SRM 51-40-02; DWG 149A8102 SH15 AND DWG 149A8104 SH 1.
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