N213WN
Service difficulty reports · 288
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 = 'N213WN' 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 = 'N213WN' 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 SWAA2023013195981Light · 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 SWAA2023013195982Lens · missingR2 DOOR CUTOUT EXIT LIGHT LENS MISSING.<[01] FOUND AND INSTALLED EXIT LIGHT LENS AT R2 DOOR CUTOUT IAW B737-700 AMM 33-51-01-960-802.;[02] VERIFIED STEP 1.SDR SWAA2023013195978Slide · out of adjustL2 DOOR SLIDE SKIRT RUBS AGAINST SCUFF PLATE WHEN OPEN/CLOSE DOOR.<[01] REPOSITIONED L2 DOOR ESCAPE SLIDE PACK AND COVER IN REFERENCE AMM 25-66-01-400-803; CHECKED NORMAL.;[02] VERIFIED STEP 1.SDR SWAA2023013195644Battery · inoperativeFOUND EMERGENCY BATTERY POWER SUPPLY AT POSITION M1668 INOPERATIVE.<[01] REMOVED AND REPLACED EMERGENCY BATTERY POWER SUPPLY AT POSITION M1668 AS PER REF. B737 AMM 33-51-06-960-806. TEST OK;[02] VERIFIED STEP 1.SDR SWAA2023020193166Bracket · brokenAFT CARGO FWD BULKHEAD LOWER CENTER BRACKET BROKEN.<[01] REMOVED AND REPLACED AFT CARGO FWD BULKHEAD LOWER CENTER BRACKET AS PER SRM 51-40-02-0G-0;[02] VERIFIED STEP 1.SDR SWAA2023022306219Panel · peelingRIGHT SIDE OF FUSELAGE CENTER WING TO BODY FAIRING #193AR INNER SKIN FIBERGLASS PEELING OFF AT LOWER I/B EDGE<[01] CLEANED AND PREPARED AREA FOR REPAIR AT FUSELAGE CENTER WING TO BODY FAIRING 193AR AS PER BOEING 737 SRM 51-70-04-2R-6;[02] OK TO REPAIR DAMAGE ASDR SWAA2023022306218Panel · peelingLEFT SIDE OF FUSELAGE CENTER WING TO BODY FAIRING #193AL INNER SKIN FIBERGLASS PEELING OFF AT LOWER I/B EDGE<[01] PREPARED PANEL #193AL AT DAMAGED AREA FOR REPAIR PER B737 SRM 51-70-04-2R-6 AND SRM 51-70-04-2R-0;[02] VERIFIED STEP 1. OK TO APPLY REPAIR.;[03] RSDR SWAA2023013192318Floor Panel · peelingMAIN CABIN AFT WET AREA CENTER FLOOR PANEL #241AAF TOP SKIN LARGE AREA FIBERGLASS PEELING OFF<[01] REPLACED MAIN CABIN AFT WET AREA CENTER FLOOR PANEL #241AAF PER B737-700 AMM 53-21-00-400-801.;[02] PANEL #241AAF WILL BE INSTALLED ON FAULT #TTG8Q00FYE7E.;[03] SDR SWAA2023013191118Intercostal · corrodedMAIN CABIN FLOOR STRUCTURE INTERCOSTAL BETWEEN STA 294.5 AND STA 312 LBL 11.10 HAS CORROSION ON UPPER FLANGE.<[01] INSTALLED EWIS PROTECTION AS REQUIRED PER B737-700 AMM 20-60-07-913-801.;[02] EVALUATED CORRODED AREA AND FOUND OUT OF LIMITS PER B737-700 SRM 53SDR SWAA2023013191119Intercostal · corrodedMAIN CABIN FLOOR STRUCTURE PANEL BREAK BETWEEN STA 328 AND STA 344 LBL 11.10 HAS CORROSION ON UPPER FLANGE.<[01] INSTALLED EWIS PROTECCION AT FWD WET AREA;BET. STA 328 TO STA 344;LBL 11.PER B 737-700 AMM 20-60-07-913-901.;[02] REMOVED CORROSION AT PANEL BREAK;SDR SWAA2023013188516Floor Panel · crackedMAIN CABIN FWD WET AREA CENTER FLOOR PANEL #231AF WITH CRACK APROX. 6'<[01] FABRICATED MAIN CABIN FLOOR PANEL #231AF BY OUTSIDE VENDOR (AERO MARINE) WITH P.O #2002029.PANEL ASSY WILL BE INSTALLED ON FAULT #TTG8Q00FYEGE;[02] VERIFIED STEP #1 AND TTG8Q00FYEGESDR SWAA2023013188032Sign · missingEXIT SIGN COVER IS MISSING AT R/H SIDEWALL PANEL # 9.<[01] INSTALLED EXIT SIGN COVER AT R/H SIDEWALL PANEL # 9 IAW AMM 33-51-01-960-802.;[02] VERIFIED STEP #1.SDR SWAA2023013188034Floor Panel · damagedMAIN CABIN FWD WET AREA FLOOR PANEL #221BF HAS A PREVIOUS REPAIR ON TOP SKIN<[01] FABRICATED MAIN CABIN FLOOR PANEL #221BF BY OUTSIDE VENDOR (AERO MARINE) WITH P.O #2002002.PANEL ASSY WILL BE INSTALLED ON FAULT #TTG8Q00FYEHJ;[02] VERIFIED STEP #1 AND TTG8Q00FYSDR SWAA2023013188035Floor Panel · damagedMAIN CABIN FWD WET AREA FLOOR PANEL #221DF HAS A PREVIOUS REPAIR ON TOP SKIN<[01] FABRICATED MAIN CABIN FLOOR PANEL #221DF BY OUTSIDE VENDOR (AERO MARINE) WITH P.O #2002013.PANEL ASSY WILL BE INSTALLED ON FAULT #TTG8Q00FYEH5;[02] VERIFIED STEP #1.<BR>OK TO INSSDR SWAA2023020187508Bracket · crackedLEFT WING LOWER I/B T/E FIXED PANEL #551FB HAS 1 EACH BRACKET AT INNER AFT SEAL RETAINER ATTCH. CRACKED (MKD)<[01] REMOVED AND REPLACED BRACKET (1EACH) AT INNER AFT SEAL RETAINER;LEFT WING LOWER I/B.T/E. PANEL#551FB;PER B 737-700 SRM 51-40-02-0G-0.;[02] VERIFISDR SWAA2023013187126Beam · corrodedITEM CORROSION. AT AFT WET AREA FLOOR SUPPORT BEAM UPPER CAP FASTENER HOLE LBL 45. CORRECTION ITEM. CORROSION. AT AFT WET AREA FLOOR SUPPORT BEAM UPPER CAP FASTENER HOLE STA 986.5 LBL 45.<[01] FASTENER REMOVED AND CORROSION REMOVED ON FLOOR SUPPORT BEAM UPPER SDR SWAA2023013187523Floor Panel · delaminatedAFT CABIN FLOOR PANEL 241UF TOP LAYERS DELAMINATED @ CENTER AISLE<[01] PREPARED FOR REPAIR FLOOR PANEL 241 UF; AS PER B737 SRM 53-00-50-2R-1;[02] REPAIRED FLOOR PANEL 241UF ON TOP SURFACE PER B737 SRM 53-00-50-2R-1<BR>MATERIAL USED FIBER GLASS PO#1473815 AND RSDR SWAA2023013187515Floor Panel · crackedAFT MAIN CABIN FLOOR PANEL UPPER SURFACE CRACKED AT CENTER AISLE STA 787 LBL24 MKD DOT<[01] REMOVED AFT MAIN CABIN FLOOR PANEL #241RF REF AMM 53-21-00-000-801 STEP 2-E;[02] VERIFIED REMOVAL OF FLOOR PANEL 241RF.;[03] FABRICATED MAIN CABIN FLOOR PANEL #241RF BYSDR SWAA2023013190707Seat Track · wornMAIN CABIN L/H I/B SEAT TRACK EDGES WEAR MARKS @ LBL 24.75 STA 520 MKD DOT<[01] REMOVED WEAR MARKS AT LH I/B SEAT TRACK STA 520 LBL 24.75 AS PER REFERENCE SRM 51-10-02-0G-0;[02] VERIFIED STEP 1;[03] EVALUATED REWORKED AREA. MAXIMUM CLEANUP DEPTH ON THE TOP OF SDR SWAA2023013187125Structure · corroded***CORROSION*** AFT WET AREA FLOOR; R2 DOOR INNER CHORD WITH CORROSION AT NUT PLATE AREA BETWEEN STA 967-986 AND ABOUT RBL-50<[01] EVALUATED AREA AT R2 DOOR INNER CHORD; FOUND EXFOLIATING CORROSION; PASS THROUGH. FOUND OUT OF LIMITS AS PER REFERENCE SRM 53-70-SDR SWAA2023020186624Bracket · crackedLOWER CENTER WING L/H A/C BAY STA 540 CROSS-OVER DUCT I/B SUPPORT BRACKET CRACKED MKD DOT<[01] REMOVED LOWER CENTER WING L/H A/C BAY CROSS OVER DUCT I/B SUPPORT BRACKET RED BOEING 737 ARM 51-40-02-0G-0;[02] VERIFIED STEP #1.;[03] OK TO INSTALL NEW SUPPORT BRACSDR SWAA2023013186607Floor Panel · brokenAFT WET AREA STA 1016 R/H CORNER SMALL FLOOR PANEL 242XF BROKEN MKD DOT<[01] REPLACED MAIN CABIN AFT WET AREA FLOOR PANEL #242XF. FLOOR PANEL 242XF WILL BE INSTALL ON FAULT #TTG8Q00FYEFP;[02] VERIFIED STEP 1.SDR SWAA2023013186620Intercostal · crackedFWD CABIN FLOOR WET AREA INTERCOSTAL UPPER CAP CRACKED @ BL-0 BETWEEN STA 380 AND 400 MKD DOT<[01] INSTALLED EWIS PROTECCION.ON FAULT # TTG8Q003DV3A.;[02] REMOVED ANGLE (UPPER CAP)AT FWD CABIN WET AREA.STA 380 TO STA 400;BL 0.PER B 737-700 SRM 51-40-02-0G-0.;[SDR SWAA2023013186605Beam · corrodedCORROSION. AT AFT WET AREA FLOOE SUPPORT BEAM UPPER CAP FASTENERS HOLES LBL-24 TO LBL45 STA 986.5 MKD DOTS<[01] REMOVED FASTENER (1EA) AT FLOOR BEAM STA 986.5 LBL 45 FOR ACCESS TO CORROSION REMOVAL PER REF SRM 51-40-02-0G-0.;[02] REMOVED CORROSION AT FLOOR BEASDR SWAA2023013186611Beam · corrodedCORROSION. AFT CABIN WET AREA FLOOR BEAM UPPER CAP AT STA 986.5 RBL 45 MKD DOT<[01] REMOVED FASTENER (1EA) AT FLOOR BEAM STA 986.5 RBL 45 FOR ACCESS TO CORROSION REMOVAL PER REF SRM 51-40-02-0G-0.;[02] REMOVED CORROSION AT FLOOR BEAM UPPER CAT STA 986.5 RBL 45SDR SWAA2023013186613Web · corrodedCORROSION AFT WET AREA GALLEY SUPPORT FLOOR WEB 3EA SPOTS RBL 45 STA 986.5 MKD DOT 100<[01] EVALUATED CORROSION AREA. NO DAMAGE PERMITTED AT WEB AREA AS PER REF SRM 53-70-51-1A-1.;[02] REMOVED AFT WET AREA GALLEY SUPPORT FLOOR WEB AS PER REFERENCE SRM 51-40-02SDR SWAA2023013186614Angle · corrodedCORROSION AT FWD CABIN WET AREA FLOOR SUPPORT ANGLE FASTENER HOLE @ RBL 11 STA 294.5 MKD DOT<[01] REMOVED CORROSION AT FWD CABIN WET AREA FLOOR SUPPORT ANGLE;AT FASTENER HOLE;RBL 11'' STA 294.5'' PER B 737-700 SRM 51-10-02-0G-0.;[02] VERIFIED STEP #1.;[03] PERSDR SWAA2023013186619Structure · corrodedCORROSION AT R-1 DOOR LOWER SILL INNER CHORD FROM STA 294.5 TO STA 340 MKD DOTS<[01] REMOVED CORROSION AT R1 DOOR LOWER SILL INNER CHORD;FROM STA 294.5 TO STA 340;PER B 737-700 SRM 51-10-02-0G-0;[02] VERIFIED STEP #1.;[03] PERFORMED UT THICKNESS INSP. ON REWORSDR SWAA2023013186312Structure · corrodedCORROSION AT R-2 DOOR ENTRY LOWER SILL INNER CHORD FROM STA 947.75 TO STA 992.8<[01] R2 DOOR INNER CHORD IS FOUND OUT OF LIMITS AND CONTINUE WORK ON CARD TTG8Q00H09ZV.;[02] VERIFIED STEP 1SDR SWAA2023013186081Panel · crackedAFT CARGO PANEL 142NW CRACKED<[01] REPLACED AFT CARGO ACCESS PANEL 142NW AND WILL BE INSTALLED IN THE ITEM TTG8Q00G430M PER AMM 25-52-18-400-801.;[02] VERIFIED STEP 1.SDR SWAA2023013186204Frame · crackedFWD CABIN FUS SUPPORT FRAME FLANGE CUTOUT CRACKED ABOVE L-1 DOOR CUTOUT @ STA 312<[01] PERFORMED HFEC INSP ON SUPPORT FRAME FLANGE CUTOUT CRACKED; IAW B 737 NDT PART 6 51-00-00 PROC 23. CRACK OF 0.250' LENGTH CONFIRMED. TOOL NORTEC 600. BC 166316. CALIB DUE 10SDR SWAA2023013186319Intercostal · crackedFWD WET AREA FLOOR SUPPORT INTERCOSTAL CRACKED @ UPPER CAP BL-0 BETWEEN STA 344 AND STA 360 MKD DOT<[01] INSTALLED EWIS.ON FAULT # TTG8Q003DV3A.;[02] REMOVED INTERCOASTAL AT FWD WET AREA STA 340 TO STA 360;BL 0.PER B 737-700 SRM 51-40-02-0G-0.;[03] VERIFIED STSDR SWAA2023013186320Structure · crackedFWD CABIN WET AREA INNER CHORD CRACKED @ LBL-50 STA 303.9 MKD DO 001<[01] PERFORMED HFEC INSP. ON SUSPECTED CRACK AT FWD CABIN WET AREA INNER CHORD LBL-50 STA 303.9 IAW B737 NDT PART 6; 51-00-00; PROCEDURE 23. CRACK CONFIRMED (CRACK LENGTH 1') <BR>TOOL: NORTECSDR SWAA2023013186317Structure · corrodedCORROSION @ L-1 DOOR LOWER SILL INNER CHORD FROM STA 312 TO STA 344 MKD DOT<[01] L-1 DOOR INNER CHORD FROM STA 277 THRU STA 370 WAS REPLACED ON FAULT #TTG8Q00GYPNH;[02] VRRIFIED STEP 1SDR SWAA2023013186314Rib · crackedR/H HORIZONTAL STABILIZER FRONT SPAR L/E REMOVEABLE FAIRING CRACKED AT RIB 1 MKD DOT<[01] REMOVED R/H HORIZONTAL STAB. FRONT SPAR L/E; RIB #1 AS PER SRM 51-40-02-0G-0;[02] VERIFIED STEP 1. OK TO INSTALL NEW RIB.;[03] INSTALLED R/H HORIZONTAL STAB. FRONT SPAR LSDR SWAA2023013186315Rib · crackedL/H HORIZONTAL STABILIZER FRONT SPAR L/E REMOVEABLE FAIRING CRACKED AT SUPPORT RIB 1 MKD DOT<[01] REMOVED L/H HORIZONTAL STABILIZER FRONT SPAR RIB #1 AS PER REFERENCE SRM 51-40-02-0G-0;[02] VERIFIED STEP 1. OK TO INSTALL NEW RIB.;[03] INSTALLED L/H HORIZONTAL SDR SWAA2023013186318Rib · crackedL/H HORIZONTAL STABILIZER FRONT SPAR REMOVEABLE FAIRING CRACKED AT SUPPORT RIB 4 MKD DOT<[01] REMOVED L/H HORIZONTAL STABILIZER FRONT SPAR RIB #4 AS PER REFERENCE SRM 51-40-02-0G-0;[02] INSTALLED L/H HORIZONTAL STABILIZER FRONT SPAR RIB #4 AS PER REFERENCE SRMSDR SWAA2023013186316Fairing · elongatedL/H HORIZONTAL STABILIZER FRONT SPAR L/E REMOVEABLE FAIRING INB EDGE CENTER FASTENER HOLE ELONGATED<[01] PREVIOUS EXTERNAL REPAIR FOUND AT LE STA 251 (CENTER OF THE DOUBLER REPAIR) WITH AN AREA OF 65.0' FROM O/B AND 202.0' FROM I/B; EDGE; REPAIR EXTENDS FROM USDR SWAA2023013186309Panel · elongatedAFT CENTER WHEEL WELL ACCESS PANEL # 193D HAS CRACKED/ELONGATED HOLES<[01] CLEANED THE REPAIR AREA; NO WATER NOTE AND FILLED THE DAMAGED HOLES WTIH LAMINATING RESIN AND CHOPPED FIBERS; AT ACCESS PANEL 193D REF B737 SRM 51-70-04-2R- 9 PARAGRAPH 4.;[02] VERIFIEDSDR SWAA2023013185696Skin · crackedCRACK FOUND ON RT HORIZ.STAB. LOWER SKIN STAB STA 193.90 I/B ROW ; 16' FROM FRONT SPAR. CRACK LENGTH : 1'. CRACK FOUND ON RT HORI.STAB. LOWER SKIN STAB STA 193.90 I/B ROW 16" FROM FRONT SPAR. CRACK LENGTH : 1".<[01] REMOVED RT HORIZ. STAB FRONT SPAR ACSDR SWAA2022102563671Light · inoperativeEXTERIOR EMERGENCY LIGHT BEHIND FWD ENTRY DOOR INOP / [01] REMOVED AND REPLACED EXTERIOR EMER LIGHT BEHIND FWD ENTRY DOOR PER AMM 33-51-04. OPS CHECKS GOOD AT THIS TIMESDR SWAA2022101859471Structure · crackedDOT A-24-100 LH I/B FIXED L/E WTB FAIRING SUPPORT STRUCTURE CRACKED AT FASTENER HOLE AT LOWER FWD EDGE OF PANEL 195AL. / [01] HFEC IAW B737 NDT PART 6; 51-00-00 PROC 23. CRACK VERIFIED MARKED IN BLACK. TOOL#31823; DUE 23DEC22;[02] REMOVED CRACKED FAIRING SUPPOSDR SWAA2022101757935Floor Panel · pulledDOT A-24-21 CENTER CABIN FLOOR PANEL 231ZF HAS PULLED COMPOSITE FIBER DAMAGE ON UPPER SURFACE. / [01] EVALUATED PANEL 231ZF AND FOUND DAMAGE TO UPPER SURFACE PULLED FIBERS. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR 1A. CLEAN AND PREP. IAW B737SDR SWAA2022101457939Floor Panel · pulledDOT A-24-24 CENTER CABIN FLOOR PANEL 241CF HAS PULLED COMPOSITE FIBER DAMAGE ON UPPER SURFACE. / [01] EVALUATED DAMAGE; UPPER SURFACE FOUND TO BE REPAIRABLE IAW B737 SRM 53-00-50-2R-1. TAP TEST GOOD NO DELAMINATION NOTED. <BR><BR>CLEANED AND PREPPED UPPER SURFSDR SWAA2022101457938Floor Panel · pulledDOT A-24-23 CENTER CABIN FLOOR PANEL 242BF HAS PULLED COMPOSITE FIBER DAMAGE ON UPPER SURFACE. / [01] EVALUATED AND FOUND MISSING FIBERS ON UPPER SURFACE AT EDGE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED ANSDR SWAA2022101457936Floor Panel · pulledDOT A-24-22 CENTER CABIN FLOOR PANEL 231XF HAS PULLED COMPOSITE FIBER DAMAGE ON UPPER SURFACE. / [01] EVALUATED AND FOUND MULTIPLE AREAS OF FIBER DAMAGE ON UPPER SURFACE AND IS REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1.<BR>CLEANED AND SDR SWAA2022101457934Floor Panel · pulledDOT A-24-20 CENTER CABIN FLOOR PANEL 241AF HAS PULLED COMPOSITE FIBER DAMAGE ON UPPER SURFACE. / [01] EVALUATED AND FOUND MISSING FIBERS ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PREPPESDR SWAA2022101757458Doubler · crackedEGPR SURROUND DOUBLER IS CRACKED ON AFT SIDE OF DOOR CUT OUT BS 219.8+15' BETWEEN S-21R & S-22R AT WL 180 / [01] REMOVED EXISTING -1 DOUBLER IAW SRM 51-40-02-0G-0;[02] TRIMMED OUT DAMAGED AREA ON EGPR SURROUND DOUBLER IAW SRM 53-10-15-2R-4 REPAIR 4;[03] ACCOMPSDR SWAA2022051004857Light · inoperativeEMERGENCY LIGHT INOP IN CABIN AT ROW 11 RIGHT / [01] R+R EMERGENCY AREA LIGHT LAMP PER AMM 33-51-03SDR SWAA2022010504591Access Panel · delaminatedSUPPLEMENTAL INFORMATION: INTERNAL DELAMINATION ON ACCESS PANEL 193AL ON LOWER FUSELAGE / REPAIRED ACCESS PANEL 193AL ON LOWER FUSELAGE IAW B737-700 SRM 51-70-05-2R-2
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