N219WN
Service difficulty reports · 301
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 = 'N219WN' 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 = 'N219WN' 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 SWAA2023031302105Angle · corrodedCORROSION ANGLE LOCATED BS500D BETWEEN LBL21 TO RBL21 AND WL156 AT FWD CARGO COMPARTMENT 2023-113046<[01] REPLACED ANGLE LOCATED BS500D BETWEEN LBL21 TO RBL21 AND WL156 AT FWD CARGO COMPARTMEN IAW B737-700 SRM 51-10-02 Ï¿½TEM 9. PERFORMED VISUAL INSPECTION ON SDR SWAA2023031302104Support · corrodedCORROSION SUPPORT ZEE LOCATED BS500A TO BS500D RBL21 AND WL156 AT FWD CARGO COMPARTMENT 2023-113045<[01] TOOL USED: ULTRASONIC EQUIPMENT; P/N: 45 MG; S/N: 130063701; DUE DATE: 16-JUN-23.;[02] REPLACED SUPPORT ZEE LOCATED BS500A TO BS500D RBL21 AND WL156 AT FWDSDR SWAA2023031302102Track · crackedCRACK CARGO TRACK LOCATED BS500 RBL13.84 AND WL156 AT FWD CARGO COMPARTMENT 2023-113043<[01] TOOL USED: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 220273012; DUE DATE: 17-DEC-23;[02] INSPECTION REJECT IN STEP 7<BR>SEE TTG8Q00J8N87;[03] PERFORMED PERMANENT RSDR SWAA2023031302100Web · crackedCRACK WEB TRAILING EDGE LOCATED BTW ORSS261 TO ORSS279 AT RT WING 2023-113028<[01] REPLACED WEB TRAILING EDGE LOCATED BTW ORSS261 TO ORSS271 AT RT WING I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 115A2512 SHEET 11 REV.- DUE TO NOT FOUND ALLOWASDR SWAA2023031301788Panel · crackedCRACK INTERNAL CAVITY PHENOLIC STRAP LOCATED AT LEVEL ORSS 273 TRAILING EDGE AT LT WING 2023-112987<[01] REPLACED OUTBOARD TRAILING EDGE CORRUGATE PLATE (ASSY) LOCATED AT ORSS 273 AT LT WING I.A.W. B737-700 SRM 51-10-02 AND SRM 51-40-02 AND DWG 115A2001 SHEET SDR SWAA2023031301790Plate · crackedCRACK OUTBOARD TRAILING EDGE CORRUGATED PLATE LOCATED AT ORSS 261 AT RT WING 2023-113010<[01] REPLACED OUTBOARD TRAILING EDGE CORRUGATE PLATE LOCATED AT ORSS 261 AT RT WING I.A.W. B737-700 SRM 51-10-02 AND SRM 51-40-02 AND DWG 115A2001 SHEET 32 REV.-. DUE TO NSDR SWAA2023031301787Plate · crackedCRACK INTERNAL CAVITY CORRUGATE PLATE LOCATED AT LEVEL IRSS 248 TRAILING EDGE AT LT WING 2023-112990<[01] REPLACED CORRUGATE PLATE LOCATED AT LEVEL IRSS 248 TRAILING EDGE AT LT WING AND FASTENERS IAW<BR>B737-700 SRM-51-40-02; SRM 51-10-02 AND DWG 115A2001 REV:SDR SWAA2023031301789Plate · crackedCRACK INTERNAL CAVITY CORRUGATE PLATE LOCATED ORSS261 TRAILING EDGE AT LT WING 2023-112989<[01] REPLACED CORRUGATE PLATE AND FASTENERS LOCATED ORSS261 TRAILING EDGE AT LT WING IAW B737-700 SRM 51-40-02.;[02] CORRECTED STEP 1.<BR>REPLACED CORRUGATE PLATE AND FASDR SWAA2023031301468Angle · crackedCRACK ANGLE LOCATED BS291.5 TO BS294.5 AT LEVEL STR17R AT FWD GALLEY AREA 2023-112929<[01] REPLACED ANGLE LOCATED BS291.5 TO BS294.5 AT LEVEL STR17R AT FWD GALLEY AREA I.A.W B737-700 SRM 51-40-02 AND DWG 141A8310- 33 REV B. <BR>SEE INDIVIDUAL SIGN OFF BELLOW;[SDR SWAA2023031301465Intercostal · crackedCRACK WEB LOCATED BS294.5 TO BS303.9 AT LEVEL STR16L AT PASSENGER CABIN 2023-112925<[01] REPLACED WEB INTERCOSTAL LOCATED BS294.5 TO BS303.9 AT LEVEL STR16L AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 141A8180 REV;C. SEE INDIVIDUASDR SWAA2023031301466Frame · crackedCRACK FRAME ON BS 312 BETWEEN STR5L TO STR6L FWD GALLEY AND LAV 2023-112926<[01] PERFORMED REPAIR ON FRAME BS 312 BETWEEN STR 5L TO STR 6L FWD GALLEY AND LAV I.A.W EA M-22-153-01244;[02] CERTIFIED STEP 1; COMPLETED <BR>ITEM RIISDR SWAA2023031301473Cover · crackedCRACK COVER LOCATED BS992.8 AT LEVEL STR10R AT PASSENGER CABIN 2023-112949<[01] REPLACED COVER LOCATED BS992.8 AT LEVEL STR10R AT PASSENGER CABIN I.A.W B737-700 AMM 52-71-11-400-801 STEP 3. F. (5).;[02] CERTIFIED WORK PERFORMED.SDR SWAA2023031301474Cover · crackedCRACK COVER LOCATED BS992.8 AT LEVEL STR10L AT PASSENGER CABIN 2023-112950<[01] REPLACED COVER LOCATED BS992.8 AT LEVEL STR10L AT PASSENGER CABIN I.A.W B737-700 AMM 52-71-11-400-801 STEP 3F ITEM (5);[02] REPLACED COVER LOCATED BS992.8 AT LEVEL STR10L AT PASSENSDR SWAA2023031301463Tie Clip · crackedCRACK TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN 2023-112927<[01] REPLACED TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN AND FASTENERS I.A.W B737-700 SRM 51-40-02 DWG:141A1110 SHEET:18 REV:- SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK COMPLETED; RSDR SWAA2023031300803Rib · crackedCRACK INSPAR RIB 120.30 AT 28 INCHES OF FRONT SPAR LT HORIZONTAL STAB 2023-112863<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138203; DUE DATE: 11-APR-23.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138203;SDR SWAA2023031300804Bracket · crackedCRACK SUPPORT BRACKET BS540 LT SIDE AT AIR CONDITIONING BAY 2023-112867<[01] REPLACED SUPPORT BRACKET BS540 LT SIDE AT AIR CONDITIONING BAY IAW B737-700 51-40-02;[02] REPLACED SUPPORT BRACKET BS540 LT SIDE AT AIR CONDITIONING BAY IAW B737-700 51-40-02SDR SWAA2023031300810Intercostal · crackedCRACK WEB - INTERCOSTAL LOCATED BETWEEN BS847 TO BS867; LBL20 CEILING AREA AFT CARGO COMPARTMENT 2023-112884<[01] REPLACED WEB - INTERCOSTAL LOCATED BETWEEN BS847 TO BS867; LBL20 CEILING AREA AFT CARGO COMPARTMENT IAW B737-700 SRM-51-40-02 AND DWG-149A8100 REVSDR SWAA2023031000819Scuff Plate · crackedCRACK ON AFT CORNER SCUFF PLATE OF FWD CARGO COMPARTMENT 2023-112901<[01] TOOL USED DIGITAL CALIPER P/N:2340A11;S/N:B17119057;DUE DATE:05-DEC-23.;[02] TOOL USED: BLACK LIGHT METER : P/N XDS- 1000 S/N 1998072 DUE DATE : 03-MAY-23.;[03] REPAIRED AFT CORNER SCUFFSDR SWAA2023031000820Scuff Plate · crackedCRACK ON FWD CORNER SCUFF PLATE OF AFT CARGO COMPARTMENT 2023-112904<[01] TOOL USED: BLACK LIGHT METER : P/N XDS- 1000 S/N 1998072 DUE DATE : 03-MAY-23.;[02] REPAIRED BY WELD CORNER SCUFF PLATE OF AFT CARGO COMPARTMENT I.A.W. BOEING 737-700 SRM 53-60-15-2R-1 RSDR SWAA2023031300401Beam · corrodedCORROSION FLOOR STRUCTURE BEAM LOC STA 986.5 BTW RBL 40 TO RBL 45 AND WL 208.1 AT AFT GALLEY AREA 2023-112824<[01] TOOL USED: CALIPER; PN: 500-752-20; SN: B20317422; DUE DATE: 29-AUG-23.;[02] RADIUS GAUGE; PN: 2204A3; SN: AE-408657; DUE DATE: 14-FEB-23.;[03] TSDR SWAA2023031300399Structure · crackedCRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOC. STA 312 TO STA 328 AND RBL 31 FWD GALLEY AND LAV 2023-112818<[01] REPLACED WEB INTERCOSTAL FLOOR STRUCTURE LOC. STA 312 TO STA 328 AND RBL 31 FWD GALLEY AND LAV I.A.W B737-700 SRM 51-40-02 AND DGW: 141A5400 REV: - SSDR SWAA2023031300398Intercostal · crackedCRACK WEB - INTERCOSTAL FLOOR STRUCTURE BTW STA 277 TO STA 294.5 AND BL 0 FWD GALLEY AND LAV 2023-112817<[01] REPLACED INTERCOSTAL WEB LOCATED ON FLOOR STRUCTURE BTW STA 277 TO STA 294.5 AND BL 0 FWD GALLEY AND LAV I.A.W. B737-700 SRM 51-40-02 AND DWG 141A5400SDR SWAA2023031000416Panel · elongatedELONGATED HOLE BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT 2023-112859<[01] FABRICATED BULKHEAD 141JW AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 AND DRAWIN 453A2510 SHEET 4 REV- A MATERIAL USED PN CONOLITE #A60SG4W; PO# 2022-003394;[02] FABRISDR SWAA2023031399935Panel · crackedCRACK INDICATION FOUND ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 RIB AND 16 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 0.700 INCH. APPROX. 2023-112752<[01] TOOL USED: CALIPER; PN: 500-752-20; SN: B20317422; DUE DATSDR SWAA2023031399447Angle · crackedCRACK TRAILING EDGE SUPPORT ANGLE INTERNAL CAVITY ORSS 271 AT RT WING 2023-112631<[01] REPLACED TRAILING EDGE SUPPORT ANGLE INTERNAL CAVITY ORSS271 AT RT WING I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 115A2930 SHEET 8 REV.- DUE TO NOT FOUND SDR SWAA2023031399444Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED INTERNAL CAVITY ORSS 275 AT LT WING 2023-112629<[01] REPLACED ANGLE TRAILING EDGE LOCATED INTERNAL CAVITY ORSS 275 AT LT WING I.A.W B737-700 SRM 51-10-02 Ï¿½TEM 9 AND DWG #115A6200 REV:-;[02] REPLACED ANGLE TRAILING EDGE LOCATSDR SWAA2023031399445Web · crackedCRACK WEB TRAILING EDGE LOCATED ORSS 271 AT RT WING 2023-112634<[01] REPLACED WEB AT TRAILING EDGE LOCATED ORSS271 AT RT WING I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 115A2930 SHEET 6 REV.-.<BR>SEE INDIVIDUAL SIGN-OFF BELOW;[02] COMPLETED SSDR SWAA2023031399446Angle · crackedCRACK TRAILING EDGE SUPPORT ANGLE INTERNAL CAVITY ORSS 271 AT LT WING 2023-112628<[01] REPLACED SUPPORT ANGLE LOCATED TRAILING EDGE INTERNAL CAVITY ORSS 271 AT LT WING IAW B737-700 SRM 51-40-02-0G-0 AND DWG 115A2930 SHEET 7 REV - . SEE INDIVIDUAL SIGN-OFF BELOSDR SWAA2023031399449Panel · debondedCUSTOMER REQUEST - DEBONDED IB MAIN FLAP WEDGE PANEL LOWER SURFACE AT LT WING 2023-112679<[01] TOOL USED; CALIPER PN: 500-197-30; SN: B20189526; DUE DATE: 20/DEC/23.;[02] TOOL USED: HOTBONDER P/N: HCS9200B-AV S/N: 18196021 DUE DATE: 24-JAN-24; PROSITECTOR 6000SDR SWAA2023031399450Flap · debondedCUSTOMER REQUEST - DEBONDED OB AFT FLAP LOWER SURFACE LOCATED INBOARD SIDE AT LT WING 2023-112680<[01] TOOL USED; CALIPER PN: 500-197-30; SN: B20189526; DUE DATE: 20/DEC/23.;[02] TOOL USED CALIPER PN: 500-464 S/N: B17030933 DUE DATE: 17/OCT/23;[03] TOOL USED: SDR SWAA2022111771683Lens · crackedOVERHEAD BIN EMERGENCY LIGHT COVER CRACKED AT 4ABC AND 11DEF. R & R THE LENS IAW AMM 33-51-03.SDR SWAA2022110965683Angle · crackedCRACK FOUND ON UPPER ATTACH ANGLE STA 663 (WL 167) AT LBL 40 / [01] STARTED REMOVING FASTENERS FROM UPPER ATTACH ANGLE STA 663 IAW SRM 51-40-02-0G-0;[02] DOCUMENTED STARTED INSTALL OF ATTACH ANGLE ENTERED AS CORRECTIVE ACTION 1;[03] ACTION 2 SHOULD STATE REMOVSDR SWAA2022110865905Panel · pulledDOT A24-65 MID CABIN FLOOR BOARD PANEL 242BF HAS PULLED COMPOSITE FIBERS ON UPPER SIDE OF PANEL. / [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. TAP TEST GOOD;[02] CLEANSDR SWAA2022110865685Panel · pulledDOT A24-52 MID CABIN FLOOR BOARD PANEL 241BF HAS PULLED COMPOSITE FIBERS ON UPPER SIDE OF PANEL. / [01] EVALUATED AND FOUND BOARD TO BE BER AND TO REPLACE BY FABRICATION PER SAMPLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL STEP 4 AND TABLE 204<BR>VERIFIED MATERIALSSDR SWAA2022110865895Panel · pulledDOT A24-56 MID CABIN FLOOR BOARD PANEL 231XF HAS PULLED COMPOSITE FIBERS ON UPPER SIDE OF PANEL. / [01] EVALUATED DAMAGE; TOP SIDE OF PANEL IS REPAIRABLE IAW B737 SRM 53-00-50-2R-1 REPAIR 1; TAP TEST GOOD NO DELAMINATION NOTED. <BR><BR>CLEANED; PREPPED AREAS ISDR SWAA2022110865896Panel · pulledDOT A24-57 MID CABIN FLOOR BOARD PANEL 241AF HAS PULLED COMPOSITE FIBERS ON UPPER SIDE OF PANEL. / [01] EVALUATED AND FOUND MISSING PLIES THE LENGTH OF BOARD. TAP TEST GOOD. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PREPPED IAW SRM 53-00SDR SWAA2022110865901Panel · pulledDOT A24-58 MID CABIN FLOOR BOARD PANEL 232RF HAS PULLED COMPOSITE FIBERS ON UPPER SIDE OF PANEL. / [01] EVALUATED PANEL 232RF AND FOUND DAMAGE TO BE B.E.R. MANUFACTURED NEW PANEL PER SAMPLE. IAW B737-700 SRM 53-00-50-2R-0 PAR 1A & NOTE AND TABLE 204. (A1409978SDR SWAA2022110865902Panel · pulledDOT A24-60 MID CABIN FLOOR BOARD PANEL 242AF HAS PULLED COMPOSITE FIBERS ON UPPER SIDE OF PANEL. / [01] EVALUATED AND FOUND BOARD TO BE BER AND TO REPLACE BY FABRICATION PER SAMPLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL STEP 4 AND TABLE 204<BR>VERIFIED MATERIALSSDR SWAA2022110865904Panel · pulledDOT A24-64 MID CABIN FLOOR BOARD PANEL 232SF HAS PULLED COMPOSITE FIBERS ON UPPER SIDE OF PANEL. / [01] EVALUATED AND FOUND PANEL 232SF DAMAGED B.E.R.. FABRICATE NEW FLOOR BOARD PER SAMPLE AND DWG 144A5810-159 IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 204.<BRSDR SWAA2022110465684Floor Panel · pulledDOT A24-52 MID CABIN FLOOR BOARD PANEL 231ZF HAS PULLED COMPOSITE FIBERS ON UPPER SIDE OF PANEL. / [01] MID CABIN FLOOR BOARD 231ZF REPLACED BY FABRICATION OF NEW PANEL ON NON-ROUTINE #TTG8Q000FS2GY.;[02] VERIFIED STEPSSDR SWAA2022110465689Floor Panel · pulledDOT A24-53 MID CABIN FLOOR BOARD PANEL 241CF HAS PULLED COMPOSITE FIBERS ON UPPER SIDE OF PANEL. / [01] EVALUATED AND FOUND BOARD TO BE BER AND TO REPLACE BY FABRICATION PER SAMPLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL STEP 4 AND TABLE 204 <BR>VERIFIED MATERIALSDR SWAA2022092949146Light · inoperativeEXTERIOR LH OVERWING EMERGENCY LT INOP. OK TO CONTINUE PER MEL 33-14-01; SP1. REPLACED CABIN LH OVERWING EMERGENCY LIGHTING POWER SUPPLY IAW AMM 33-51-06. OPERATIONAL CHECK GOOD.SDR SWAA2022090750205None · inoperativeLH OVERWING EXIT LIGHT OVER DOOR INOP / [01] R&R?D LH EMERGENCY EXIT OVERWING BATTERY PACK AT BS 603 REF AMM 33-51-06. OPS CHECK GOOD.SDR SWAA2022080939953Light · inoperativeEMERGENCY BATTERY PACK (M1668) INOP. / [01] REMOVED AND REPLACED EMERGENCY BATTERY PACK (M1668) AND PERFORMED INSTALLATION TEST AS PER B737 AMM 33-51-06-960-805. TEST OK.;[02] VERIFIED STEP 1SDR SWAA2022080237597Shear Tie · corrodedAFT CARGO COMPARTMENT; FRAME SHEAR TIE AT BS 847; S-23L WL165 CORROSION NOTED.<[01] REMOVED DAMAGE SHEAR TIE AT AFT CARGO COMP BS 847 S-23L TO S-24L PER REF B737 SRM 51-40-02-0G-0.;[11] (RII) FINAL INSPECTED; SHEAR TIE EXFOLIATION FOUND OUT OF LIMITS; ACCOMPLISDR SWAA2022080236140Skin · corrodedFUSELAGE SKIN BELOW TOILET SERVICE DOOR HAS EVIDENCE OF CORROSION.<[01] INSTALLED EWIS PROTECTION AT AFT CARGO COMPARTMENT BETWEEN STA 847 AND STA 867 LBL 25 LOWER SECTION AS PER B737-700 AMM 20-60-07-913.;[02] REMOVED INSULATION BLANKETS AT AFT CARGO COMPARTMSDR SWAA2022072935196Skin · corrodedFUSELAGE SKIN BELOW TOILET SERVICE DOOR HAS EVIDENCE OF CORROSION / [01] TRANSFERRED TO SA-M 663 LP# 2039647 DUE TO FERRY FLIGHT.;[02] TRANSFERRED TO SA-M 663 LP# 2039647 DUE TO FERRY FLIGHT.SDR SWAA2022060112585Light · brokenEMERGENCY EXIT SIGN/PLACARD (LOWER) IS EVIDENCED AS BROKEN AT AIRCRAFT LEFT / [01] FOUND L/H OVERWING EXIT SIGN LOOSE. REINSTALLED L/H OVERWING EXIT SIGN PER AMM33-51-01SDR SWAA2022060113869Sign · brokenEMERGENCY EXIT SIGN/PLACARD (LOWER) IS EVIDENCED AS BROKEN AT AIRCRAFT LEFT / [01] FOUND L/H OVERWING EXIT SIGN LOOSE. REINSTALLED L/H OVERWING EXIT SIGN PER AMM33-51-01SDR SWAA2022012462453Light · inoperativeLEFT OVER WING EXIT LIGHT IS DIM ; / [01] RELAMPED EMER EXIT LIGHT REF AMM 33-51-04 OPS CK GOOD
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