N286WN
Service difficulty reports · 295
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 = 'N286WN' 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 = 'N286WN' 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 SWAA2022061411975Scuff Plate · crackedFWD CARGO DOOR CUT OUT LOWER SILL AFT CORNER SCUFF PLATE CRACKED. / [01] ACCOMPLISHED WELD REPAIR AND NDT INSPECTED DAMAGE SCUFF PLATE PER REF B737 SRM 53-30-15-2R-1; REPAIR ACCOMPLISHED BY OUTSIDE VENDOR; PO # 413565.;[02] VERIFIED STEP 1<BR>OK TO TREAT AND PSDR SWAA2022061409517Threshold Web · crackedFWD CARGO THRESHOLD WEB CRACKED AT FASTENER HOLE. 8-81 / [01] RECEIVED; LOCATED AND DRILLED NEW THRESHOLD WEB AT FWD CARGO AS PER B737-700 SRM 51-40-05-0G-0. INSTALLATION WILL BE ACCOMPLISHED ON MOC TTG8Q004E9LR.;[02] VERIFIED STEP 1;[03] COMPLETESDR SWAA2022061409785Floor Panel · delaminatedCOCKPIT PNL 211FW HAS DELAMINATED AREA. 8-82 / [01] PREPARED FOR REPAIR AT PANEL 211 FW AS PER B 737 SRM 51-70-06-2R-7;[02] VERIFIED STEP 1. OK TO APPLY REPAIR.;[03] REPAIRED AT PANEL 211 FW ;AS PER B737 SRM 51-70-06-2R-7 MATERIAL USED PO.1690463 AND PO.175379SDR SWAA2022061407709Panel · corrodedPANEL 192F LWR SURFACE HAS CORROSION AT 3 ANTENNA MOUNT AREAS. 8-80 / [01] RECEIVED NEW PANEL 192F ; THIS PANEL WILL BE INSTALL ON TTG8Q00BGPCF;[02] VERIFIED 1SDR SWAA2022061406196Floor Panel · crackedAFT EDGE OF FLOOR PANEL 241ADF IS CRACKED . / [01] NEW REPLACEMENT PANEL 241ADF FABRICATED BY OUTSIDE VENDOR AVENIR AVIATION LLC AND WILL BE INSTALLED ON ROUTINE CARD # TTG8Q00BGPF8;[02] VERIFIED AND INSPECTED STEP #1.<BR>CERTIFICATE OF CONFORMANCE. TRACKING#:SDR SWAA2022061409734Panel · elongatedL/W PANEL 561AB HAS FOUR HOLE SCREW ELONGATED. / [01] PERFORMED VISUAL AND TAP TEST INSPECTION ON PANEL #521VB AND FOUND NO ENTRY OF WATER; OIL; FUEL; OR OTHER UNWANTED MATERIAL PER B737 NDTM 51-05-01;[02] CORRECTION TO STEP 1 PERFORMED VISUAL AND TAP TEST INSSDR SWAA2022061410394Floor Panel · crackedFLT DECK CONTROL STAND LT ACCESS PANEL 211B IS CRACKED. 124-034 / [01] DRILLED A 1/16'' DIAMETER HOLE AT END OF THE CRACK AND PREPARED DAMAGED AREA TO APPLY REPAIR ON ACCESS PANEL 211B. REF B737-700 AMM 25-00-00-340-801 PARAGRAPH 8 E.;[02] VERIFIED STEP #1; ARSDR SWAA2022061405457Gusset · crackedFWD CARGO AT FRAME STA 500D GUSSET AT STRINGERS 19R CRACKED. 8-59 / [01] RECEIVED NEW GUSSET P/N 143A9481-5 P/O# 1770018;[02] REMOVED GUSSET AT FWD CARGO AT RT SIDE AT FRAME STA 500 D AT STRINGER 19R IN IAW SRM 51-40-02-0G-0;[03] LOCATED AND DRILLED NEW GUSSETSDR SWAA2022061413005Gusset · crackedFWD CARGO AT FRAME STA 500D GUSSET AT STRINGERS 19L CRACKED. 8-60 / [01] REMOVED CRACKED GUSSET AT FRAME STA 500D; STRINGER 19L FWD CARGO AS PER B737-7000 SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW GUSSET AT FRAME STA 500D; STRINGER 19L FWD CARGO AS PER BSDR SWAA2022061405222Panel · bulgedPNL 193B HAS INNER SURFACE AT SCREW HOLES BULGING. 8-48 / [01] PERFORMED VISUAL AND TAP TEST INSPECTION ON PANEL #193B AND FOUND NO ENTRY OF WATER; OIL; FUEL; OR OTHER UNWANTED MATERIAL PER B737 NDTM 51-05-01;[02] PREPARED PANEL 193B AT DAMAGED AREA FOR REPAIRSDR SWAA2022061404748Channel · corrodedAFT CARGO COMPARTMENT LH Z CHANNEL HAS SEVERAL SPOTS OF CORROSION BETWEEN STA 727A TO STA 807. / [01] RECEIVED NEW AFT CARGO LH Z CHANNEL (PO#1765410). PART WILL BE INSTALLED ON MOC #TTG8Q004F290.;[02] VERIFIED STEP #1SDR SWAA2022061404750Shield · corrodedAFT CARGO COMPARTMENT;FWD FLOOR SUPPORT SHIELD HAS CORROSION BETWEEN STA 767 TO STA 792. / [01] RECEIVED NEW AFT CARGO COMPARTMENT FWD FLOOR SUPPORT SHIELD (PO#1728471). PART WILL BE INSTALLED ON MOC #TTG8Q004F290.;[02] VERIFIED STEP #1SDR SWAA2022061404739Hinge Box · crackedCRACK AT R1 DOOR FWD CUTOUT; DOOR HINGE UPPER BOX SEAL SUPPRESSOR MKD 126-01. / [01] REMOVED DOOR HINGE UPPER BOX SEAL SUPPRESSOR AT<BR>R1 DOOR FWD CUTOUT. REF.SRM-51-40-02-0G-0;[02] LOCATED AND DRILLED HINGE BOX. REF. B-737-7 SRM-51-40-05-0G-0;[03] CORRECTIONSDR SWAA2022061403499Floor Panel · delaminatedAFT WET AREA FLOOR PANEL 241 XF FOUND DELAMINATED / [01] REPLACEMENT FLOOR PANEL 241XF FABRICATED BY OUTSIDE VENDOR AVENIR AVIATION LLC AND WILL BE INSTALLED ON ROUTINE CARD.;[02] REPLACEMENT FLOOR PANEL 241XF FABRICATED BY OUTSIDE VENDOR AVENIR AVIATION LLC ASDR SWAA2022061403496Floor Panel · delaminatedAFT WET AREA FLOOR PANEL 242 UF FOUND DELAMINATED AND UPPER SURFACED AREAS PEELED / [01] RECEIVED BRAND NEW PANEL P/N: 147A5810-95 ; PANEL WILL BE INSTALLED ON T/C: TTG8Q00BGQJX.;[02] RECEIVED BRAND NEW PANEL P/N: 147A5810-95 ; PANEL WILL BE INSTALLED ON T/C: SDR SWAA2022061403503Floor Panel · corrodedFWD WET AREA FLOOR PANEL 221 AF FOUND INSERTS CORRODED AND DELAMINATED / [01] RECEIVED NEW FLOOR PANEL # 221 AF ; THIS PANEL WILL BE INSTALL ON TTG8Q00BGQKX;[02] VERIFIED; STEP # 1.SDR SWAA2022061403509Floor Panel · peelingPASSENGER CABIN FLOOR 241 AF FOUND AREAS OF UPPER SURFACED PEELED / [01] RECEIVED NEW CABIN FLOOR 241AF (PO#1752943). PANEL WILL BE INSTALLED ON ROUTING CARD #TTG8Q00BGPF4.;[02] FINAL INSPECTION; RECEIVED NEW CABIN FLOOR 241AF (PO#1752943). PANEL WILL BE INSTASDR SWAA2022061403321Floor Panel · corrodedLH PASSENGER CABIN FLOOR ACCESS PANEL 221CF HAS INSERTS MISSING AND CORRODED. (STA 300) / [01] RECEIVED BRAND NEW PANEL P/N: 141A5810-9. PANEL WILL BE INSTALLED ON T/C: TTG8Q00BGQKT.;[02] NEW PNL VERIFIED ; INSPECTED .SDR SWAA2022061403322Floor Panel · corrodedLH PASSENGER CABIN FLOOR ACCESS PANEL 221EF HAS SEVERAL INSERTS MISSING; BROKEN AND CORRODED. (STA 350) / [01] RECEIVED BRAND NEW PANEL P/N: 141A5810-249. PANEL WILL BE INSTALLED ON T/C: TTG8Q00BGQKP.;[02] NEW PNL VERIFIED ; INSPECTED .SDR SWAA2022061403318Floor Panel · corrodedLH PASSENGER CABIN FLOOR ACCESS PANEL 222BF HAS SEVERAL CORRODED INSERTS. (STA 300) / [01] RECEIVED NEW PANEL P/N: 141A5810-464. PANEL WILL BE INSTALLED ON T/C: TTG8Q00BGQKF.;[02] NEW PNL VERIFIED ; INSPECTED .SDR SWAA2022061403323Floor Panel · brokenLH PASSENGER CABIN FLOOR ACCESS PANEL 222DF HAS BROKEN EDGE AT ONE INSERT HOLE LOCATION / [01] NEW REPLACEMENT PANEL 222DF FABRICATED BY OUTSIDE VENDOR AVENIR AVIATION LLC. AND WILL BE INSTALLED ON ROUTINE CARD # TTG8Q00BGQKB.;[02] VERIFIED AND INSPECTED.;[03]SDR SWAA2022061403326Floor Panel · brokenLH PASSENGER CABIN FLOOR ACCESS PANEL 221GF HAS SIDE EDGE TIP BROKEN. / [01] RECEIVED BRAND NEW PANEL P/N: 141A5810-181. PANEL WILL BE INSTALLED ON T/C: TTG8Q00BGQKK.;[02] NEW PNL VERIFIED ; INSPECTED .SDR SWAA2022061403327Floor Panel · corrodedLH PASSENGER CABIN FLOOR ACCESS PANEL 221BF HAS SEVERAL MISSING AND CORRODED INSERTS. STA 280. / [01] RECEIVED BRAND NEW PANEL P/N: 141A5810-56. PANEL WILL BE INSTALLED ON T/C: TTG8Q00BGQKV.;[02] NEW PNL VERIFIED ; INSPECTED .SDR SWAA2022061403328Floor Panel · brokenLH PASSENGER CABIN FLOOR ACCESS PANEL 221BF HAS A BROKEN EDGE TIP. / [01] RECEIVED BRAND NEW PANEL P/N: 141A5810-56. PANEL WILL BE INSTALLED ON T/C: TTG8Q00BGQKV.;[02] VERIFIED AND INSPECTED NEW PNL.SDR SWAA2022061403320Floor Panel · delaminatedLH PASSENGER CABIN FLOOR ACCESS PANEL 221DF HAS DELAMINATION AND A SIDE EDGE BROKEN. STA 300. / [01] RECEIVED NEW FLOOR PANEL 221DF; INSTALLATION WILL BE ACCOMPLISHED ON FAULT TTG8Q00BGQKR .;[02] NEW FLOOR PANEL 221DF; INSTALLATION WILL BE ACCOMPLISHED ON FAULSDR SWAA2022061403523Intercostal · crackedFWD CABIN BETWEEN STA 312 AND STA 328 LBL 46 WL 208.1 INTERCOSTAL IS CRACKED AS MARKED. 124-014 / [01] REMOVED INTERCOSTAL AT FWD CABIN BTW STA 312 AND 328 LBL 46 WL 208.1 AS PER B737-700 SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW INTERCOSTAL AT FWD CABINSDR SWAA2022061403525Intercostal · crackedFWD CABIN BETWEEN STA 277 AND STA 294.5 RBL 1 WL 208.1 INTERCOSTAL IS CRACKED AS MARKED. 124-019 / [01] REMOVED DAMAGE INTERCOSTAL AT FWD CABIN SB 277 TO 294.5 RBL1 PER REF B737 SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW INTERCOSTAL PER REF B737 SRM 51-40SDR SWAA2022061403526Intercostal · crackedFWD CABIN BETWEEN STA 344 AND STA 360 LBL 11 WL 208.1 INTERCOSTAL IS CRACKED AS MARKED. 124-020 / [01] REMOVED INTERCOSTAL AT STA 344 AND 360; LBL 11; WL 208.1 AREA AS PER B737-700 SRM 51-40-02-0G-0.;[02] CUT UPPER FLANGE DAMAGE AREA AT INTERCOSTAL REF B737-70SDR SWAA2022061403530Floorbeam · corroded*CORROSION* FWD CABIN STA 328 RBL 42.5 TO RBL 56 WL 208.1 FLOOR SUPPORT BEAM HAS CORROSION AS MARKED. 124-023 / [01] REMOVED CORROSION AT FWD CABIN STA 328 RBL 42.5 TO RBL 56 WL 208.1 FLOOR SUPPORT IAW SRM 51-10-02-0G-0 REMAINING MATERIAL 0.108' FOUND OUT OF LSDR SWAA2022061403527Intercostal · crackedFWD CABIN BETWEEN STA 344 AND STA 360 BL 0 WL 208.1 INTERCOSTAL IS CRACKED AS MARKED. 124-021 / FABRICATE NEW REPAIR FITTING FOR NEW INTERCOSTAL REPAIR PER REF B 737 SRM 53-10-51-2R-9 FIG 207 ; VENDOR PO# 1770639 ACCOMPLISHED FLAP PEEN AT CUT EDGES AND REPAIR SDR SWAA2022061403531Intercostal · crackedFWD CABIN BETWEEN STA 294.5 AND STA 312 RBL 15 WL 208.1 INTERCOSTAL IS CRACKED AS MARKED. 124-024 / [01] REMOVED INTERCOSTAL AT FWD CABIN BTW STA 294.5 AND STA 312; RBL 15 WL 208.1; AS PER B737-700 SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW INTERCOSTAL (PSDR SWAA2022061403515Structure · corrodedL2 DOOR LOWER SILL INNER CHORD HAS SEVERAL CORROSION FROM STA 920 TO STA 1008. / [01] REMOVED ALL CORROSION FROM L2 DOOR LOWER SILL INNER CHORD AT STA 920 TO STA 1008 IAW B 737-700 SRM 51-10-02-0G-0;[02] VERIFIED STEP #1; CORROSION REMOVED.;[03] PERFORMED UT TSDR SWAA2022061403522Intercostal · corroded*CORROSION* FWD CABIN BETWEEN STA 294.5 AND STA 312 LBL 12 WL 208.1 INTERCOSTAL HAS CORROSION AS MARKED. 124-017 / [01] RE-INSPECTED AREAS AT FWD CABIN FLOOR BETWEEN STA 294.5 AND STA 312 LBL 12 WL 208.1 FOUND OUT OF LIMITS ( EXFOLIATION CORROSION) AS PER REF SDR SWAA2022061403524Support Beam · corroded*CORROSION* FWD CABIN STA 312 LBL 12 TO LBL 48 WL 208.1 FLOOR SUPPORT BEAM HAS CORROSION AROUND FASTENER HOLES AS MARKED. 124-018 / [01] REMOVED CORROSION AT FWD CABIN STA 312 LBL 12 TO LBL 48 WL 208.1 FLOOR SUPPORT BEAM IAW SRM 51-10-02-0G-0;[02] VERIFIED STESDR SWAA2022061403513Floorbeam · corrodedFLOORBEAM STA 986.5;BETWEEN LBL40 TO LBL47 HAS CORROSION. / REMOVED EXFOLIATED UPPER CHORD OF THE FLOORBEAM AT STA 986.5 FROM BL 0 TO RBL 50 WL 208.1 REF B737-700 SRM 51-40-02-0G-0.FABRICATED LOCATED AND DRILLED NEW UPPER TEE CHORD FROM LBL 50 TO RBL 50 STA. 9SDR SWAA2022061403506Shear Web · corrodedCORROSION AT RIGHT SIDE WEB: STA 219 STA 225; RBL 40; WL 208. 8-39 / [01] REMOVED CORROSION AT RIGHT SIDE WEB STA 219- STA 225; RBL 40 WL 208.9 IAW SRM 51-10-02-0G-0[22] EVALUATED DAMAGE AREA AT RT SIDE SHEAR TIE WEB BS219-225 RBL 40; FOUND EXFOLIATION OUT OF SDR SWAA2022061403536Attach Angle · crackedCRACK AT UPPER VAPOR BARRIER ATTACH ANGLE STA 663 RBL 7 SEEN THRU AC BAY. 8-28 / [01] REMOVED FASTENERS AT UPPER VAPOR BARRIER ATTACH ANGLE STA 663 RBL 7 FOR ACCESS TO REPAIR IN REF B 737-700 SRM 51-40-02-0G-0;;[21] ACCOMPLISHED PERMANENT REPAIR OF DAMAGE UPPESDR SWAA2022061403033Rib · crackedRH HORIZONTAL STABILIZER;RIB 4 STAB STA 120.3;# 4 STIFFENER IS CRACKED. / [01] CUT AND REMOVED THE DAMAGE FROM THE VERTICAL STIFFENER #4 OF THE RIB #4 FIG 202/ REPAIR 4 SHEET 1 IN IAW SRM 51-10-02-0G-0 AND 55-10-09-2R-4TRIMMED OUT DAMAGED HOLES AT LOWER CHORD SDR SWAA2022061403032Stiffener · crackedRH HORIOTAL STABILIZER RIB 4 STAB STA 120.3;#3 STIFFENER IS CRACKED. / CUT AND REMOVED THE DAMAGE FROM THE WEB AND MEASURED THE CORNER RADII OF THE WEB CUTOUT A MINIMUM OF 0.167' IN IAW SRM 51-10-02-0G-0 AND 55-10-09-2R-4;[02] PERFORMED HFEC INSP ON CUT OUT ARSDR SWAA2022061403040Frame · crackedABOVE L1 CUTOUT LWR END OF FRAME BS 312 CRACKED AT RADIUS BETWEEN S-5L AND S-6L. 8-25 / FABRICATED REPAIR PART FOR STA 312 UPPER CHORD BETWEEN S-5L - S6L; MATERIAL USED 7075-O 0.063' PO#1742517 REF B737-700 SRM 53-10-07-2R-1 FIG 203 TABLE 201.;[03] HEAT TREATESDR SWAA2022061402310Floor Panel · corrodedRH PASSENGER CABIN FLOOR ACCESS PANEL 242TF AT STA 940 HAS SEVERAL INSERTS CORRODED. / [01] RECEIVED NEW PANEL P/N: 147A5810-94. PANEL WILL BE INSTALLED ON T/C: TTG8Q00BGQJZ.;[02] RECEIVED NEW PANEL P/N: 147A5810-94. PANEL WILL BE INSTALLED ON T/C: TTG8Q00BGQJSDR SWAA2022061403030Floor Panel · peelingCABIN FLOOR PNL 232SF HAS AREAS OF UPPER SURFACED PEELED. 8-22 / [01] RECEIVED NEW PANEL 232SF; INSTALLATION WILL BE ACCOMPLISHED ON FAULT TTG8Q00BGPGW;[02] VERIFIED STEP 1SDR SWAA2022061403045Floor Panel · peelingCABIN FLOOR PANEL 231ZF HAS UPPER SURFACE PEELED. 8-24. / [01] RECEIVED FLOOR PANEL 231ZF AND INSTALLED PANEL ON ITEM TTG8Q00BGPH8.;[02] VERIFIEDSTEP #1SDR SWAA2022061403493Stiffener · crackedRT A/C BAY HAS IB AFT CORNER FITTING CRACKED AT UPPER END BS 663 RBL 6. 8-27 / [01] REMOVED HORIZONTAL SUPPORT ANGLE AT BS 663 FOR ACCESS PER REF B737 SRM 51-40-02-0G-0;[02] PARTIALLY REMOVED VERTICAL STIFFENER AT BS 663 RBL 6 PER REF B737 SRM 51-40-02-0G-0;[0SDR SWAA2022061403043Floor Panel · delaminatedAFT WET AREA FLOOR PANEL 241 ABF FOUND DELAMINATED / [01] RECEIVED BRAND NEW PANEL P/N: 141A5810-88. PANEL WILL BE INSTALLED ON T/C: TTGQ00BGPFC.;[02] NEW PNL VERIFIED ; INSPECTED .SDR SWAA2022061403044Structure · corrodedR2 DOOR LWR SILL INNER CHORD HAS EXFOLIATING CORROSION BS 947-996. 3-30 / [01] REMOVED EXFOLIATED LWR SILL INNER CHORD AT R2 DOOR IAW SRM 51-40-02-0G-0.;[02] VERIFIED STEP #1; EXFOLIATED SILL REMOVED.;[03] LOCATED AND DRILLED NEW LOWER SILL INNER CHORD AT R 2 SDR SWAA2022061403042Structure · corrodedL1 DOOR LWR SILL INNER CHORD HAS EXFOLIATING CORROSION BS 305-315. DOT 8-29 / [01] REMOVED EXFOLIATED L1 DOOR LWR SILL INNER CHORD IAW B737-700 SRM 51-40-02-0G-0.;[02] VERIFIED STEP #1; LWR SILL INNER CHORD REMOVED.;[03] BEGAN LOCATING AND DRILLING L1 DOOR LWRSDR SWAA2022061403038Stiffener · crackedLH HORIZONTAL STABILIZER RIB 5 STAB STA 129.5;#3 STIFFENER IS CRACKED. / [01] REMOVED DAMAGE AREA AT LH HORIZONTAL STABILIZER RIB 5 STA. 129.5 # 3 STIFFENER IAW B737-700 SRM 55-10-09-2R-4 FIG202.[14] (FINAL) REMOVED DAMAGE AREA AT LH HORIZONTAL STABILIZER RIB SDR SWAA2022061401843Floor Panel · crackedAFT CARGO COMPARTMENT FWD BULKHEAD PANEL #141JW; EDGE CRACK/DETERIORATED. (DOT-003). / [01] FABRICATED AFT CARGO COMPARTMENT FWD BULKHEAD PANEL #141JW IAW AMM 25-52-01-201-801. MATERIAL USED: A60SG4W.;[02] FINAL INSPECTION; PANEL FABRICATED.SDR SWAA2022061401841Floor Panel · crackedAFT CARGO COMPARTMENT FWD BULKHEAD PANEL #142MW; EDGE CRACK/DETERIORATED. (DOT-002). / [01] FABRICATED AFT CARGO COMPARTMENT FWD BULKHEAD PANEL 142MW IAW AMM 25-52-01-201-801. MATERIAL USED A60SG4W-60144.;[02] FINAL INSPECTION; BULKHEAD PANEL FABRICATED.
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