N428WN
Service difficulty reports · 302
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 = 'N428WN' 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 = 'N428WN' 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 SWAA2022072922425Floor Panel · elongatedAFT CARGO COMPARTMENT FLOOR PANEL 140BF HAS ELONGATED HOLES / [01] REPLACE FLOOR PANEL 140 BF AS PER B737-700 AMM 25-52-01-201.;[02] VERIFIED STEP 1SDR SWAA2022072922550Stringer · corrodedCORROSION AT STRINGER SPLICE END STR 28L; STA 360; WL 149 / [01] INSTALLED EWIS PROTECTED AROUND CORROSION AREA AT STR 28L STA 360 WL 149 PER BOEING 737-700 AMM 20-60-07-913-801.;09] LOCATED AND PARTIALLY DRILLED NEW STRINGER SPLICE AT STA 360; STR 28L PER BOESDR SWAA2022072922264Baffle · crackedAFT OF AFT CARGO COMPARTMENT BILGE FLOOR SUPPORT BRACKET CRACKED @ S-25R O/B UNDERNEATH Z CHANNEL STA 947.75 MKD DOT / [01] REMOVED AND REPLACED BILGE FLOOR SUPPORT ( BAFFLE ) AT AFT CARGO COMPARTMENT ABOVE S-25R UNDERNEATH Z CHANNEL AS PER B737-700 SRM 51-40-SDR SWAA2022072922266Stringer · crackedFORWARD PASSENGER COMPARTMENT STR. 15R CRACKED AT FASTENER HOLE B.S. 460+4. (51-001) / [01] REMOVED[ 19] FABRICATED SPLICED AND SHIMS BOTH SIDE AT FWD PASSENGER COMP STR 15 R FWD STA 460+4' IAW B737 SRM 53-00-03-2R-1.;[20] PERFORMED HFEC AT CUT OUT AT STR-15R SDR SWAA2022072922267Stringer · crackedFORWARD PASSENGER COMPARTMENT STR. 15R CRACKED AT FASTENER HOLE B.S.460+16. (51-002) / [01] REMOVED FASTENER FOR ACCESS NDT REF B-737-700 SRM 51-40-02-0G-0;[19] FABRICATED SPLICED AND SHIMS BOTH SIDE AT FWD PASSENGER COMP STR 15 R AFT STA 460+16 'IAW B737 SRM SDR SWAA2022072922271Stringer · crackedFORWARD PASSENGER COMPARTMENT STR. 15L CRACKED AT FASTENER HOLE B.S. 460+4. (51-003) / [01] REMOVED FASTENER FOR ACCESS NDT REF B-737-700 SRM 51-40-02-0G-0;21] FABRICATED SPLICED AND SHIMS AT FWD PASSENGER COMP STR 15 L FWD STA 460 +4'IAW B737 SRM 53-00-03-2R-SDR SWAA2022072922268Stringer · crackedFORWARD PASSENGER COMPARTMENT STR. 15L CRACKED AT FASTENER HOLE B.S. 460+16. (51-004) / [01] REMOVED FASTENER FOR ACCESS NDT REF B-737-700 SRM 51-40-02-0G-0;[22] FABRICATED SPLICED AND SHIM AT FWD PASSENGER COMP STR 15 L AFT STA 460+ 16'IAW B737 SRM 53-00-03-2SDR SWAA2022072922261Channel · corrodedCORROSION ** AFT CARGO COMPARTMENT BILGE R/H ZEE CHANNEL FLOOR SUPPORT @ S-25R FROM STA 727 TO STA 767 MKD DOT / [01] AFTER CORROSION EVALUATION AT R/H ZEE FOUND SPOTS OUT OF LIMITS AT STA727D TO 767 AS PER B737 -700 SRM 53-00-53-1A-2.( FROM STA 727 THRU STA 7SDR SWAA2022072922262Channel · corrodedCORROSION. SPOTS AFT CARGO BILGE L/H ZEE CHANNEL S-25L FROM STA 727 TO STA 847 / [01] CLEANED CORROSION AT AFT CARGO COMP BILGE L/H Z CHANNEL ABOVE STR 25L FROM STA 727 TO STA 847;FOUND EXFOLIATED CORROSION OUT OF LIMITS AT STA 727 A AND STA 767 AS PER REF B73SDR SWAA2022072922272Rib · crackedL/H HORIZONTAL RONT SPAR MOVEABLE L/E FAIRING CRACKED @ RIB 2 END MKD DOT / [01] PERFORMED HFEC INSP. ON L/H HORIZ STAB. FRONT SPAR MOVABLE L/E FAIRING @ RIB #2 END IAW B737 NDT PART 6 51-00-00 PROC. 23. CRACK CONFIRMED; EQUIP: NORTEC 600 B/C 172389 CAL DUE: 3SDR SWAA2022072921370Fitting · crackedVERTICAL FIN; TERMINAL FITTING ASSY. LOWER AFT TRAILING EDGE SPRING ANGLE 2EA. CRACKS NOTED. (DOT 223-001). / [01] REMOVED ON VERTICAL FIN TERMINAL FITTING ASSY. LOWER AFT TRAILING EDGE SPRING ANGLE IAW B737 SRM 51-40-02-0G-0.;[02] VERIFIED 1;[03] LOCATED AND SDR SWAA2022072920814Panel · elongatedAFT OF MAIN W/W ACCESS PANEL # 194 E HAS ELONGATED & CRACKED HOLES AT EDGES / [01] MEASUREMENTS;[02] CLEANED AREA AND REPAIRED DAMAGE HOLES AS MARKED ON ACCESS PANEL 194E WITH A PERMANENT REPAIR AS PER B737 SRM 51-70-04-2R-9; MATERIALS USED PO#1690463 AND PO#1SDR SWAA2022072920815Fitting · crackedL/W REAR SPAR T/E FIXED DEFLECTION CONTROL RIB PANEL LOWER VERTICAL BULB SEAL FITTING CRACKED I/B SIDE MKD DOT / [01] REMOVED L/W REAR SPAR T/E FIXED DEFLECTION CONTROL RIB SEAL FITTING AS PER B-737-700 SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW L/W REAR SDR SWAA2022072920809Floor Panel · delaminatedCABIN FLOOR PANEL 231XF HAVE DELAMINATION IN MULTIPLES AREAS. / [01] MEASUREMENTS;[02] REPAIRED TOP SURFACE DAMAGE AS MARKED ON MAIN CABIN FLOOR PANEL #231XF WITH A PERMANENT REPAIR AS PER B737 SRM 53-00-50-2R-1. MATERIALS USED PO#1690463 AND PO#1740319;[03] PSDR SWAA2022072920813Support Angle · damagedSUPPORT ANGLE FRETTEN MARKS AT LOWER FUSELAGE CENTER WING BOX O/B L/H AIR CONDITION AIR EXIT DUCT MKD DOT / [01] BLENDED OUT DAMAGE AT SUPPORT ANGLE LOWER FUSELAGE CENTER WING BOX O/B L/H A/C AIR EXIT DUCT AS PER SRM 51-10-02-0G-0.;[02] VERIFIED BLEND;[03] EVASDR SWAA2022072920810Floor Panel · delaminatedCABIN FLOOR PANEL 231AF HAVE DELAMINATION IN MULTIPLES AREAS. / [01] MEASUREMENTS;[02] CLEANED DAMAGE AREA AND REPAIRED DAMAGE ARE AS MARKED WITH A PERMANENT REPAIR ON MAIN CABIN FLOOR PANEL #231AF UPPER SURFACE AS PER B737SRM 53-00-50-2R-1; MATERIALS USED PO#SDR SWAA2022072920510Floor Support · crackedMAIN CABON CENTER WING BOX FLOOR SUPPORT BREAK CRACKED @ STA 540 LBL-1 MKD DOT / [01] REMOVED FLOOR CABIN PANEL 231UF AS PER B-737-700 SRM 51-40-02-0G-0.;[02] REMOVED MAIN CABIN CENTER WING BOX FLOOR SUPPORT STA 540 LBL-1 AS PER B-737-700 SRM 51-40-02-0G-0.;[0SDR SWAA2022072920511Floor Support · crackedMAIN CABON CENTER WING BOX FLOOR SUPPORT BREAK CRACKED @ STA 540 RBL-1 MKD DOT / [01] REMOVED FLOOR CABIN PANEL 231UF AS PER B-737-700 SRM 51-40-02-0G-0.;[02] REMOVED MAIN CABIN CENTER WING BOX FLOOR SUPPORT STA 540 RBL-1 AS PER B-737-700 SRM 51-40-02-0G-0.;[0SDR SWAA2022072920512Frame · crackedFWD CABIN WET AREA L/H FUSELAGE ATTACHED FRAME CRACKED @ LOWER FLAGE CUTOUT ABOVE L-1 DOOR CUTOUT SILL STA 312 MKD DOT / [01] REMOVED FASTENERS AS REQUIRED TO ACCESS REPAIR UPPER CHORD AT STA 312 BETWEEN STG 5L AND 6L IN REFERENCE B-737 SRM 51-40-02.;[02] VERISDR SWAA2022072919193Stiffener · crackedLOWER FUSELAGE. CENTER WING BOX STIFFENER CRACKED @ LOWER RADIUS W/W FWD BULKHEAD STA 663.75 LBL 25 O/B OF AIR CONDITION AIR EXIT DUCT MKD DOT / [01] REMOVED STIFFENER AT LOWER FUSELAGE STA 663.75 LBL 25 AS PER SRM 51-40-02-0G-0.;[02] REMOVED ONE (EACH) WIRE BSDR SWAA2022021471878Lens · delaminatedEMERGENCY EXIT LIGHT LENS BETWEEN 13/14DEF IS SEPARATING FROM OVERHEAD BIN BULLNOSE. ; EMERGENCY EXIT LIGHT LENS BETWEEN 1314DEF IS SEPARATING FROM OVERHEAD BIN BULLNOSE. / [01] INSTALLED EMERGENCY LITE COVER LENS BETWEEN SEATS 13/14 DEF PER AMM 33-51-03; [02]SDR SWAA2022013164135None · inoperativeSUPPLEMENTAL INFORMATION: F/O SIDE OVERWING EXIT DOOR LIGHT INOP 01/30 DEN MX REPORTS BALLAST REQUIRED FOR FIX / [01] AC OK TO CONTINUE PERMEL 33-2-03 SP1B. AUTH #45437;[02] REPLACED RIGHT OVERWING EXIT DOOR LIGHT BALLAST ASSY; SATISFACTORY OP CK REF AMM 33-21SDR SWAA2021121451888Panel · elongatedSUPPLEMENTAL INFORMATION: 193D CENTER WHEEL WELL PANEL HAS 4 ENLARGED HOLES AT FWD CENTER / [01] DRILLED AND TRIMMED NEW PANEL REF SRM 51-40-05SDR SWAA2021111843819Sign · brokenSERVICE ENTRY DOOR FWD EXIT SIGN BROKE OFF ; / [01] R/R FWD SERVICE DOOR EMERGENCY EXIT LIGHT ASSY IAN 33-51-01SDR SWAA2021102632433None · out of adjustSUPPLEMENTAL INFORMATION: FWD SERVICE DOOR HANDLE CAM PLATE HAS PLAY ; / [01] ADJUSTED FWD SERVICE DOOR HANDLE CAM PLATE PER AMM 52-41-00SDR SWAA2020112331192Wire · exposedREF SA-M 767 H24921-6 EMERGENCY EXIT LIGHT SWITCH AT AFT F/A STATION HAS EXPOSED SPRING WIRE. R & R AFT EMERGENCY LIGHT SWITCH COVER AT AFT F/A STATION, REF AMM 33-51-03.SDR SWAA2020082509877Light · inoperativeRH OVERWING EXTERIOR EMERGENCY LIGHT INOP / REMOVED AND REPLACED SLIDE OVERWING EMERGENCY LIGHT RH AS PER B737 AMM 33-51-04-960-801 TEST NORMAL.SDR SWAA2020082508760Cover · damagedMAIN CABIN FWD L1 DOOR HEADER LIGHT COVER DAMAGED / REMOVED AND REPLACED FWD L1 DOOR HEADER LIGHT COVER AS PER REF B737-7 AMM 33-51-01-960-802. PERFORMED EMERGENCY LIGHTS OPERATIONAL CHECK AND OPERATIONAL TEST CHECK NORMAL PER B737 AMM 33-51-00-720-801 AND 33-SDR SWAA2020082508761Light · damagedMAIN CABIN R1 DOOR HEADER EMMERGENCY LIGHT ASSY DAMAGED / REMOVED AND REPLACED R1 DOOR HEADER EMERGENCY LIGHT ASSY AS PER REF B737-7 AMM 33-51-01-960-802. PERFORMED EMERGENCY LIGHTS OPERATIONAL CHECK AND OPERATIONAL TEST; CHECK NORMAL PER B737 AMM 33-51-00-720SDR SWAA2021081907956Dome Nut · brokenFWD CARGO STA.500D LOWER SIDE OF STR.17R; 1 EACH DOME NUT BROKEN / REMOVED AND REPLACED DOME NUT AT FWD CARGO STA 500D LOWER SIDE OF STR 17 AT RH B737 SRM 51-40-02-0G-0SDR SWAA2020082508218Baffle · crackedFWD CARBO COMP FLOOR R/H ZEE CHANNEL BAFFLE CRACKED FROM STA 500A TO 500B. / REPAIRED CRACKED BAFFLE @ FWD CARGO COMP. FLOOR R/H ZEE CHANNEL FROM STA 500A TO 500B AS PER B737-700 SRM 53-30-53-2R-1SDR SWAA2020082506991Skin · crackedL/H WING INBOARD MAIN T/E FLAP LOWER SURFACE SKIN HAS 0.250' CRACK; 12' FROM THE T/E & 15' FROM THE OUTBOARD EDGE; / CLEANED AND REPAIRED DAMAGE AREA AS MARKED ON L/W I/B MAIN FLAP T/E O/B WEDGE LOWER SURFACE AS PER B737 SRM 51-70-10-2R-4; REPAIR 4 PERMANENT SDR SWAA2021071504368Support Angle · crackedAFT OF AFT CARGO COMPARTMENT WATER SERVICE COMPARTMENT BASE FITTING AFT SUPPORT ANGLE CRACKED AT FLOOR GILGE BETWEEN STA 905 & 927 MKD DOT 60-028 / REMOVED AND REPLACED AFT CARGO COMPARTMENT WATER SERVICE BASE FITTING AFT SUPPORT ANGLE AS PER B737-700 SRM 51-4SDR SWAA2021072903863Web · corroded***CORROSION*** FWD CARGO ENTRY THRESHOLD HAS SPOTS OF LIGHT CORROSION; BS 440-492 WL 156; RBL24 / REMOVED OLD WEB AT FWD CARGO DOOR ENTRY AND REPLACED WITH NEW WEB (THRESHOLD) AS REQUIRED REF # B737 SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; SRM 51-40-08-0G-0 AND SDR SWAA2021040803860Channel · damagedFWD CARGO R/H Z CHANNEL HAS ELONGATED HOLES FROM STA. 500A TO AFT BULKHEAD. / REPLACED 'Z' CHANNEL@ FWD CARGO R/H SIDE FROM STA 500A TO AFT BULKHEAD AS PER B737-700 51-40-02-06-0SDR SWAA2021033003858Channel · elongatedFWD CARGO R/H Z CHANNEL HAS ELONGATED HOLES FROM STA.420 TO STA.440. / REMOVED AND REPLACED FWD CARGO Z CHANNEL(SHIELD) BS 420 TO 440 REF B737-700 SRM 51-40-02-0G-0.SDR SWAA2020082503859Channel · corrodedCORROSION FWD CARGO L/H Z CHANNEL HAS SPOTS OF CORROSION AROUND NUTPLATE HOLES FROM STA.500 TO STA. 500B; LBL22; WL 156 / REPLACED CORRODED SECTION OF 'Z' CHANNEL AT FWD CARGO L/H SIDE; LBL 22; WL 156; STA 500 - AFT BULKHEAD AS PER B737-700 SRM 53-00-53-2R-6SDR SWAA2021062903400Scuff Plate · crackedFORWARD CARGO FWD SCUFF PLATE CRACKED / RECIEVED WELDED SCUFF PLATE FOR FWD CARGO FWD CORNER INSTALLATION WILL BE ACCOMPLISHED ON ROUTINE CARD J753-140-00-01YSDR SWAA2020082503394Floorbeam · corrodedCORROSION ON THE CABIN FLOOR FRAME AT STA.986.5 HAS CORROSION AROUND 3 NUTPLATE HOLES FROM LBL 6 TO RBL 15. WL 208. / ACCOMPLISHED EA 1-A53-8241 REV 3.; CORROSION REMOVED ON CABIN FLOOR BEAM AROUND NUTPLATES HOLES; STA 986.5 FROM LBL 6 TO RBL 15; WL 208SDR SWAA2020082503395Floorbeam · corroded***CORROSION*** CABIN FLOOR FRAME HAS CORROSION AROUND NUTPLATE HOLE STA.986.5 RBL44. WL 208. / ACCOMPLISHED EA 1-A53-8241 REV 3.; CORROSION REMOVED ON CABIN FLOOR BEAM AROUND NUT PLATES HOLES STA 986.5 RBL 44; WL 208SDR SWAA2020082503396Floorbeam · corrodedCORROSION ON THE CABIN FLOOR FRAME HAS CORROSION AROUND NUTPLATE HOLE AT STA.986.5 RBL 36. WL 208. / ACCOMPLISHED EA 1-A53-8241 REV 3.; CORROSION REMOVED ON CABIN FLOOR BEAM; AROUND NUT PLATES HOLES; STA 986.5 RBL 36'; WL 208SDR SWAA2020082503390Structure · corrodedCORROSION ON THE INNER CHORD AT L2 ENTRANCE HAS CORROSION; STA.947.5 TO STA.986.5. LBL 47.50 TO LBL 53. WL 208. / REMOVED CORROSION AT L2 ENTRE DOOR INNER CHORD; FOUND OUT OF LIMITS; REMOVED AND REPLACED L2 DOOR INNER CHORD PER REF. B737-700 SRM 51-40-02-0G-0SDR SWAA2020082503393Structure · corrodedCORROSION ON THE RT INNER CHORD JUST I/B OF R2 DOOR CORRODED FROM STA.947.5 TO STA.987. RBL 47.50 TO RBL 53. WL 208. / REMOVED CORROSION; FOUND TO BE OUT OF LIMITS; REMOVED AND REPLACED R/H R2 DOOR INNER CHORD PER REF B737-700 SRM 51-40-02-0G-0 AND DWG 147A854SDR SWAA2021062903384Attach Angle · corroded***CORROSION*** FWD CABIN AT L-1 DOOR SILL SCUFF PLATE ATTACHMENT I/B ANGLE HAS CORROSION. [DOT 124-020] STA. 303-348; W.L. 208; STR 17L / REPLACED FWD CABIN L-1 DOOR SILL SCUFF PLATE ATTACHMENT I/B ANGLE AS PER B737-700 SRM 51-40-02-0G-0SDR SWAA2021052603386Gusset · crackedFWD CARGO STA 500D S-19R GUSSET BRACKET CRACK. / REMOVED AND REPLACED GUSSET AT FWD CARGO COMPARTMENT STA 500D S-19R REF B737-7 SRM 51-40-02-0G-0; SRM 51-40-0G-0 AND DRAWING # 143A7902.SDR SWAA2021052603387Gusset · crackedFWD CARGO STA 500D S-21R GUSSET BRACKET CRACK. / REMOVED AND INSTALLED AT FWD CARGO COMPT GUSSET BRACKET STA 500D STR 21R IAW B737-700 SRM 51-40-02-0G-0 AND SRM 51-04-05-0G-0.SDR SWAA2020082503380Floor Support · damagedFWD CABIN BETWEEN STA. 312 AND STA. 328 LBL 46 INTERCOSTAL FASTENER HOLE IS DAMAGED AND CRACKED. [DOT 124-016] / REPLACE INTERCOSTAL @ FWD CABIN BETWEEN STA 312 AND 328 LBL 46 AS PER B737-700 SRM 51-40-02-0G-0SDR SWAA2020082503381Floor Support · crackedFWD CABIN BETWEEN STA. 328 AND STA. 344 LBL 46 INTERCOSTAL HAS 2 CRACKS EXTENDING FROM FASTENER HOLE. [DOT 124-017] / REPLACED INTERCOSTAL @ FWD CABIN BETWEEN STA 328 AND STA 344 LBL 46 AS PER B737-700 SRM 51-40-02-0G-0SDR SWAA2020082503348Pressure Panel · cracked2 CRACKS FOUND ON HORIZONTAL PRESSURE WEB AT RBL 42 AND RBL 43 AT STA663. / ACCOMPLSIHED HORIZONTAL PRESSURE WEB REPAIR AT RT SIDE STA 663 BETWEEN RBL 40' TO RBL 60' REF B737-700 SRM 53-40-51-2R-2 DETAIL (A) FIG 202.SDR SWAA2021081703150Bracket · crackedL/H WING T/E REAR SPAR @ WS 261.00 HAS (1 EACH) BRACKET CRACKED. (18-011) / REMOVED AND REPLACED BRACKET AT LH WING T/E REAR SPAR WS261.00 AS PER B737-7 SRM 51-40-02-0G-0
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